RELAY CATALOG
LABINAL POWER SYSTEMS TF300-9E 32 LABINAL POWER SYSTEMS TF300-9E
LABINAL POWER SYSTEMS TF300-9E 32 LABINAL POWER SYSTEMS TF300-9E
SENSING & CONTROLS RELAY CATALOG
Capabilities and Featured Products
Remote Controlled Circuit Breakers
Power Relays
Hermetically Sealed Power Relays
Lightweight Relays
Generator Contactors
Custom Flat Packs
Table of Contents
Fast Information Finder
Part Number to Page Index
Capabilities and Featured Products
Labinal Power Systems Capabilities
Featured Products Article
(High Volt DC / Next Generation Contactors /
Power Distribution Boxes)
Remote Controlled Circuit Breakers
Remote Controlled Circuit Breakers
Remote Power Controllers
Power Relays
Gasket Sealed - 100 to 1000A
Gasket Sealed - 25 to 400A, Type II and Type III
Hermetically Sealed Power Relays
Hermetically Sealed - 12 to 50A
Hermetically Sealed - 100 to 400A
Terminal Covers
Lightweight Relays
Hermetically Sealed
Environmentally Sealed
Generator Contactors
Custom Flat Packs
Reference
Military to Labinal Power Systems Part Number
Index
3
4
4
5-8
9-20
21-30
31-37
38-41
42-43
44-46
46
Table of Contents
Reference
LABINAL POWER SYSTEMS TF300-9E 54 LABINAL POWER SYSTEMS TF300-9E
FAST INFORMATION FINDER
Find Information Fast
• Have an Labinal
Power Systems part
number and need more
information? Use the
part number to page
index on this page to get
the exact page of the full
product listing.
• Have a Military part
number and need
applicable Labinal
Power Systems part
number? Use the
Military part number
Index in the back of this
catalog.
• Need additional
information not
contained in this
catalog? For technical
questions, application
assistance, or the name
of your local authorized
distributor, call 1-800-
955- 7354.
Labinal Power Systems Part
No. Page No.
49- 36
6041H- 25
6042H- 31
6046H- 25
9565H 25
SM15 40
SM100D- 21
SM150D- 21
SM200D- 21
SM400D- 21
SM1000D- 21
SM100H1 38
SM135B2 42
SM400H 34
SM600BA5 - 100 10
SM600BA125 - 200 19
SM601BA10 - 60 10
Part Number to Page Index
LABINAL POWER SYSTEMS TF300-9E 54 LABINAL POWER SYSTEMS TF300-9E
CAPABILITIES
Market Trends
Aircraft and commercial off-
highway vehicle Original
Equipment Manufacturers
(OEMs) are continuously
pursuing efficiencies
associated with the design
and manufacture of vehicle
platforms. Additionally, the
OEMs are working on increasing
the functionality of system
components while reducing
operating and life cycle costs.
These activities are leading to
the migration of engineering
and system design activities
to Tier 1 system integrators
and their supply partners such
as Labinal Power Systems.
This supplier team will be
required to design, develop,
and manufacture performance
rated products such as relays,
"smart" contactors, high voltage
DC contactors, and power
distribution junction boxes that
minimize cost, reduce weight,
and limit product dimensions in
order to support accomplishing
OEM objectives.
What Problem Does
Labinal Power Systems
Solve?
Aircraft OEMs discovered that
outsourcing power distribution
management requirements to
Tier 1-system integrators and
their vendor base is an effective
alternative that mitigates risk
and leverages the subsystem
and component manufacturer
expertise. The success of such
outsourcing efforts benefits the
OEM and leads to more reliance
on qualified Tier 1-System
Integrators for electrical
systems. To compliment
this OEM strategy, Labinal
Power Systems formed the
ES&C product divison, which
combines the product pedigree
of illuminated pushbutton
switches, cockpit displays and
keyboards, NVIS products, pilot
controls, and a variety of MIL-
qualified aerospace switches,
relays, contactors, and circuit
breakers, to broaden the product
portfolio and support execution
of a subsystem strategy. Labinal
Power Systems' objective is
to be the leading candidate for
the supply of aerospace power
distribution components and
subsystems.
The Labinal Power
Systems Solution
Labinal Power Systems is
an attractive partner in the
design and development of
integrated relay and contactor
components and subsystem
power junction boxes. Our
development process employs
sound methodology to identify,
assess, and manage program
risk. The components of this
approach include Phase-Gate
Reviews, Project Management,
and Six Sigma for Design and
Development. This process in
conjunction with Labinal Power
Systems' extensive Product
Portfolio and Capabilities
enable the Aerospace Group's
ES&C division to be a single
source supplier for power
protection, distribution, and
switching components. The
system integrators have the
option of sourcing pedigree
relays and contactors for their
power distribution box designs
or subcontracting the entire
power distribution subsystem to
Labinal Power Systems.
Phase-Gate Reviews
This process organizes product
development activities from the
idea through product launch
into a series of phases. The
activities within each phase
are multifunctional, and are
designed to provide information
that progressively reduces risk.
Consistent application of the
process promotes successful
on-time product development,
as well as competitive pricing
and high quality levels.
Project Management
Product development projects
involve the iterative planning,
execution and control of project
team activities in order to meet
the competing demands of
scope, timing, cost, risk and
quality. Project management
methodology affords the
application of knowledge, skills,
tools and techniques to meet
these requirements.
Six Sigma for Design and
Development
Six Sigma for Design and
Development is a methodology
using normal Six Sigma
tools, but applies them early
in the design process. This
methodology instills the product
development process with
the same Six Sigma process
rigor found in Labinal Power
Systems manufacturing to
create successful products in a
competitive marketplace.
Product Portfolio
Labinal Power Systems'
complete product portfolio
allows flexibility to partner with
customers having a variety of
relay and contactor subsystem
and component needs. Labinal
Power Systems' engineers
design additional value into
traditional power distribution
components and subsystems
through electronics, while
balancing customer concerns
for size, weight, cost, and
performance. Labinal Power
Systems' Power Distribution
Boxes are a prime example of
value-added engineering. Proven
relay, contactor, and circuit
breaker products are packaged
into a single line replaceable
assembly that offers the user
a customized power module
that significantly reduces overall
system weight, improves
system level reliability, and
maintainability.
The Labinal Power Systems
product portfolio is recognized in
the aerospace industry as MIL
qualified for performance rated
power distribution products.
Labinal Power Systems'
experience in designing relays
and contactors to MIL Spec
requirements such as MIL-
PRF-83383, MIL-R-6106/9,
/10, /11, and MIL-R-6101/48
ensures the customer of
relays and contactors that
will operate in the most
challenging environments and
in accordance with the strictest
performance requirements.
These same component design
considerations are incorporated
into Labinal Power Systems'
latest designs such as High
Voltage DC Contactors and also
in subsystem designs such as
a Power Distribution Box (PDB).
These products are highlighted
in the Featured Products
Article on page 7-8.
LABINAL POWER SYSTEMS TF300-9E 76 LABINAL POWER SYSTEMS TF300-9E
CAPABILITIES
The product portfolio includes:
• Smart Contactors with cur rent
sensing protection, Ground
Fault Interrupt technology,
or Arc Fault Circuit Interrupt
technology.
• 28 Vdc Contactors (50 to 1000
amperes).
• 270 Vdc Contactors (25 to
350 amperes).
• 115/230 Vac 400 Hertz
Contactors (30 to
430 amperes).
• 750 Vdc Contactors (100 to
600 amperes).
• Power Distribution Junction
Boxes.
• A variety of aerospace
switches (rocker, toggle,
pushbutton and limit)
• Pilot Controls including
customized flap controls,
landing gear controls, throttle
controls, trim controls (for
mechanical pitch, roll and yaw),
and fire emergency controls.
• Displays, readable in both
direct sunlight and at night,
including the popular Series
900 fiber optic displays,
as well as displays with
surface mount devices and
programmable electronic
arrays.
• Keyboards that are sunlight
and night light readable
and suited for virtually any
application, including flight
management panels, handheld
data communications panels,
shipboard computer control
panels, fire system control
panels, ground support
equipment, and radar and
telemetry control panels.
Labinal Power Systems
Aerospace keyboards also
incorporate logic boards, photo
sensors, rotary and toggle
switches, and annunciators,
and have features such as
micro-processor interfacing
and programmable logic
control.
• NVIS products such as
cockpit controls, displays and
keyboards, and illuminated
push button switches that
conform to MIL and NVIS
specifications and any unique
customer needs.
• Illuminated Pushbutton
switches with a multitude of
options ranging from sunlight
readable, NVIS-compatible,
incandescent and LED
lighting to various mounting
and termination options for
flexible installation and retrofit
applications.
• Electro-mechanical thermal
circuit breakers (0.5 to 300
amperes) - single phase or
three phase thermally actuated
devices offered in conventional
design or with integrated
Arc Fault Circuit Interrupt
technology.
• Remote Control Circuit
Breakers (5 to 125 amperes)
- single phase or three-phase
devices sold separately or as a
subsystem when combined
with a necessary indicator
control unit (0.5 ampere circuit
breaker).
• Electromechanical Remote
Power Controllers (125 to
200 amperes) - single-phase
devices sold separately or as
a subsystem when combined
with a necessary indicator
control unit (0.5 ampere circuit
breaker).
Labinal Power Systems
Capabilities
• Proven excellence in
component and subsystem
design, development, testing,
qualification, and production for
both military and commercial
aerospace applications.
• A manufacturing organization
that emphasizes customer
satisfaction by focusing on
cost, quality, and delivery of
the product portfolio.
• Altitude / temperature testing
chamber simulating altitude to
80,000 feet and temperatures
from -65°C to 125°C.
• Test capabilities of 115/200 Vac
400 Hz to 3600 amps, 28 Vdc
to 10,000 amps, 270/350/475
Vdc to 1,500 amps.
• Environmental tests for Sand
and Dust, Shock, and
Vibration.
• Latest CAD/CAM finite
element analysis and
stereolithographic techniques,
and PRO-E design.
• Model Shop flexibility to
respond to design changes
and rapid turn around of
prototypes.
The Labinal Power
Systems Difference
There are a number of relay
and contactor suppliers
in the aerospace market.
However, few possess the
vertical integration needed
to engineer and manufacture
to both MIL Spec and OEM
customer specifications to
ensure consistency of quality
operation in components and
subsystems.
Labinal Power Systems affords
its customers the following
difference:
• Strong brand recognition,
customer loyalty, and
demonstrated market
presence for over 80 years
• Ability to leverage the
company's size, financial
strength, and scope to drive
superior results. Labinal
Power Systems has the ability
to leverage the engineering
resources of a multi-billion
dollar company.
• An extensive product
portfolio that complements
integrated subsystem design
competency.
• A flat organizational structure
that allows for the optimal
blend of best value technical
approach and test support
within budget and schedule
constraints.
• Dedicated program managers
that understand and
communicate the "voice of the
customer". Design software
that promotes concurrent
engineering and the exchange
of customer data.
• Co-located engineering,
manufacturing, and
development resources
promote robust product
development and product
support.
Labinal Power Systems' unique
product portfolio, its ability
to design and manufacture
components and subsystems,
and customer centric strategy
mitigates the risk associated
with new aircraft electrical
power distribution systems.
Labinal Power Systems is an
ideal candidate to consider for
engineering and manufacturing
collaboration on all future
commercial, General Aviation,
and military programs.
LABINAL POWER SYSTEMS TF300-9E 76 LABINAL POWER SYSTEMS TF300-9E
FEATURED PRODUCTS
Changing Aerospace
Industry
In today's consolidating
aerospace industry, Tier
1-System Integrators and
Airframe Manufacturers
desire more value from their
component suppliers. A qualified
supplier must not only have
an extensive product portfolio,
but must also display proven
subsystem capabilities. These
abilities include the capacity
to design, manufacture,
and test customized power
distribution assemblies that
consolidate multiple functions
in a single package. Over the
past decade, Labinal Power
Systems acknowledged this
fact, and has focused its
attention on developing these
value-add competencies to
become a recognized leader in
integrated power distribution
systems. Specifically, Labinal
Power Systems has stayed
at the forefront of product
/ technology development
through the development of
the following components and
subassemblies: High-Voltage
DC (HVDC) Contactors, Next-
Generation Alternating Current
(AC) Contactors, and Power
Distribution Boxes.
High-Voltage DC
Contactors
As electrical power systems of
270Vdc and greater become
the application standard for
high performance aircraft, the
requirements for switching and
protection components become
increasingly demanding. DC
switching has always posed
greater design challenges versus
AC applications. With AC, the
current naturally passes through
zero each half cycle resulting in
quick arc extinction after contact
separation.
Conventional 28Vdc switching
can also be accomplished using
single or double break contact
sets. In this case, the inherent arc
voltage generated by the anode
and cathode of the arcing contact
sets is capable of opposing and
interrupting the current flow. The
low voltage device counts little
on the arc voltage generated in
the actual arc column to drive the
current to zero.
Once the system voltage is
increased beyond the 48Vdc
rating, the interruption scheme
becomes more challenging.
Although the arc voltage
generated by the arc column
is generally small compared
to the anode and cathode
voltages, it will increase as the
open contact gap widens. The
actual arc voltage generated is
a function of contact materials,
the gas or atmosphere in the
contact region, application
current, and contact gap.
Unfortunately, there is
zero crossover to facilitate
interruption, and the design
must rely on open gap or arc
stretching to match the system
voltage. Therefore, with a single
or double break contact set,
the ability to interrupt 270Vdc
quickly becomes size impractical
without a more involved
interruption scheme.
Labinal Power Systems
Technical Approach
The technology chosen for
use within the Labinal Power
Systems line of 270Vdc
contactors is splitting the arc into
multiple series arcs under the
influence of a constant magnetic
field. This is accomplished by
driving the arc column into a set
of metallic plates housed within
an insulated arc chute assembly.
The multiple plates then provide
the significant anode and
cathode contribution to the arc
voltage required for interruption.
The plates also help to cool the
arc column, causing the arc to
exist at a higher potential and be
stabilized in a predictable location
in the plate. By placing multiple
plates within the arc chute, the
arc voltage generated during
interruption can be increased
resulting in less volume required
by the arc chute.
With the use of permanent
magnets for controlling the
arc column, the interruption is
consistent even at low levels of
application current. This results
in extended low-level contact
life. This Labinal Power Systems
design allows for smaller device
size and the ability to the mount
the products in a compact
power distribution subsystem.
Benefits of Labinal Power
Systems HVDC Technology
The Aerospace Group's ES&C
division has long been involved
in programs addressing
requirements for High Voltage
Direct Current (HVDC)
applications. Few competitors
rival Labinal Power Systems'
knowledge and experience in
this technology over the past two
decades. The proven air break
technology used by the Labinal
Power Systems HVDC contactor
line provides the following
benefits that competitive HVDC
product offerings (hermetic) do
not provide:
• Labinal Power Systems
was the first contactor
manufacturer to complete
product design and flight
safety tests for 270Vdc aero
space devices.
• Hermetic sealing material
adds unnecessary device
weight. Hermetic sealing
material degrades over time
compromising the controlled
atmosphere within the arc
chamber, potentially leading to
device failures. Labinal Power
Systems devices have no
requirement for a seal.
• Hermetic sealed devices are
classified by an allowable
leakage rate, suggesting
they are inherently unstable
over time and susceptible
to "dormant" failures. The
Labinal Power Systems design
increases reliability because
the splitter plates eliminate
single point of failure (inability
to interrupt) associated with
failed hermetic devices.
• Load Polarity - Labinal
Power Systems' devices
are bi-directional without
restriction. Labinal Power
Systems devices reliably
switch small current loads as
well as high current loads.
• Electrical Life - Labinal Power
Systems end of life characterized
by contact voltage drop.
• Labinal Power Systems'
design is robust and operates
well in harsh environments as
demonstrated by past program
performance and application of
commercialized product.
• Labinal Power Systems' device
is a "Qualified" technology per
MIL-R-6106 standard for all
contactors.
• Labinal Power Systems' device
packaging easily tailored for
application footprint.
• Increased capability to
dissipate energy for switching
inductive loads.
• Consistent and controlled
switching transients due to
ramped build up of arc voltage
upon interruption.
• Line Replaceable Unit
packaging minimizes
maintenance time.
LABINAL POWER SYSTEMS TF300-9E 98 LABINAL POWER SYSTEMS TF300-9E
The Labinal Power Systems
design does not require a
hermetic seal, providing several
advantages in application. In
military applications, the use
of splitter plate technology
allows the device to function
reliably throughout the life
of the airframe while being
subjected to harsh combat
field environments and flight
profiles that involve extreme
levels of vibration and shock that
can compromise competitors'
hermetic seal product designs.
The loss of a hermetic seal
causes device failure as it relies
on the sealed atmosphere within
the device to interrupt high
voltage. A failure of this nature
could cause mission cancellation,
mission abort, or even loss of
aircraft. If installed in commercial
aircraft applications, hermetically
sealed devices would require
periodic maintenance crew
checks to prevent the risk of
"dormant" failures associated
with this design. The Labinal
Power Systems design
reduces/eliminates the need
for maintenance involvement
and better supports Air Carrier
objectives for maintenance-free
devices.
Combining ongoing research
with current product
development, Labinal Power
Systems continually strives to
be a premier supplier of High-
Voltage DC components and
subsystems.
Next Generation
Contactors
Labinal Power Systems has
extensive experience in
the research, design, and
development of various AC
Contactor product lines,
including "Smart" contactors with
integrated current sensing and
Arc Fault Circuit interrupt (AFCI)
technology, 28Vdc Lightweight
Contactors, and Advanced
Generator Contactors.
"Smart" Contactors
Labinal Power Systems is
currently developing 175/60 amp
packages for galleys, pumps,
and primary load distribution.
These contactors use the latest
technologies, and can include
current sensors for overcurrent
protection and/or AFCI sensing.
Internal / centralized electronics
control are also features of these
devices. Labinal Power Systems
is continually looking for lower
weight / size product solutions; a
prime example being the 60 amp
"Smart" contactor that is currently
no bigger than an Labinal Power
Systems 3-phase motor circuit
protection device.
28Vdc Lightweight Contactors
Labinal Power Systems is also
developing a new 28Vdc, 50-400
Amp contactor family whose
focus is on the reduction of
weight and cost. Bolt-on designs
combine power terminations
and mechanical mounting, and
contain captive hardware for
all mounting fasteners. Both
Single Pole Single Throw and
Single Pole Double Throw
configurations are available with
features such as SubD or sealed
in-line connectors.
Advanced Generator
Contactors
Based upon Labinal Power
Systems' existing SM15 product
line, a new AC Generator
contactor line of products is
emerging. These contactors have
automatic control connector
mating and either Three Pole
Single Throw or Three Pole
Double Throw main contacts.
Labinal Power Systems offers
115 VAC or 230 VAC (350-800Hz)
generator contactors that are
bolt-on designs with SubD
connectors and rated at either
260 amps or 430 amps. They
are currently one of the smallest
and lightest AC contactors in
the aerospace generator relay
market, accommodate Variable
Frequency and double voltage
aircraft architectures, and are
suitable for either stand-alone
applications or power distribution
boxes.
Power Distribution Boxes
Labinal Power Systems' proven
component expertise and
packaging capabilities have
allowed ES&C to become a
subsystem supplier in both the
commercial jet and military
aircraft markets. An example of
these competencies is evident
in the development of ED&C
Power Distribution Boxes. A
Power Distribution Box provides
the next generation of AC and DC
power distribution and protection,
whereby conventional relays,
contactors, and circuit protection
devices are incorporated into a
densely packaged, single line
replaceable assembly. Benefits
of this type of bundled packaging
include weight reduction,
reduced maintenance labor
time due to the line replaceable
nature of these boxes, minimal
program risk since commercially
off the shelf components are
incorporated as often as possible
into the design, significantly
lower on-aircraft test time since
they are tested to the customer
acceptance testing standards
prior to shipment, and reduced
overall aircraft build time since
Power Distribution Boxes
support a centralized power
distribution architecture.
Power Distribution Boxes
(PDBs) are typically designed
and manufactured for each of
the main generators onboard an
aircraft in order to provide power
to various bus lines and aircraft
systems, while other, separate
Battery/ External PDBs can
provide switching power to a
standby power bus and several
components such as overhead
panels, service lights, and the
emergency locator transmitter.
Labinal Power Systems has
supplied customers with AC
Power Distribution Boxes with
features that direct outputs to
high current loads, serve as
power feeders to lower current
circuit breakers, or act as current
transformers to monitor all
outputs. DC Power Distribution
Boxes contain such features as
Transformer Rectifier Units and
Battery Contactors that direct
outputs to high current loads, and
incorporate Hall Effect sensors
to monitor outputs. All Power
Distribution Boxes can incorporate
customized current carrying bus
structures, and provide spare
electrical power generation
capacity to support future
electrical systems growth/capacity.
FEATURED PRODUCTS
LABINAL POWER SYSTEMS TF300-9E 98 LABINAL POWER SYSTEMS TF300-9E
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB)
Qualified
Qualified to demanding perfor-
mance parameters of MIL- PRF
- 83383 standard.
Use as a Relay, Circuit Breaker, Or
Both
RCCBs combine the best attri-
butes of a circuit breaker and a
relay. Automatically protects the
wires and the load device dur-
ing circuit/load breakdown, but
allows the flight deck control of
the load during normal opera-
tion.
Weight and Cost Savings
In distributed-load applications,
RCCBs are a more efficient
power distribution solution pro-
moting cost and weight savings
through the elimination of long
runs of heavy cables associ-
ated with the conventional relay
- flight deck circuit protector
method. Control of the RCCB
requires only one #22 AWG
control wire from the ICU on the
flight deck to the RCCB.
Cockpit Space Savings
An RCCB system removes the
presence of large circuit break-
ers from the cockpit while per-
mitting remote On/Off operation
from the flight deck. Combine
Labinal Power Systems RCCB
with Indicator Control Unit (ICU)
model #1500-052-05.
OVERLOAD CALIBRATION DATA
Specification
Table
Must Hold
Must Trip
MIN
115 %
@ 25°C
MAX
138%
@ +71°C
MIN
115 %
MAX
138%
@ -54°C
MIN
115 %
MAX
150%
Test Time
Parameters
% for 1 Hour
% Within 1 Hour
Single Pole
• 28 VDC
• 115/200 VAC 400 Hz
Three Phase
• 115/200 VAC 400 Hz
• Three Phase Only
Rupture Levels 3600 A (115 VAC or 28VDC for 1 Pole and 115VAC for 3 Pole)
Endurance 50,000 Cycles
(Resistive & Inductive (Motor)
Endurance (Motor) 5-50A: 50,000 cycles; 60-100A: 25,000 cycles
Endurance (Lamp) 5-25A: 50,000 cycles; 35-50A: 25,000 cycles; 60-100A: no rating
Dielectric Strength 1500V, 60 Hz, MIL-STD-202, method 301, 0.5 MA max
Insulation Resistance 100 mega ohm min, MIL-STD-202, method 302
Thermal Temperature Range -54°C to 71°C (-65°F to 160°F). MIL-STD-202, Method 107
Vibration 10G's to 2000 Hz. Exceeds MIL-STD-202, Method 204, Condition
C, 10 microseconds max. chatter
Shock 25G's. MIL-STD-202, Method 213, 10 microseconds max. chatter
Altitude 50,000 ft.
EMI Requirements MIL-STD-461, Requirements CS114 and RE102 over the frequency
range of 14 kHz to 400 MHz and RE102 limits for Aircraft and
Space Systems.
EMI/RFI Susceptibility MIL-STD-461, Class 1D
and Generation
Moisture Resistance MIL-STD-202, method 106
Salt Spray Resistance MIL-STD-202, method 101, Condition B
Sand and Dust Resistance MIL-STD-202, method 110, Condition A
Fungus Resistance MIL-HDBK-454, Guideline 4
Explosion Proof MIL-STD-202, method 109
Weight (Single Pole) 5-25A: 318 grams (0.703 lbs.); 35-50A: 325 grams (0.719 lbs.); 60-
100A: 332 grams (0.734 lbs.)
Weight (w/ Auxiliary Contacts) 5-25A: 332 grams (0.734 lbs.); 35-50A: 339 grams (0.750 lbs.); 60-
100A: 346 grams (0.766 lbs.)
Weight (Three Phase) 2.0 lbs. max.
PERFORMANCE DATA
LABINAL POWER SYSTEMS TF300-9E 1110 LABINAL POWER SYSTEMS TF300-9E
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB)
Three Pole Single Throw (Double Break Contacts)
Catalog
Number
Rated Contact Load
(Amperes)
115/200 V 400 Hz MIL-PRF-83383
Part NumberRes. Ind. Motor Lamp
SM601BA10A1 10 10 10 10 M83383/04-03
SM601BA15A1 15 15 15 15
SM601BA20A1 20 20 20 20 M83383/04-05
SM601BA25A1 25 25 25 25
SM601BA35A1 35 35 35 35 M83383/04-07
SM601BA40A1 40 40 40 40 M83383/04-08
SM601BA50A1 50 50 50 50
SM601BA60A1 60 60 60 60 M83383/04-10
Contact factory on alternate amperage, trip times, control configurations,
grounding, auxiliary switches, and mounting systems.
Engineering Data
Single Pole Single Throw (Double Break Contacts)
Catalog
Number
Rated Contact Load (Amperes)
MIL-PRF-83383
Part Number
Maximum
Weight Oz/gm
28 Vdc 115/200 V 400 Hz
Res. Ind. Motor Lamp Res. Ind. Motor Lamp
SM600BA5A1 5 5 5 5 5 5 5 5 M83383/02-01 11.75/332
SM600BA5N1
10 10 10 10 10 10 10 10
M83383/01-02 11.25/318
SM600BA10A1 M83383/02-03 11.75/332
SM600BA10N1
15 15 15 15 15 15 15 15
M83383/01-03 11.25/318
SM600BA15A1 M83383/02-04 11.75/332
SM600BA15N1
20 20 20 20 20 20 20 20
M83383/01-04 11.25/318
SM600BA20A1 M83383/02-05 11.75/332
SM600BA20N1
25 25 25 25 25 25 25 25
M83383/01-05 11.25/318
SM600BA25A1 M83383/02-06 11.75/332
SM600BA25N1
35 35 35 35 35 35 35 35
M83383/01-06 11.25/318
SM600BA35A1 M83383/02-07 12.00/339
SM600BA35N1
40 40 40 40 40 40 40 40
M83383/01-07 11.50/325
SM600BA40A1 M83383/02-08 12.00/339
SM600BA40N1
50 50 50 50 50 50 50 50
M83383/01-08 11.50/325
SM600BA50A1 M83383/02-09 12.00/339
SM600BA50N1
60 60 60 — 60 60 60 —
M83383/01-09 11.50/325
SM600BA60A1 M8338/02-10 12.25/346
SM600BA60N1
75 75 75 — 75 75 75 —
M83383/01-10 11.75/332
SM600BA75A1 M83383/02-11 12.25/346
SM600BA75N1
100 10 0 100 —100 10 0 10 0 —
M83383/01-11 11.75/332
SM600BA100A1 M83383/02-13 12.25/346
SM600BA100N1 M83383/01-13 11.75/332
LABINAL POWER SYSTEMS TF300-9E 1110 LABINAL POWER SYSTEMS TF300-9E
ORDERING INFORMATION
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB)
OVERLOAD CALIBRATION DATA
Ratings
All
Percent
Rated Current
115 %
138%
115 %
150%
Ambient Temperature
Degrees C. ± 5°
25°C & 71°C
-54°C
Tripping Time
No Trip
1 Hour Max.*
No Trip
1 Hour Max.*
* Must trip in one hour.
SINGLE POLE
OVERLOAD CALIBRATION DATA
Ratings
All
Percent
Rated Current
115 %
138%
115 %
150%
Ambient Temperature
Degrees C. ± 5°
25°C & 71°C
-54°C
Tripping Time
No Trip
1 Hour Max.*
No Trip
1 Hour Max.*
* Must trip in one hour.
TRIPLE POLE
TRIP CURVE
Contact business unit for trip curve.
AMPERE
RATING
AMPERES
5
7. 5
10
15
20
25
35
40
50
60
75
80
100
MIN
SECONDS
7
11
12
13
14
15
16
16
13
13
13
14
17
200% Trip Times
-54°C to +71°C
MAX
SECONDS
40
40
42
45
46
50
55
55
55
60
60
60
63
400% Trip Times
-54°C to +71°C
MIN
SECONDS
1. 2
2.4
2.8
1. 7
2.9
2.6
2.8
2.9
2.9
2.6
2.5
2.7
3.5
MAX
SECONDS
6.4
6.8
8.5
8.3
7. 6
8.7
8.3
9.2
10
13
13
12.5
13
1000% Trip Times
-54°C to +71°C
MIN
SECONDS
0.3
0.33
0.42
0.35
0.4
0.4
0.35
0.36
0.4
0.26
0.26
0.3
0.38
MAX
SECONDS
1. 2
1. 1
1.05
1. 2
1. 15
1. 3
1. 3
1. 3
1.25
1. 8
1. 8
2
1. 9
OVERLOAD CALIBRATION DATA — SINGLE POLE
AMPERE
RATING
5
7. 5
10
15
20
25
35
40
50
60
75
80
100
MS P/N
M83383/01-01
M83383/01-03
M83383/01-04
M83383/01-05
M83383/01-06
M83383/01-07
M83383/01-08
M83383/01-09
M83383/01-10
M83383/01-11
M83383/01-13
Single Pole Single Throw (Double Break Contacts) Three Pole Single Throw (Double
Break Contacts)
Standard w/ Auxiliary Contacts w/ Auxiliary Contacts
*
*
*
*
Labinal Power
Systems P/N
SM600BA5N1
**
SM600BA10N1
SM600BA15N1
SM600BA20N1
SM600BA25N1
SM600BA35N1
SM600BA40N1
SM600BA50N1
SM600BA60N1
SM600BA75N1
**
SM600BA100N1
MS P/N
M83383/02-01
M83383/02-03
M83383/02-04
M83383/02-05
M83383/02-06
M83383/02-07
M83383/02-08
M83383/02-09
M83383/02-10
M83383/02-11
M83383/02-13
Labinal Power
Systems P/N
SM600BA5A1
**
SM600BA10A1
SM600BA15A1
SM600BA20A1
SM600BA25A1
SM600BA35A1
SM600BA40A1
SM600BA50A1
SM600BA60A1
SM600BA75A1
**
SM600BA100A1
MS P/N
M83383/04-03
M83383/04-05
M83383/04-07
M83383/04-08
M83383/04-10
Labinal Power
Systems P/N
**
**
SM601BA10A1
SM601BA15A1
SM601BA20A1
SM601BA25A1
SM601BA35A1
SM601BA40A1
SM601BA50A1
SM601BA60A1
All Ampere Ratings equal to Rated Contact Loads (Resistive, Inductive, Motor, and Lamp) except as noted.
* No Lamp Load Rating
** Contact Factory
Note: Contact factory on alternate amperage, trip times, control configuations, grounding, auxilary switches, mounting systems, etc.
AMPERE
RATING
AMPERES
10
15
20
25
35
40
50
60
MIN
SECONDS
12
13
14
15
16
16
13
13
200% Trip Times
-54°C to +71°C
MAX
SECONDS
80
80
80
80
80
80
80
80
400% Trip Times
-54°C to +71°C
MIN
SECONDS
2.8
1. 7
2.9
2.6
2.8
2.6
2.9
2.4
MAX
SECONDS
11
10
9.6
10
11
10
10
16
1000% Trip Times
-54°C to +71°C
MIN
SECONDS
0.42
0.35
0.4
0.4
0.35
0.36
0.4
0.26
MAX
SECONDS
1. 3
1. 2
1. 15
1. 3
1. 3
1. 3
1.25
1. 8
OVERLOAD CALIBRATION DATA — THREE POLE
LABINAL POWER SYSTEMS TF300-9E 1312 LABINAL POWER SYSTEMS TF300-9E
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB)
Engineering Data
Application Note
C8
FLIGHT DECK
SWITCH
MS22073-1/2 OR
MS26574-1/2
B
U
S
SL
O
A
D
1/2 AMP
100 AMPS RCCB
With RCCB Distributed Load Concept
Typical Wiring Diagrams
NOTE: Terminals 5A and 5B internally grounded to the mounting leg (s). Integrated Wire
Termination (IWT) module accepts pin contacts P/N M39029/1-100 or -101. Use with
insertion/extraction tool M81969/14-02.
Contacts and Coil
Circuits Only
S2
S3
Three Pole
A2
Auxiliary Contacts
S1
Intermittent Duty
Coils Current Cut-Off
Controlled Electronically
B2
C2
A1
B1
C1
Contacts and Coil
Circuits Only
S2
S3
A2
S1
A1
Single Pole
Intermittent Duty
Coils Current Cut-
Off Controlled
Electronically
Without RCCB
C8
C8
B
U
S
S
FLIGHT DECK
100 AMPS
RELAY
SWITCH1/2 AMP
100 AMPS
L
O
A
D
Integrated Wire Termination Module
(MIL-STD-1549)
5A 5B
S3 S1 S2
A1
A2
To Indicator/
Control Unit
Circuit Breaker
Type MS22073-
1/2 OR MS26574-
1/2 Backup Control Power (when used)
115 V 400 Hz or 28 Vdc
(Must be same AC Phase as the
“Line” Power)
Internal Connection
Auxiliary Contacts When Applicable
LINE
LOAD
3 4 6
LOAD
LOAD
LOAD
LINE
LINE
LINE
To Indicator/
Control Unit
Circuit Breaker
Type MS22073-
1/2 OR MS26574-
1/2
5A 5B
S3 S1 S2
Backup Control
Power (when
used) 28 Vdc
Internal Connection
Auxiliary Contacts
3 4
Wiring for Multiple
Line Protection
345A 6
5B
345A 6
5B
345A 6
5B
LABINAL POWER SYSTEMS TF300-9E 1312 LABINAL POWER SYSTEMS TF300-9E
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB) — 1 POLE AND 3 POLE
Engineering Data
Approximate Dimensions - 1 Pole
Options
• Special application auxiliary
switches
• Unique grounding
• Power sources
• Other current ratings
• Control via systems other
than I/CU
• Low level auxiliary contacts
available
• Data Bus/Interface capability
available
• Electronically held coil
• Moisture resistant sealing
Three Pole
Typical Placement of
Rating on Top Plane
LOAD A2
LINE A1
50
.172/4.37 DIA.
2 MTG. HOLES
R. 20
5.08
.688/
17.48
2.940
74.68
3.250
82.55
Main Contact
Position Indicator
Red: Closed; Green: Open
Mtg. Flanges
Mate As Shown
1.530
38.86
2.250
57.15
.350
8.89
.07
1.778
.500 - .610
12.70 - 15.24
.180
4.57
3.42
86.87
Name
Plate
.084
2.13
4.26
108.20
.056
1.42
.42
10.67
1.200
30.48
LOAD A2
LOAD B2
LOAD C2
LINE A1
LINE B1
LINE C1
50
2.526
64.16
2.940
74.68
3.250
82.55
2.526
64.16
Main Contact
Position Indicator
Red: Closed;
Green: Open
2.28
57.91
1.50
38.86
.350
8.89
.07
1.78
.05
1.27
4.26
108.20
3.43
87.12
.130
3.30
.77
19.56
2.03
51.56
3.29
83.57
3.69
93.73
Location of
NamePlate
Coil Operate Current/Set And Trip Time RCCB
Circuits
1 Pole
3 Pole
Nominal
System
Voltage
28 Vdc
(18 volts MIN.)
115 Vac
400 Hz (104 V.
MIN.
28 Vdc
(18 volts MIN.)
115 Vac
400 Hz (104 V.
MIN.)
I/CU Set
Current
@ Nom
Voltage
(Mulliamp)
2
2
2
2
Set Coil
Current
@ Nom
Voltage
Pulse
3.0 AMP
MAX
10 AMP
MAX
7.0 AMP
MAX
13.0 AMP
MAX
Nominal
Voltage &
Room Temp.
20 Millisec
15 Millisec
20 Millisec
15 Millisec
MAX. Set Time
Most Adverse
Condition - MIN.
Voltage 71°C.
Ambient
35 Millisec
30 Millisec
35 Millisec
30 Millisec
*I/CU. Trip Current Nominal
71°C &
Nominal
Voltage
1.4 AMP
6.8 AMP
**
1.5 AMP
4.3 AMP
**
-54°C &
Nominal
Voltage
1.9 AMP
6.3 AMP
**
2.0 AMP
3.3 AMP
**
Room Temp.
Nominal
Voltage
1.6 AMP
8.6 AMP
**
1.7 AMP
4.5 AMP
**
71°C &
Nominal
Voltage
0.9 AMP
***
6.1 AMP
**
0.9 AMP
***
4.0 AMP
**
-54°C &
Nominal
Voltage
2.1 AMP
7.0 AMP
**
2.2 AMP
3.1 AMP
**
MAX.
Standby
Current
Milliamp
10
10
10
10
* MAX. I/CU. Line Impedance 7.5 Current Decreases w/Time so that I2t
** Average Half-Wave Rectified DC Current ***Absolute Min. Value from -54° to +71°C
LABINAL POWER SYSTEMS TF300-9E 1514 LABINAL POWER SYSTEMS TF300-9E
Description
The Remote Control Circuit
Breakers (RCCB) concept, as
load controllers in distributed-
load applications, provides for a
more efficient power distribution
system with less line loss at a
lower cost and with less weight
than the conventional relay-flight
deck circuit protector method.
Designed to meet the
requirements of MIL-PRF-83383,
the RCCB's capability and
advantages include:
• Fusible link fail safe
• Remote on/off operation from
the flight deck
• Visual indicators for open
(green) and closed (red) on
top surface
• Substantial reduction in
weight and size
• Most direct route from power
source to load
• Single wire control line from
I/CU to RCCB
• Double-break power contact
assembly
• Indication of trip or set by
position of the ½ ampere circuit
breaker on the flight deck
• Elimination of long runs of
heavy and costly cables
• Magnetically latched coils
(low power consumption)
• Use as a relay or circuit
breaker or both
• Flanges mate for in-line or
side-by-side mounting
• 1PST for DC or single phase AC
• 3PST for three phase AC only
Application
The Remote Control Circuit
Breaker (RCCB) is a combination
relay and circuit breaker which
can be released or set by
applying a release or set coil
current electronically controlled
by a command from the
Indicator/Control Unit (I/CU) (a ½
ampere fast trip, thermal circuit
breaker).
With power available to terminal
#4 and/or terminal A1 (28 Vdc or
115 V 400 Hz) on 1PST RCCB:
to terminal #4 (28 Vdc) and/
or both terminals B1 and C1
(115 V 400 Hz) on 3PST RCCB,
the RCCB will assume the
state requested/indicated by
the I/CU. If power is removed
from terminal #4 and A1 on
1PST or from terminal #4 and
both B1 and C1 on 3PST, the
RCCB will remain in the state it
was in prior to power removal.
When power is reapplied to
the terminals, the RCCB will
assume the state indicated by
the I/CU.
With the RCCB closed, an
overload or fault current on any
line or lines will cause the RCCB
to trip and in turn will cause a
controlled overload of the I/CU,
causing it to trip also. A fault or
overload on any power contact
will cause the RCCB to trip open
within the time limits specified
regardless of the availability of
coil power. To reclose the RCCB,
the I/CU line (line 3 to ground)
must be opened by the I/CU or
series switch and reconnected
to ground.
Other Performance
Parameters For MIL-
PRF-83383
• Coordination. An overload
applied to two devices in
series with a 2 to 1 current
rating will result in only the
lower rated device opening.
• Rupture capability to 3600A
(115 Vac rms or 28 Vdc for
SM600BA and 115 Vac rms
for SM601BA series)
• Dielectric. 1500 V, 60 Hz,
MIL-STD-202, Test Method
301, 0.5 MA maximum
• Explosion-proof. MIL-
STD-202, Test Method 109
• Thermal Temperature Range.
-54°C to 71°C (-65°F to
160°F). MIL-STD-202, Test
Method 107
• Insulation Resistance. MIL-
STD-202, Test Method 302,
100 Megohms minimum
• Aircraft Electrical Power. MIL-
STD-704
• Vibration. 10 g's to 2000 Hz.
MIL-STD-202, Test Method
204. Condition C (-54°C,
25°C, and 71°C). Maximum
duration of contact transfer to
uncommanded state: 10x10-6
seconds.
• Shock. 25 g's. MIL-TD-202,
Test Method 213. Maximum
duration of contact transfer to
uncommanded state: 10x10-6
seconds.
• Altitude. 50,000 feet
• EMI, MIL-STD-461, Class 1D
• Moisture Resistance. MIL-
STD-202, Test Method 106
• Fungus Resistance. MIL-STD-
454, Guideline 4
• Sand and Dust Resistance.
MIL-STD-202, Test Method
110, Test Condition A
• Salt Spray Resistance. MIL-
STD-202, Test Method 101,
Test Condition B
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB) — 1 POLE AND 3 POLE
Engineering Data
LABINAL POWER SYSTEMS TF300-9E 1514 LABINAL POWER SYSTEMS TF300-9E
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB)
Introduction
Part of the weight of the
modern jet aircraft comes from
the electrical wires and power
control systems needed to
distribute the electrical energy.
As these aircraft increase
their passenger carrying
capability, the electrical power
management system becomes
more complex and could
become heavier. Wire runs of
more than 300 feet from the
flight deck circuit breakers to
the load become common.
Utilization of Labinal Power
Systems' Remote Controlled
Circuit Breakers (RCCB) close
to the load or power source will
eliminate much of these long,
heavy, and expensive wire/
cable. Control of the RCCB
requires only one #22 AWG
control wire from the flight deck
to the RCCB.
Weight reduction, directly from
wire use and indirectly from
(generator) line heat loss, and
installation and maintenance
cost reductions becomes
significant.
The RCCB combines the
best attributes of a circuit
breaker and a relay. The RCCB
automatically protects the wires
and the load device during
circuit/load breakdown, but
allows flight deck control of the
load during normal operation.
Operation
The RCCB is basically a relay
and a circuit breaker and allows
the utilization of each identity
singularly or in combination,
depending upon the application.
All of the RCCB's capabilities
apply in either application.
It can be employed as a relay
located adjacent to its load and
remotely operated much like
relays are today through control
wiring and a switching device in
the flight deck.
It can also be utilized as a circuit
breaker and mounted adjacent
to the load, the power source,
or even the flight deck.
Single Pole RCCB
Motor Operation
Figure 1 depicts a simplified
presentation of the RCCB.
Figure 2 describes the "motor",
which when "energized", will
result in typical armature
transfer operation.
The magnetic circuit utilizes
a permanent magnet as a
fulcrum and latch for the rocking
armature and uses electro-
magnets (coils) at each end of
the armature stroke for transfer
purpose. In the set position
(Figure 2), the flux generated by
the permanent magnet follows
a patch from the top of the
permanent magnet through the
armature, through the left leg of
the electro-magnet and back to
the permanent magnet.
When the coil T1 -T2 is
energized, the flux generated
is such that it "flows" through
the permanent magnet in the
same direction as the flux
generated by the permanent
magnet itself. Its path now,
however, is through the right leg
of the electro-magnet. The flux
generated by the electro-magnet
increases in magnitude as
power is applied, and as the flux
builds up in the path through
the right leg of the electro-
magnet, the flux tending to latch
the armature in the left leg of
the electro-magnet becomes
very small in comparison. The
armature then "transfers" and
seals at the pole face of the
right leg of the electro-magnet.
The cutthroat contact B in series
with coil T1 -T2 is opened by
mechanical actuation due to
the armature movement. In
Figure 2, a "dotted extension"
of the armature represents
the mechanical actuator of the
cutthroat contacts. In actual
design, this is accomplished
more conveniently through only
one armature extension and
an appropriate actuator which
drives both contacts B and A.
Single Pole
• 28 VDC
• 115/200 VAC 400 Hz
Three Phase
• 115/200 VAC 400 Hz
• Three Phase Only
Qualified
Meets MIL-PRF-83383
Weight and Cost Savings
Saves fuel by eliminating long
runs of heavy, costly cables
Space Savings
Keeps larger breakers out of
cockpit
RCCB System for Remote
Operation
To form an RCCB system
enabling remote On/Off opera-
tion from the flight deck, com-
bine the Labinal Power Systems
RCCB with Indicator Control
Unit (ICU) model #1500-053-05
on pg. 13.
Single Wire from Flight
Deck
Control of the RCCB requires
only one #22 AWG control wire
from the ICU on the flight deck
to the RCCB.
Use as a Relay, Circuit
Breaker, or Both
Combines the best attributes
of a circuit breaker and a
relay. Automatically protects
the wires and the load device
during circuit/load breakdown,
but allows the flight deck
control of the load during
normal operation.
Design Concept
BI-METAL
E-PIVOT
H-LATCH
G-PIVOT
LOAD-L2 LOAD-L1
K
B
D
A
S1 S2
M
N
J
T2
T1
L-LEVER
ARMATURE
PERMANENT MAGNET
DOUBLE THROW
TOGGLE SWITCH
SET
POSITION
TRIP
POSITION
STATIONARY
CONTACTS
I
LATCH
BAR
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
SET
(CLOSED)
COIL
C
B
S
N
A
S1 S2
T2
T1
PERMANENT MAGNET
TRIP
(OPEN)
COIL
SET
(CLOSED)
COIL
Figure 1
BI-METAL
E-PIVOT
H-LATCH
G-PIVOT
LOAD-L2 LOAD-L1
K
B
D
A
S1 S2
M
N
J
T2
T1
L-LEVER
ARMATURE
PERMANENT MAGNET
DOUBLE THROW
TOGGLE SWITCH
SET
POSITION
TRIP
POSITION
STATIONARY
CONTACTS
I
LATCH
BAR
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
SET
(CLOSED)
COIL
C
B
S
N
A
S1 S2
T2
T1
PERMANENT MAGNET
TRIP
(OPEN)
COIL
SET
(CLOSED)
COIL
Figure 2
LABINAL POWER SYSTEMS TF300-9E 1716 LABINAL POWER SYSTEMS TF300-9E
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB) — DESIGN CONCEPT
The opening of contact B occurs
in the last several thousandths
of an inch travel of the armature
movement. After coil opening,
the armature movement
continues (until it seats i.e.
seals), due in some degree to
the inertia of the armature, but
mostly due to the magneto-
motive force of the permanent
magnet in conjunction with the
decreasing air gap at the right
pole face.
The device now is again in a
stable position, but the armature
has transferred and the following
conditions exist:
Contact A is closed and contact
B is open, and the armature
is sealed and latched at the
right leg of the electro-magnet.
To transfer the armature to its
original position, energizing the
coil S1-S 2 allows the process
described above to occur in the
opposite direction.
There are a number of
advantages to this design
approach of the "motor."
1. The coils open upon transfer
of the armature; hence, the
actual "on time" or duty cycle
approximately equals the
operate time of the relay.
Accordingly, the coil can
be driven hard without fear
of burnout. The "hot coil"
with the low timer constant
results, in turn, in fast operate
times.
2. Using intermittent duty
coils (smaller coils with less
copper) results in less weight
and smaller sizes.
3. Power is conserved. This is
important for two reasons.
If a relay is to use power, it
must be available. In some
of the present day and future
vehicles, power remains an
expensive commodity, and
elimination of coil power
drawing (10-35 watts) in
power devices can add up
especially when vehicles
sophistication requires use
of a significant number
of these devices. Also, it
must be remembered that
power utilized by relay coils
generate heat which must
be dissipated. The necessary
elimination of this heat, in
turn, requires the use of
additional energy from the
main power source.
4. As indicated, the cutthroat
contacts are opened by the
armature mechanically during
the last several thousandths
of an inch travel of armature
movement. Note: In actual
RCCB, the cutthroat contacts
function is replaced by
electronic control of coil on
time.
RCCB Operation As A Relay
To examine the RCCB operation
as a relay, refer to Figure 3 and
4. The device is shown in the
set position in Figure 3 and in
the tripped position in Figure 4.
The circuit path is from L2,
through the bimetal to one of
the stationary contacts. L1 is
connected directly to the other
stationary contact.
The movable bridge closes the
circuit by bridging between the
two stationary contacts.
As can be seen, movement of
the armature about its fulcrum
will determine the position of
the contacts. When coil S1-S
2 has been energized such
that the armature seals on the
left-hand pole face (Figure 3),
the mechanical linkage system
closes the contacts. Conversely,
when coil T1-T 2 has been
energized, such that the
armature seals on the right-
hand pole face (Figure 4), the
relay contacts will open due
to the spring forces exerted by
compression spring K.
Note: there is an "upward force" directed on the lever L through the linkage tying into the armature
at point D. During operation as a relay, point C (interface between lever L and latch bar I) is "fixed"
in place, and the lever L actually rotates about point C when moving the contact structure from the
opening to the closed, and from the closed to the open position.
BI-METAL
E-PIVOT
H-LATCH
G-PIVOT
LOAD-L2 LOAD-L1
K
B
D
S
N
A
S2 U1
S1 U2
M
N
J
T2
T1
V1
V1
L-LEVER
ARMATURE
PERMANENT MAGNET
STATIONARY
CONTACTS
I
LATCH
BAR
BUCKING
COIL
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
BUCKING
COIL
SET
(CLOSED)
COIL
BI-METAL
E-PIVOT
H-LATCH
G-PIVOT
LOAD-L2
LOAD-L1
K
B
D
S
N
A
S2 U1
S1 U2
M
C
C
N
J
T2
T1
V1
V1
L-LEVER
ARMATURE
PERMANENT MAGNET
STATIONARY
CONTACTS
I
LATCH
BAR
BUCKING
COIL
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
BUCKING
COIL
SET
(CLOSED)
COIL
E-PIVOT
H-LATCH
G-PIVOT
BI-METAL
LOAD-L2
LINE-L1
B
K
D
S
N
A
S1 S2
N
M
ARMATURE
J
T2
T1
PERMANENT MAGNET
STATIONARY
CONTACTS
L-LEVER
I
LATCH
BAR
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
SET
(CLOSED)
COIL
Figure 3
BI-METAL
E-PIVOT
H-LATCH
G-PIVOT
LOAD-L2 LOAD-L1
K
B
D
S
N
A
S2 U1
S1 U2
M
N
J
T2
T1
V1
V1
L-LEVER
ARMATURE
PERMANENT MAGNET
STATIONARY
CONTACTS
I
LATCH
BAR
BUCKING
COIL
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
BUCKING
COIL
SET
(CLOSED)
COIL
BI-METAL
E-PIVOT
H-LATCH
G-PIVOT
LOAD-L2
LOAD-L1
K
B
D
S
N
A
S2 U1
S1 U2
M
C
C
N
J
T2
T1
V1
V1
L-LEVER
ARMATURE
PERMANENT MAGNET
STATIONARY
CONTACTS
I
LATCH
BAR
BUCKING
COIL
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
BUCKING
COIL
SET
(CLOSED)
COIL
E-PIVOT
H-LATCH
G-PIVOT
BI-METAL
LOAD-L2
LINE-L1
B
K
D
S
N
A
S1 S2
N
M
ARMATURE
J
T2
T1
PERMANENT MAGNET
STATIONARY
CONTACTS
L-LEVER
I
LATCH
BAR
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
SET
(CLOSED)
COIL
Figure 4
BI-METAL
E-PIVOT
H-LATCH
G-PIVOT
LOAD-L2 LOAD-L1
K
B
D
S
N
A
S2 U1
S1 U2
M
N
J
T2
T1
V1
V1
L-LEVER
ARMATURE
PERMANENT MAGNET
STATIONARY
CONTACTS
I
LATCH
BAR
BUCKING
COIL
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
BUCKING
COIL
SET
(CLOSED)
COIL
BI-METAL
E-PIVOT
H-LATCH
G-PIVOT
LOAD-L2
LOAD-L1
K
B
D
S
N
A
S2 U1
S1 U2
M
C
C
N
J
T2
T1
V1
V1
L-LEVER
ARMATURE
PERMANENT MAGNET
STATIONARY
CONTACTS
I
LATCH
BAR
BUCKING
COIL
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
BUCKING
COIL
SET
(CLOSED)
COIL
E-PIVOT
H-LATCH
G-PIVOT
BI-METAL
LOAD-L2
LINE-L1
B
K
D
S
N
A
S1 S2
N
M
ARMATURE
J
T2
T1
PERMANENT MAGNET
STATIONARY
CONTACTS
L-LEVER
I
LATCH
BAR
MOVEABLE
CONTACT
BRIDGE
TRIP
(OPEN)
COIL
SET
(CLOSED)
COIL
Figure 5
LABINAL POWER SYSTEMS TF300-9E 1716 LABINAL POWER SYSTEMS TF300-9E
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB) — DESIGN CONCEPT
Note that the coil U1-U2 is
connected in parallel with T1-T2.
It is wound on the left-hand
core of the electro-magnet such
that when energized along with
T1-T2, the force it generates will
be in a direction opposing the
latching force generated in that
core by the permanent magnet.
The utilization of a permanent
magnet and intermittent duty
coils, in conjunction with
cutthroat contacts, allows a
considerable reduction in copper
and iron from that normally
required in electro-magnets for
continuous duty operation.
RCCB Operation as a
Circuit Breaker
To examine the operation of
the device as a breaker, refer to
Figures 3, 4, and 5.
In Figure 3, the device is shown
in the closed contact position
(presumably) carrying rated
current. Should an overload
occur, currents greater than
rated currents now "flow"
through the device "entering"
through L2, passing through the
bimetal, through the connection
of the bimetal to one stationary
contact, through the bridging
moveable contact structure, to
the other stationary contact, and
"out" through L1.
Depending upon the size of the
overload, the bimetal will begin to
deflect as shown in Figure 5 until
the actuating end of the bimetal
engages latch H at point J.
Motion and force due to the
deflection of the bimetal moves
latch H such that it rotates in
a counter-clockwise direction
around its pivot point E.
When latch H has moved an
adequate distance, the upward
force of lever L, applied at point
C to latch bar I, will rotate latch
bar I counter-clockwise around
its pivot point G. This allows the
main lever L to rotate clockwise
around point D (where it is
engaged with the armature) due
to the "contact return" spring
(compression spring) force
K acting upon the moveable
contact bridge.
Note that when this overload
occurs, the armature is not
transferred to the "off" (tripped)
position, but instead remains
in the latched position normally
associated with the "on" (set)
position of the device.
To "reset" the device after the
fault or overload clears could
be readily accomplished by
energizing the "trip" coil (T1-
T2) through a toggle or push-
button switch (see Figure 1)
located in the flight deck. The
armature would then transfer
and seal on the right-hand core
of the electro-magnet, which
is the "open" position shown in
Figure 4. At that time, springs
M and N (tension springs)
would reposition latch bar I and
latch H to the position shown
in Figure 4, providing that
the bimetal has now cooled
sufficiently and returned to
its original position as shown
in Figure 4. At this stage,
the RCCB is still in an "open
position" i.e. (the contacts are
open), but as outlined above,
the fault or overload has been
cleared through action and
operation of the device through
bimetallic activity, i.e. "Circuit
Breaker" operation.
To re-close the contacts, it is
now only necessary to energize
coils S1-S2 and re-establish a
mechanism position similar to
that shown in Figure 3. If the
fault of overload condition is still
in existence, the device would
again trip through bimetallic
activity as just described.
2.5 MILLISECONDS
1.0 RECTIFIED A
C
2Ø RECTIFIED AC
APPROXIMATELY
0.4 MILLISECONDS OFF TIME
1Ø AC
2Ø AC
ØB
ØB
ØC
1.25 MILLISECONDS OFF TIME
Figure 6
LABINAL POWER SYSTEMS TF300-9E 1918 LABINAL POWER SYSTEMS TF300-9E
Three Pole RCCB
The design principles employed
in the 3-pole RCCB have
followed many of the same
paths utilized in the 1-pole
RCCB. Differences other
than the obvious, such as
size, weight, shape, etc., are
explained below.
Motor Operation
The principles of motor
operation and construction
of the three pole devices are
similar to those employed in the
single pole RCCB. In the 3-pole
device, the AC operating power
is drawn from two of the three
phases. The "off" time between
current pulses during coil
energization is approximately
0.4 milliseconds. In comparison,
the "off" time for single-phase
power is approximately 1.25
milliseconds. See Figure 6.
The timing circuit establishes
a coil "on" time longer than
the actual transfer time of the
armature. The operation of the
3-pole RCCB is identical to the
1-pole.
Control Circuit
Refer to Figure 7. There is one
minor difference in operating
principles and parameters from
the single pole devices.
The difference is the addition
of a power junction area in the
electronics. (see Figure 7).
The 3-pole RCCB is designed for
use in 3-phase circuits and is a
400 Hz AC load controller. The
power junction is designed to
use AC power only. DC operate
(coil) power may be used even
though AC loads are to be
controlled. This connection is
made at terminal 4 of the IWTS
connector. In Figure 7, two
separate power junctions are
shown: one for AC and one for
DC. In the event both AC and
DC are connected to the RCCB,
only AC would be utilized by the
logic circuit. Should AC power
be lost, the DC connection
would automatically take over
the control function.
The other differences between
1-phase and 3-phase control
circuitry, i.e. timer addition, is
directly related as described
in the above Motor Operation
section.
LINE POWER
115 V 400 Hz
1/CU
(1/2 AMP C.B.)
SET
SWITCH
(FET)
EMERGENCY
(BACK-UP)
POWER
28Vdc
TRIP
SWITCH
(FET)
LOGIC
POWER
SUPPLY
POWER
JUNCTION TRIP COIL
LOGIC
TIMER
DC
ØB
ØC
Set Coil
Figure 7
*Indicates In 3 Phase Electronics
*
REMOTE CONTROLLED CIRCUIT BREAKER (RCCB) — DESIGN CONCEPT
LABINAL POWER SYSTEMS TF300-9E 1918 LABINAL POWER SYSTEMS TF300-9E
REMOTE POWER CONTROLLERS — WITH ELECTRONIC CURRENT SENSING
OVERLOAD DATA
% Rated
Current
100%
125%
200%
400%
Trip in Seconds
-55°C to +85°C
No Trip
45 Sec. Trip
0.22 Sec. Trip
0.095 Sec. Trip
Electronic Current Sensing
The electronic over current
sensing of these devices offer
several advantages over the
bi-metal sensing RCCB. Trip
current levels can be closely
controlled, for better protection
of sensitive loads, trip times are
faster, and both can be custom-
ized for specific applications.
Other advantages included less
heat buildup, and higher current
capabilities in the same small
package.
Use as a Relay, Circuit
Breaker, Or Both
RPCs, like RCCBs, combine the
best attributes of a circuit break-
er and a relay. Automatically
protects the wires and the load
device during circuit/load break-
down, but allows the flight deck
control of the load during nor-
mal operation.
Weight and Cost Savings
In distributed-load applications,
RPCs are a more efficient power
distribution solution promoting
cost and weight savings through
the elimination of long runs of
heavy cables associated with
the conventional relay - flight
deck circuit protector method.
Control of the RPC requires only
one #22 AWG control wire from
the ICU (model #1500-053-05)
on the flight deck to the RPC.
Single Pole
• 28 VDC
ORDERING INFORMATION
AMPERE
RATING
125
150
175
200
Labinal Power
Systems P/N
SM600BA125A1
SM600BA150A1
SM600BA175A1
SM600BA200A1
Single Pole Single Throw (Double Break Contacts)
Rated Contact Load (Amperes)
28 VDC
Res.
125
150
175
200
Ind.
125
150
150
150
Motor
125
150
175
175
Min.
5
5
5
5
Notes:
• One auxiliary contact included on each unit
• Contact Business Unit on Alternate Amperages, Trip Times, Control Configurations, Grounding, Auxiliary Switches, Mounting Systems, etc.
PERFORMANCE DATA
Rupture Levels 2500 A (28VDC)
Endurance (Resistive) 50,000 Cycles
Endurance (Inductive and Motor) 25,000 cycles
Endurance (Lamp) No Rating
Mechanical Life 100,000 cycles
Dielectric Strength Sea Level - VRMS .2-3 seconds: Coil to Case - 1250 initial. 1,000
After Life, All other Points 1,800 Initial, 1350 After Life
50,000 ft - VRMS 1 Minute: Coil to Case 500 Initial & After Life.
All other Points 700 Initial & After Life
Insulation Resistance 1100 Megaohms initial, 50 Megohms after Life, MIL-STD-202,
method 302, test condition B
Thermal Temperature Range -55°C to 85°C (-67°F to 185°F).
Vibration Sinusoidal 5 to 10 Hz: 0.08 DA; 10 TO 55 Hz: 0.06 DA; 55 to 2000
Hz: 10G's
Shock 50G's. (1/2 sine, 10-12 ms)
Altitude 50,000 ft. Maximum
EMI Requirements MIL-STD-461, Requirements CS114 and RE102 over the frequency
range of 14 kHz to 400 MHz and RE102 limits for Aircraft and
Space Systems
Moisture Resistance MIL-STD-202, method 106
Salt Spray Resistance MIL-STD-202, method 101, Condition B
Sand and Dust Resistance MIL-STD-202, method 110, Condition A
Fungus Resistance MIL-HDBK-454, Guideline 4
Explosion Proof MIL-STD-202, method 109
Weight (Standard) 425.017 grams (0.937 lbs.)
LABINAL POWER SYSTEMS TF300-9E 2120 LABINAL POWER SYSTEMS TF300-9E
REMOTE POWER CONTROLLER (RPC)
Engineering Data
Typical Wiring Diagram
Approximate Dimensions
A2 A1
3 A2 A2 A2
LOAD LINE
28 VDC
Back Up
Power
To Indicator /
Control Unit Circuit
Breaker Type
MS22073 - 1/2 Or
MS26574 - 1/2
S2
S3 S1
A1
A2
Auxiliary
Contacts
Over Current Detector
5A 5B
3
4
5A 3
5B S3 S2 S1
4
Module: Integrated wire termination. Terminals
will accept PIN contact per M39029/1 - 101. Use
insertion/extraction tool M81969/14 - 02.
COIL OPERATE CURRENT/SET AND TRIP TIME
Nominal
System
Voltage
28 VDC
(18 volts
Min)
I/C Set
Current @
Nom. Voltage
(milliamp)
2
Set Coil
Current
@Nom
Voltage
Pulse
3.7 Amp
Nominal
Voltage @
Room Temp
20 Millisec
MAX. Set Time
Most Adverse
Condition-Min.
Voltage 71°C
Ambient
35 Millisec
*I/CU. Trip Current Nominal
71°C and
Nominal
Voltage
1.76 Amp
-54°C and
Nominal
Voltage
1.25 Amp
Room Temp
and Nominal
Voltage
1.89 Amp
Max.
Standby
Current
(milliamp)
30
* MAX I/CU. LINE IMPEDANCE 7.5 Ohms CURRENT DECREASES W/TIME SO THAT I2t >= 2
Typical
Placement
of Rating
on Top
Plane
LOAD A2
LINE A1
125
.172/4.37 DIA.
2 MTG. HOLES
.688/
17.48
2.940
74.68
3.250
82.55
Position Indicator
Red: Closed
Green: Open
1.530
38.86
2.250
57.15
.350
8.89
.07
1.778
.05/1.27
.180
4.57
3.42
86.87
Name
Plate
R.06
1.52
4.26
108.20
.056
1.42
.42
10.67
1.200
30.48
Integrated
Wire Module
.256/6.50
.150
3.81
Barrier Black
Nylon Per
MIL-M-
20693A Type
I. General
Purpose
Terminal
Pad .6 DIA.
Approximate Dimensions - 1 Pole
LABINAL POWER SYSTEMS TF300-9E 2120 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — GASKET SEALED - 100 AMPS TO 1,000 AMPS
Typical Characteristics
Specifications
• Design to meet the general
requirements of MIL-R-6106
Type II continuous Duty
Unsealed
• Contacts are covered & gasketed
• Double break contacts
• All units are thermal breaker
compatible at rated relay
resistive load
• Some models available with
auxiliary circuits
• Gold-plated auxiliary contacts
for low-level applications
available
• Auxiliary contacts ratings:
28 Vdc: 5 amps resistive
3 amps inductive
2.5 amps lamp
Ratings Per MIL-R-6106:
• Salt spray, humidity,
accelera tion, sand & dust,
intermediate current
• Vibration:
5 to 10 Hz -.08 DA
10 to 55 Hz -.05 DA
55 to 500 Hz -2.0 g's
• Shock: 25 g's (6-9 MS ½ sine
wave)
• Life: (-55 to 71°C)
50,000 cycles electrical at
full rated load
100,000 cycles mechanical
tested at 25% rated load
• Altitude: 50,000 feet
Typical Characteristics
(Figures 1 through 8)
(For additional details, con-
tact your local Labinal Power
Systems Technical Sales
Representative)
• Power Contact Voltage Drop:
Initial 0.15 V After Life Test:
0.175 V
• Insulation Resistance: Initial
200 Meg ohm.
• After Life Test: 100 Meg ohm
Dielectric Withstanding Voltage:
2.5 Seconds Sea Level
Initial: 1250 V
After Life Test: 1000 V
Power Contacts: 650 V
50,000 Feet 60 Seconds
Initial & After Life Test: 500 V
Circuit Diagrams
A
1A2
#1
X1
X2
#2
X1
X2
A1
13
12
11
A2
23
22
21
A
2
#3
X1
X2
B1
A1
12
11
11
A
2
23
22
21
A
1A2
#1
X1
X2
#2
X1
X2
A1
13
12
11
A2
23
22
21
A
2
#3
X1
X2
B1
A1
12
11
11
A
2
23
22
21
#1
#2 #3
Part Number Rated Contact Load Rupture
Current
Contact Rating
28 Vdc Intermittent Power
28 Vdc
Res. Ind. Motor Intermediate 15
Minute
5
Minute
1
Minute
Max.o
Inrush
SM100D2
SM100D3
SM150D1
SM150D2
SM150D3
SM150D4
SM150D5l
SM200D1
SM200D2
SM200D3
SM400D1
SM400D2
SM400D3
SM1000D11r
100
100
150n
150n
150n
150n
150
200
200
200
400
400
400
1000
80
80
50
50
50
50
50
100
100
100
100
100
100
—
100
100
150
150
150
150
150
200
200
200
400
400
400
—
4
4
15
15
15
15
15
20
20
20
40
40
40
50
1000
1000
1200
1200
1200
1200
1200
2000
2000
2000
4000
4000
4000
6000
130
130
195
195
195
195
195
260
260
260
520
520
520
1200
150
150
225
225
225
225
225
300
300
300
600
600
600
1500
200
200
300
300
300
300
300
400
400
400
800
800
800
2000
600
600
900
900
900
900
900
1200
1200
1200
2400
2400
2400
2500s
600 Amp make, 200 Amp break
kDuty cycle: 1 minute on, 1 minute off; 1 minute on, 20 minutes off
lMaximum vibration 2000 Hz 2 g’s
mDuty cycle: 1.5 minutes on, 3 minutes off
nWill carry 200 Amps at 20% on duty cycle per minute
oMaximum inrush provided coil voltage as noted is maintained
pOperate time at 28 Vdc & 25 deg. C.
qContact bounce is average of 5 conse cutive ratings.
rAvailable in normal closed circuit.
s 1 sec. on, 60 sec. off
LABINAL POWER SYSTEMS TF300-9E 2322 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — GASKET SEALED - 100 AMPS TO 1,000 AMPS
Insulation Resistance:
Initial: 100 Meg ohms
After Life Test: 50 Meg ohms
Dielectric Withstanding Voltage:
(2.5 Seconds Sea Level)
Initial: 1250 V
After Life Test: 1000 V
Dimensions (See next page for other dimension figures)
Figure 9
Life at 1000 Amps limited to 10,000 cycles. Life at 50 Amps is 50,000 cycles minimum. Rupture life is 20 cycles at 6000 Amps. This unit is available with inverted termi-
nals, bottom mounting, available with normally closed power contacts, and DPDT auxiliary circuits.
Unit Shown Without Auxiliary Contacts
Contact Transfer
Milliseconds, Max.
Coil Data
Op.o
Time
Rel.
Time
Contact
BounceqPoles
& Throw
Weight
Lbs./gm
Circuit
Dia.
Dimension
Fig.
Res.
(OHMS)
Max.
Volts
Pick
Up
Max
Volts-
Drop
Out
Duty
Cycle
Mounting Auxiliary
Termination
Part
Number
35
35
40
40
15
15
40
25
25
25
40
40
20
60
15
15
15
15
12
12
15
10
10
18
15
15
15
30
6
6
5
5
5
5
5
2.5
2.5
5
10
10
10
3
SPST/NO
SPST/NO
SPST/NO
SPST/NO
SPDT
SPDT
SPDT
SPST/NO
SPST/NO
SPST/NO
SPST/NO
SPST/NO
SPST/NO
SPST/NO
0.6/272
0.6/272
0.95/430
0.95/430
1.25/567
1.25/567
1.25/567
1.3/588
1.3/588
1.3/588
2.6/1177
2.6/1177
2.6/1177
4/1810
1
1
2
2
3
3
3
2
2
2
2
2
2
1
1
2
3
3
4
4
4
5
6
6
7
8
8
9
94.2
94.2
82.7
82.7
6.6
6.6
60
66
66
10
60
60
10
38
18
18
16.5
16.5
6.5
6.5
18
18
18
7. 5
18
18
7. 0
18
7 to 1.5
7 to 1.5
1 to 7
1 to 7
0.2 to 3
0.2 to 3
0.6 to 8.5
1.5 to 7
1.5 to 7
0.5 to 3
1.5 to 7
1.5 to 7
0.5 to 3
1 to 7
Cont
Cont
Cont
Cont
Interk
Interk
Cont
Cont
Cont
Interm
Cont
Cont
Interm
Cont
Side
Top
B
B
B
B
B
Side
B
B
Side
B
B
Side
—
—
Screw
IWTS
Screw
IWTS
Screw
Lug
Lug
Lug
Lug
Lug
Lug
—
SM100D2
SM100D3
SM150D1
SM150D2
SM150D3
SM150D4
SM150D5
SM200D1
SM200D2
SM200D3
SM400D1
SM400D2
SM400D3
SM1000D11
600 Amp make, 200 Amp break
kDuty cycle: 1 minute on, 1 minute off; 1 minute on, 20 minutes off
lMaximum vibration 2000 Hz 2 g’s
mDuty cycle: 1.5 minutes on, 3 minutes off
nWill carry 200 Amps at 20% on duty cycle per minute
oMaximum inrush provided coil voltage as noted is maintained
pOperate time at 28 Vdc & 25 deg. C.
qContact bounce is average of 5 consecutive ratings.
rAvailable in normal closed circuit.
LABINAL POWER SYSTEMS TF300-9E 2322 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — GASKET SEALED - 100 AMPS TO 1,000 AMPS
Dimension Figures
Figure 1 Figure 2
Figure 3 Figure 4
X1 X2
1.875
(47.62)
2.385
(60.55)
.937
(23.8)
.219 (5.56) DIA.
(2) MOUNTING
HOLES
.422
(10,7)
2.68
(68.0)
#6-32 UNC-2A
2 COIL TERM
1.72
(43.69)
.986
(25.0)
.625
(15.87)
2.22
(56.38)
2.75
(69.85)
.250
(6.35)-28 UNF-3A
2 Power Term
SM100D2 SM100D3
SM150D4
Unit Shown Without Auxiliary Contacts
2.64
(67)
.219
(5.56) DIA.
MOUNTING
HOLES
1.312
(33.3)
2.68
(68)
2.22
(56.3)
2.188
(55.5)
.250
(6.35)-28 UNF-3A
2 POWER TERM
.625
(15.8)
2.68
(68)
1.72
(43.6)
X2 X1
SM150D1
SM150D2
SM150D3
SM150D5
SM150D4
SM150D2
Unit Shown Without Auxiliary Contacts
X2X1
A2A1
WILL ACCEPT TERMINAL-PIN
CONNECTION (DEUTSCH PA
RT
NO. 1841-1-5620)
.203 (5.15) ± .005 DIA.
4 MOUNTING HOLES
2.75
(69.8)
187 MTG
(47.5)
2.19
(55.6)
1.87 MTG
(47.5)
4.50
(114.3)
2.25
(57.1)
2.25
(57.1)
#6-32 UNC-2A
6 AUX. TERMINALS
#6-32 UNC-2A
2 COIL TERMINALS
.75
(19)
.250 (6.35)-28 UNF-2A
2 POWER TERMINALS
X2X1
B2
B3
A2A1
.250 (6.35)-28 UNF-2A
4 POWER TERMINALS
WILL EXCEPT TERMINAL-PIN
CONNECTION (DEUTSCH PART
NO 1841-1-5620)
.203 (5.15) ± .005 DIA.
4 MOUNTING HOLES
2.75
(69.8)
187 MTG
(47.5)
2.19
(55.6)
1.87 MTG
(47.5)
4.50
(114.3)
2.25
(57.1)
2.25
(57.1)
#6-32 UNC-2A
6 AUX. TERMINALS
#6-32 UNC-2A
2 COIL TERMINALS
.75
(19)
.75
(19)
LABINAL POWER SYSTEMS TF300-9E 2524 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — GASKET SEALED - 100 AMPS TO 1,000 AMPS
Dimension Figures
Figure 5 Figure 6
Figure 7 Figure 8
SM200D1
SM400D1
SM200D2
SM200D3
SM400D2
SM400D3
2.00
(50.8) .916
(23)
.984
(25)
3.85
(97.8)
.266 2 MTG. HOLES
(6.75)
.781
(19.8)
X2
X1
A2
A1
4.00
(101.6) 2.395
(60.8)
3.5
(68.9) 4.500
(76)
.375 (9.5)- UNF-2A
#6-32 UNC-2A
COIL TERMINALS
.058 (1.47) DIA. TERMINALS
TO FIT "AMP" LUG PT.
NO. 61276-2
.058 (1.47) DIA.
TERMINALS TO FIT
"AMP" LUG PT 61276-2
4.38 MAX
(61.93)
4.31
(109.47)
1.05
(26.67)
TYP.
5.50
(139.70)
1.06
(26.9)
3.92
(99.57)
1.28
(32)
MAX
.81
(20.57)
2.406
(61.11)
.500 (12.7)-20 UNF-2A
POWER TERMINAL
#6-32 UNC-2A
COIL TERMINAL
.266 (6.76) DIA.
2 HOLES FOR MTG
MAX.
A2A1
X1 X2
.058 DIA. TERMINALS
TO FIT "AMP" LUG
PT 61276-2
1.219
MAX.
.266
(6.76)
2 HOLES FOR
MOUNTING
3.25
(82.55)
3.000
(76.20) 3.53
(89.66)
MAX.
1.89
(48.01)
1.000
±.125
.475
.500
MIN.
5.500
(139.70)MAX.
.062
(1.575)
4.45
(113.03)
MAX.
2.438
MAX.
4.312
(109.47)
2.25
(57.15)
A2
X2 X1
A1
2 X STUD, THD .138-32 UNC-2A
2 X STUD, THD .500-20 UNF-2A
POWER TERMINAL
.058 DIA. TERMINALS
TO FIT “AMP” LUG
PT 61276-2
1.219 MAX.
.266
(6.76)
2 HOLES FOR
MOUNTING
3.25
(82.55)
3.000
(76.20) 3.65
(92.7)
MAX.
1.89
(48.01)
±.125
(1.13)
.475
.500 MIN.
5.500
(139.70) MAX.
.062
(1.575)
4.45
(113.03)
MAX.
2.438 MAX.
4.312
(109.47)
2.25
(57.15)
A2
X2 X1
A1
2 X STUD, THD .138-32 UNC-2A
2 X STUD, THD .500-20
UNF-2A
POWER TERMINAL
LABINAL POWER SYSTEMS TF300-9E 2524 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — CONTINUOUS DUTY, TYPE II, UNSEALED
INTERMITTENT DUTY, TYPE III, UNSEALED
General Specifications
• Designed to MIL-R-6106
- Type II Unsealed Continuous Duty
- Type III Unsealed Intermittent Duty
- Covered/Gasketed Contact Area
- Twin-break Silver Alloy Contacts
• Meets Explosion, Humidit, Salt, Spray, Sand, and Dust requirements.
• Altitude: 50,000 feet
• Shock: 25 g's ½ Sine 6 to 9 milliseconds
- Maximum contact opening: 2 milliseconds
• Acceleration: 10 g's
• Vibration Limits:
- 5 to 10 Hz: 0.8 in DA
- 10 to 55 Hz: 0.6 in DA
- 55 to 2000 Hz: 2 g's
• Temperature Range: -55°C to 71°C
• Insulation Resistance:
- 100 megohm minimum initially
- 50 megohm minimum after tests
• Dielectric:
- 1250 Vac minimum initially
- 1000 Vac minimum after tests
• Life:
- Electrical Operations: 50,000 cycles
- Mechanical Operations at 25% of Rated Resistive Load:
100,000 cycles
• Minimum Current: 10% of Rated DC Resistive Load
• Intermittent Duty Ratings:
- % of Rated Resistive
- Time On in Minutes
- Cooling time is required between successive over load applications.
Intermittent Duty Ratings
• Options:
- Other Coil Voltage
- Alternate Mountings
• MIL-STD-461 applies to AC operated coils.
• See drawing for additional applicable details.
Cat N. 6041H217
• SPST rated 400 Amp
resistive and motor at 28 Vdc
continuous duty with top
mounting.
• MS24185-D1 - 2.6 Lbs/ 1179gm
Cat N. 6041H202
• SPST rated 200 Amp
resistive and motor at 28 Vdc
continuous duty with side
mounting.
• MS24171-D2 - 1.25 Lbs/ 567gm
Cat N. 6041H209
• 2 PST rated 100 Amp
resistive at 28 Vdc and
75 amperes 115/200 V
400 Hz intermittent duty with
top mounting.
• AN-3392-1 - 1.5 Lbs/ 680 gm
Cat N. 6041H201
• SPST rated 50 Amp resistive,
inductive and motor at 28 Vdc
continuous duty with side
mounting.
• MS24166-D2 - 0.5 Lbs/ 225 gm
Cat N. 9565H2
• 3 PST rated 25 Amp resistive,
inductive and motor at
28 Vdc and 115/200 V 400 Hz
continuous duty cycle with
base mounting.
• MS24192-D1 - 1.1 Lbs/ 499 gm
Cat N. 6046H39
• Control of split field series
motors.
• SPST see circuit diagram 6
for details.
• Rated 28 Vdc 50 Amp N.O.,
25 Amp N.C
• 2.9 Lbs./1315 gm
Minutes
15 5 1 Inrush
130% 150% 200% 600%
Rupture Time Per MIL-R-6106
(Coil Voltage must be maintained at rated value)
Special Service Use
Mechanical Interlock/Type Service
Part
Number
Reversing Transfer Dynamic
Braking
9565H29 X X —
6046H39 X — X
6046H46 X X —
6046H53 X X —
Reversing and Dynamic Braking Relay
LABINAL POWER SYSTEMS TF300-9E 2726 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — CONTINUOUS DUTY, TYPE II, UNSEALED
INTERMITTENT DUTY, TYPE III, UNSEALED
Labinal
Power Sys-
tems Part
Number
Government
Part
Number
Continuous Power Contacts, Ratings Contacts Operate
Milliseconds, Maximum
Coil Data
28VDC 115/200 VAC 400 Hz. Contact
Bounce
Poles &
ThrowmWeight
Lbs./GMS
Circuit
Dia./
Dim.
Figure
Resistance
(OHMS)±
10% Pickup/
Sealed
Volts
Pickupn
Volts
Drop-
outo
Duty
Cycle
Mounting Coil
Voltage
Nominal
RES. IND. MOTOR RES. IND. MOTOR O P.
TIME
REL
TIME
9565H2
9565H29
9565H95
6041H53k
6041H220k
6041H230
6046H39k
6041H201
6041H149
6041H200
9565H94
6041H219
6041H80
6041H144
6041H11
6041H209
6046H53
9565H13
6041H202
6041H105
6041H123
6041H203
6041H212
6041H215
6041H216
6046H46
6041H205
6041H217
6041H218
6041H206
MS24192-D2
MS24152-D1
—
—
MS24187-D1
MS24187-D2
—
MS24166-D2
—
MS24166-D1
MS24193-D1
MS24178-D1
—
—
—
AN3362-1
MS25031-D1B
—
MS24171-D2
—
—
MS24172-D2
—
MS24171-D1
MS24172-D1
MS25032-D1
MS24185-D2
MS24185-D1
MS24179-D1
MS24179-D2
25
25
25
50/25
50/25
50/25
50/25
50
50
50
50
55
100
100
100
100
100
100
200
200
200
200
200
200
200
200
400
400
400
400
25
25
25
50/25
50/25
50/25
50/25
50
50
50
50
40
80
80
80
80
80
75
100
100
100
100
100
100
100
100
100
100
100
100
25
25
25
50/25
50/25
50/25
50/25
50
50
50
50
40
80
80
80
80
80
75
200
200
200
200
200
200
200
150
400
400
400
400
25
25
25
25/25
25/25
25/25
—
—
—
—
50
55
—
—
—
75
75
100
—
—
—
—
—
—
—
150
—
—
—
—
25
25
25
—
—
—
—
—
—
—
50
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
25
25
25
—
—
—
—
—
—
—
50
35
—
—
—
65
65
75
—
—
—
—
—
—
—
100
—
—
—
—
20
20
20
20
20
20
—
20
20
20
20
—
35
22
25
—
40
25
40
25
25
40
40
40
20
20
15
15
15
15
15
15
—
10
15
10
15
—
10
15
10
—
15
18
15
10
10
15
15
15
15
15
6
6
6
5 N.O./10
N.C.
5 N.O./10
N.C.
5 N.O./10
N.C.
—
5
5
5
4
—
3.5
4
50
—
5
5
5
5
5
5
5
5
5
5
3PST
3PDT
3PST
SPDT
SPDT
SPDT
SPDT
SPST
SPST
SPST
3PST
DPST
SPST
SPST
SPST
DPST
DPDT
3PST
SPST
SPST
SPST
SPST
SPST
SPST
SPST
DPDT
SPST
SPST
SPST
SPST
1.1/498
2/909.09
1.06/482.95
.54/245.45
.54/245.45
.54/245.45
2.9/1318.18
.50/225
.56/254.55
.50/225
1.51/685
.75/340.91
1.4/636.36
1.4/636.36
1.4/636.36
1.5/685
3.5/1590.91
2.5/1136.36
1.25/568.18
1.25/868.18
1.3/590.91
1.23/560
1.3/590.91
1.33/604.55
1.33/604.55
5.5/2500.00
2.6/1181.82
2.6/1181.82
2.6/1181.82
2.6/1181.82
10 / 11
16 / 11
10 / 11
4 / 2
4 / 2
4 /2
6 / 7
1 / 4
1 / 4
1 / 4
10 / 11
2 / 2
1 / 3
1 / 3
1 / 1
2 / 2
9 / 7
12 / 11
1 / 5
1 / 5
1 / 5
1 / 5
1 / 5
1 / 1
1 / 1
8 / 7
1 / 5
1 / 1
1 / 1
1 / 5
/ 60
22 / 92
/ 1160
16.9
94.2
94.2
26
94.2
16.9
94.2
13.5 / 71.5
66
66.3
66.3
66.3
43
43
9 / 53
66
10 (+15/-10)
66
10 (+15/-10)
66
66
10(+15/-10)
41
60
60
10
10
18
18
70
8.2
18
18
18
18
8.2
18
18
18
18
18
18
20
18
18
18
9
18
7. 5
18
18
7. 5
18
18
18
7
7
1.5 to 7
1.5 to 7
8 to 38
0.8 to 4.8
1.5 to 9
1.5 to 9
7
1.5 to 7
0.8 to 4.8
1.5 to 7
1.5 to 7
1.5 to 7
1.5 to 7
1.5 to 7
1.5 to 7
1.5 to 7
1.5 to 7
1.5 to 7
1.5 to 7
3.5
1.5 to 7
0.5 to 3.0
1.5 to 7
1.5 to 7
0.5 to 3.0
1.5 to 7
1.5 to 7
1.5 to 7
0.5 to 3.0
0.5 to 3.0
CONT
CONT
CONT
CONT
CONT
CONT
CONT
CONT
CONT
CONT
Note
CONT
CONT
CONT
Note
CONT
CONT
CONT
CONT
CONT
INTERl
CONT
CONT
INTERl
CONT
CONT
CONT
INTERl
INTERl
BASE
BASE
BASE
TOP
TOP
TOP
TOP
SIDE
SIDE
TOP
BASE
TOP
SIDE
SIDE
TOP
TOP
TOP
BASE
SIDE
SIDE
SIDE
SIDE
SIDE
TOP
TOP
TOP
SIDE
TOP
TOP
SIDE
28 dc
28 dc
120 dc
12 dc
28 dc
29 dc
28 dc
28 dc
12 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
12 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
28 dc
MS Part Number Summary
AN3362-1* 6041H209 MS24179-D1 6041H218
MS24152-D1* 9565H29* MS24185-D2 6041H205
MS24166-D1 6041H200 MS24187-D1 6041H220
MS24166-D2 6041H201 MS24187-D2 6041H230
MS24171-D1 6041H215 MS24192-D1 9565H2
MS24171-D2 6041H202 MS24193-D1 9565H94
MS24172-D1 6041H216 MS25031-D1B 6046H53
MS24172-D2 6041H203 MS24185-D1 6041H217
MS24178-D1 6041H219 MS25032-1 6046H46
*Inactive for new design
Conversion Part Number
AN Part Number Use MS Part Number Labinal Power Syste-
ms Part Number
3343-1 — 9565H13
3350-1 MS24166-D2 6041H201
3362-1 — 6041H209
3370-1 MS24171-D2 6041H202
3371-1 MS24172-D2 6041H203
3380-1 MS24185-D2 6041H205
— MS25030-D1B 6041H51
3381-2 MS24179-D1 6041H218
Coil will exceed 95° C temperature rise when left on continuously in 25°
ambient, but will not be damaged. At maximum ambient temperture of 71°C,
the duty cycle should be limited to 15 minutes “on” time per half hour to
obtain maximum coil life.
k Continuous and intermittent duty ratings shown are for N.O. pole rated at 1/2
the listed continuous DC duty ratings. N.C. pole on 6041H53 and H220 limited
to 15 g’s shock.
l Time on 1 1/2 minutes at 29 Vdc. Minimum time off is 3 minutes.
m All continuous duty resistive and motor load ratings and all intermittent duty
ratings for all 3 pole relays listed under 28 Vdc apply for 120 Vdc systems with
all 3 poles of the relay connected in the series.
n Pick-up voltage below values shown may cause relay to rapidly cycle on and off
(chatter).
o Relay must drop-out at voltage value or less and may drop-out at any voltage
below the higher voltage noted.
LABINAL POWER SYSTEMS TF300-9E 2726 LABINAL POWER SYSTEMS TF300-9E
Dimensions in Inches Dimensions
in
Millimeters
Dimensions in Millimeters
Catalog
Number
Ampere
Ratings
Figure
Number
Wide
A
High
B
Deep
C
Mounting Hole F Net Stud G
Power
Coil Weight Lbs. Wide
A
High B Deep Mounting Hole
F
Weight
Grams
D E C D E
6041H11
6041H53
6041H80
6041H105
6041H123
6041H144
6041H149
6041H200
6041H201
6041H202
6041H203
6041H205
6041H206
6041H209
6041H212
6041H215
6041H216
6041H217
6041H218
6041H219
6041H220
6046H39
6046H46
6046H53
9565H2
9565H13
9565H29
9565H94
9565H95
100
50/25
100
200
200
100
50
50
50
200
200
400
400
100
200
200
200
400
400
55
50/25
50/25
200
100
25
100
25
50
25
1
2
3
5
6
3
4
2
4
5
5
5
5
2
5
1
1
1
1
2
2
7
7
7
11
11
12
11
11
3.27
2.63
2.91
4.406
4.5
3.33
2.75
2.75
2.75
4.41
4.5
5.5
5.5
3.469
4.48
4.406
4.406
5.5
5.5
2.922
2.812
4.82
7.688
6.688
3.063
3.812
4.75
3.625
3.063
3.13
3.14
3
3.28
3.575
3
2.5
2.625
2.5
3.28
3.313
3.92
3.92
3.406
3.313
3.75
3.75
4.5
4.5
2.844
3.13
3.45
4.125
3.75
2.75
3.546
2.75
3.188
2.75
2.08
2.062
2.08
1.99
2
2
2.125
2.125
2.125
1.99
2
2.438
2.438
2.656
2.466
2
2
2
2
2.031
2.062
2.25
3.468
2.656
2.75
3.28
4.125
3.312
2.75
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
1.395
2.01
1. 76
2.125
2.688
2.468
2.75
2.135
2.75
2.2
2.26
2.395
2.395
2.26
1.875
2.188
1.875
2.395
2.395
2.406
2.406
2.948
3.717
3.01
3.01
3.01
3.01
2.385
2.2
4.301
6.895
6.02
2.49
3.102
4.187
2.322
2.494
0.27
0.214
0.276
0.276
0.276
0.276
0.229
0.219
0.229
0.276
0.276
0.276
0.276
0.276
0.27
0.276
0.276
0.276
0.276
0.223
0.214
0.228
0.266
0.266
0.229
0.225
0.218
0.219
0.229
.250-28 UNF
.190-32 UNF-2A
.250-32 UNC
.375-24 UNF-2A
.375-24 UNF-2A
.250-28 UNF
.190-32 UNC-2A
.191-32 UNC-2A
.190-32 UNC-2A
.375-24 UNF-2A
.375-24 UNF-2A
.500-20 UNF-2A
.500-20 UNF-2A
.250-28 UNF-2B
.375-24 UNF-2A
.375-24 UNF-2A
.375-24 UNF-2A
.500-20 UNF-2A
.500-20 UNF-2A
.190-32 UNC-2B
.190-32 UNF-2A
.190-32
.375-24 UNF
.250-28 UNF
.190-32 UNF-2B
.250-28 UNF-2B
.190-32 UNF-2B
.190-32 UNF-2B
.190-32 UNF-2B
.138-32 UNC
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2B
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2A
.138-32 UNC-2B
.137-32 UNC-2A
.138-32 UNC
.138-32 UNC
.138-32 UNC
.138-32 UNC-2B
.164-32 UNC-2B
.164-32 UNC-2B
.164-32 UNC-2B
.164-32 UNC-2B
1. 4
0.54
1. 4
1.25
1. 3
1. 4
0.562
0.5
0.5
1.25
1.23
2.6
2.6
1. 5
1. 3
1.33
1.33
2.6
2.6
0.75
0.54
2.9
5.5
3.5
1.062
2.5
2.25
1. 5
1.06
83.06
66.8
73.91
111.92
112.01
84.58
69.85
69.85
69.85
112.01
114.3
139.7
139.7
88.11
113.79
111.91
111.91
139.7
139.7
74.22
71.42
122.43
195.28
169.88
77.8
96.82
120.65
92.08
77.8
79.5
79076
76.2
83.31
90.81
76.2
63.5
66.68
63.5
83.31
84.15
99.57
99.57
86.51
84.15
95.25
95.25
114.3
114.3
72.24
79.5
87.63
104.78
95.25
69.85
90.07
69.85
80.98
69.85
52.83
52.37
52.83
50.55
50.8
50.8
53.98
53.98
53.98
50.55
50.8
61.93
61.93
67.46
62.64
50.8
50.8
50.8
50.8
51.59
52.37
57.15
88.09
67.46
69.85
83.31
104.78
84.12
69.85
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
—
35.43
51.05
44.7
53.98
68.28
62.69
69.85
54.23
69.85
55.88
57.4
60.83
62.83
57.4
47.63
55.58
47.63
60.83
60.83
61.11
61.11
74.88
94.41
76.45
76.45
76.45
76.45
60.58
55.88
109.25
175.13
152.91
63.25
78.79
106.35
58.98
63.35
6.86
5.44
7. 0 1
7. 0 1
7. 0 1
7. 0 1
5.82
5.56
5.82
7. 0 1
7. 0 1
7. 0 1
7. 0 1
7. 0 1
6.86
7. 0 1
7. 0 1
7. 0 1
7. 0 1
5.66
5.44
5.79
6.76
6.76
5.82
5.72
5.54
5.56
5.82
636.36
245.45
636.36
568.18
590.91
636.36
255.68
225
225
568.18
560
1181.82
1181.82
681.82
590.91
604.55
604.55
1181.82
1181.82
340.91
245.45
1318.18
2500
1590.91
482.95
1136.36
1022.73
681.82
481.82
POWER RELAYS — CONTINUOUS DUTY, TYPE II, UNSEALED
INTERMITTENT DUTY, TYPE III, UNSEALED
Approximate Dimensions and Weights
Note: All coils and auxiliary terminals are 6-32, except for Catalog Number 9565 relays which have 8-32 coil terminals.
Dimensions are approximate and should not be used for construction purposes.
Dimension Figures
Figure 1 Figure 2
B
E
C
A
DIA. G
TERM.
STUD
DIA. F
MTG.
HOLES
A4
A4 A1 C
G. DIA.
TERM.
STUDS
F DIA
MTG. HOLES
A
A3
X2 X2
E
B
A4
A4 A1 C
G. DIA.
TERM.
STUDS
F DIA
MTG. HOLES
A
A3
X2 X2
E
B
LABINAL POWER SYSTEMS TF300-9E 2928 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — CONTINUOUS DUTY, TYPE II, UNSEALED
INTERMITTENT DUTY, TYPE III, UNSEALED
Dimension Figures (cont.)
Figure 3 Figure 4 Figure 5 Figure 6
Figure 7 Figure 11 Figure 12
A
C
X2
A2 A1
X1
E
F DIA.
MTG. HOLES
C DIA.
TERM.
STUDS
F
A
G DIA.
TERM.
STUDS
B
B
E
F DIA.
MTG.
HOLES
A
E
F DIA.
MTG.
HOLES
B
G DIA.
TERM.
STUDS
B
G DIA.
TERM.
STUDS
B
A
E
F DIA.
MTG.
HOLES
B
C
B
E
F DIA.
MTG.HOLES
G DIA.
TERM
STUDS
D
A
LABINAL POWER SYSTEMS TF300-9E 2928 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — CONTINUOUS DUTY, TYPE II, UNSEALED
INTERMITTENT DUTY, TYPE III, UNSEALED
Typical Wiring Diagrams
Diagram 1 Diagram 2 Diagram 3 Diagram 4
Diagram 8 Diagram 9 Diagram 10
Diagram 12 Diagram 16 Diagram 18
A
1A2
X1
X2
A1 A2
B1 B2
X1
X2
A1 A2
A3 A4
X1
X2
B1 B2
A1 A2
X1
X2
D1 D2
C1 C2
X3
X4
B1 B2
A1 A2
X1
X2
B4 A3
A4 A3
Y1
Y2
A1 A2
B1 B2
X1
X2
C1 C2
B1 B2
A1 A2
X1
X2
L1 T2
L1 T2
L1 T2
X1
X2
Y2
B1
A1
A2 B2 C2
C1
X2
X1
B3
A3
C3
Y1
X1
L2
L1
T1 T2 T3
L3
X2
X1
L12
L11
L13
X12
A
1A2
X1
X2
A1 A2
B1 B2
X1
X2
A1 A2
A3 A4
X1
X2
B1 B2
A1 A2
X1
X2
D1 D2
C1 C2
X3
X4
B1 B2
A1 A2
X1
X2
B4 A3
A4 A3
Y1
Y2
A1 A2
B1 B2
X1
X2
C1 C2
B1 B2
A1 A2
X1
X2
L1 T2
L1 T2
L1 T2
X1
X2
Y2
B1
A1
A2 B2 C2
C1
X2
X1
B3
A3
C3
Y1
X1
L2
L1
T1 T2 T3
L3
X2
X1
L12
L11
L13
X12
LABINAL POWER SYSTEMS TF300-9E 3130 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — CONTINUOUS DUTY, TYPE II, UNSEALED
INTERMITTENT DUTY, TYPE III, UNSEALED
Typical Operation:
All items shown within dotted lines are part of the relay. All other
parts external to dotted lines, including switches connected to C1 &
C2 customer supplied.
Internal Mechanical Interlocks
Prevents the opposite contacts from transferring when either one of
the coils is energized and the respective contacts are closed.
Reversing Operation
Closing either external start/stop switch at C1 or C2 will cause the
motor to turn in either direction.
Dynamic Braking Operation
Internal switch provides for dynamic braking current flow through
the motor shunt-fields series (SF) 1 and 2. Switch S is mechanically
closed when either coil is energized and maintains that position until
the alternate coil is energized. Switch S is shown in the last position
commanded by external start/stop switch at C1.
P/N 6046H39
L1+ L2-
C3
S.F.1
S.F.2
ARM
S
1
D
2
C1
3
4
C2
Dia. No. 6
6046H39 (Items shown outside dotted line
are customer supplied)
LABINAL POWER SYSTEMS TF300-9E 3130 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — HERMETICALLY SEALED - 12 AMPS TO 50 AMPS
Typical Configurations
Cat. No. 6042H285
3PST, 50 Amp w/Auxiliary
Cat. No. 6042H46
SPST, 50 Amp w/Auxiliary
Cat. No. 6042H155
SPST, 50 Amp
Characteristics:
• Electrical Life: 50,000 cycles
(sea level to 80,000 feet)
• Mechanical Life: 100,000 cycles
• Acceleration: 15 g's
• Shock: 25 g's
• Ambient Temperature Class:
- B -70°C to 125°C
- D -70°C to 71°C
• Hermetically sealed/ MIL-PRF-6106
• Twin Break Silver Alloy Main Contacts
• Vibration Levels (Typical):
5 - 10 CPS
.08 DA
10 - 55 CPS
.06 DA
55 - 200CPS
10 g’s
250 - 500 CPS
5 g’s
500 - 1500 CPS
3 g’s
Catalog
Number
Continuous
Ampere
Contact Rating
Poles
and
Throw
Operating Coil
Voltage
Number
Aux
Contacts
Dimension
Drawing
Figure
Number
Wiring
Diagram
Figure
Number
Government
Type Number
Temp Class/
Note
6042H110-2 12 3PST
28 Vdc
1 2 8 MS24143-D3 Bk
6042H141-2
6042H142-2
25 3PST
— 2 6 MS24143-D1 B
1 2 8 MS24143-D2 Bp
6042H290-2
6042H291-2
115 Vac
60 or
400 Hertz
Built In
Rectifiers
— 2 6 MS24143-A3 D
1 2 8 MS24143-A4 D
6042H155-2
50
SPST
28 Vdc
— 1 9 MS24140-D1 B
6042H156-2 1 1 10 MS24140-D2 B
6042H145-2
6042H146-2
3PST
— 2 6 MS24376-D1 B
1 2 8 MS24376-D2 B
6042H147-2
6042H148-2
6042H285-2
6042H288-2
115 Vac
60 or 400
Hertz
Built In
Rectifiers
— 2 6 MS24376-A1 Bs
1 2 8 MS24376-A2 Bs
1 2 8 MS24376-A4 Bs
— 2 6 MS24376-A3 Bs
LABINAL POWER SYSTEMS TF300-9E 3332 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — HERMETICALLY SEALED - 12 AMPS TO 50 AMPS
Ratings
Auxiliary Switch: SPDT rated 28 Vdc and 115 V 400 Hz, 5 Amp Res. & Ind. & 0.75 Amp Lamp
k Rated 100,000 operations electrical and mechanical life; Auxiliary switch rated 1,25 Amp Res. & 0.75 Amp Ind.
m These Ratings for 115 V 400 Hz only
n See MS Sheets for details
o Intermittent duty ratings for general applications. (See chart below)
p Ratings for 50/60 Hz only @ 115/200 Vac
r 400 Hz only
s Temperature Class D for 60 Hz AC Operation
Power Contact Ratings -
Continuous Duty oCoil Data Catalog
Number
28 Vdc 115/200 Vac 400 Hz Max. Coil Power Max.
Volts
Pick Up
at Amb.
Temp.
Volts
Amperes Amperes Hold Drop
Out
Res. Ind. Motor Res. Ind. Motor Amps Volts
12 12 612
25
12
25
6
25
0.6
0.6
0.6
29 dc 18 dc 7 dc 1.5 dc 6042H110-2
6042H141-2
6042H142-2
25 25 25 0.225 124 ac 90 ac 40 acr10 ac 6042H290-2
6042H291-2
50m50m50m0.50
0.50
29 dc 18 dc 7 dc 1.5 dc
6042H155-2
6042H156-2
50 50 50
50 50 50 0.6
0.6
6042H145-2
6042H146-2
50 50 50 0.225 124 ac 90 ac 40 ac 10 ac
6042H147-2
6042H148-2
6042H285-2
6042H288-2
Intermittent Duty Ratings
Continuous 15 Minutes 5 Minutes 1 Minute Max. Inrush
100% 130% 150% 200% 600%
In general, these power relays can withstand the above intermittent duty overcurrent.
Options:
Internal Coil Suppression
LABINAL POWER SYSTEMS TF300-9E 3332 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — HERMETICALLY SEALED - 100 AMPS TO 400 AMPS
Typical Configurations
Cat. No. 6042H151
SPST, 200 Amp
Cat. No. 6042H153
SPST, 300 Amp
Characteristics:
• Electrical Life:
50,000 cycles
(sea level to 80,000 feet)
• Mechanical Life:
100,000 cycles
• Acceleration: 15 g's
• Shock: 25 g's
• Ambient Temperature Class:
- B -70°C to 125°C
- D -70°C to 71°C
• Hermetically sealed/ MIL-
PRF-6106
• Twin Break Silver Alloy Main
Contacts
• Vibration Levels (Typical):
Cat. No. 6042H286
3 PST, 100 Amp
Auxiliary switch: SPDT rated 28 Vdc and 115 V 400 Hz, 5 Amp Res. & Ind. & 0.75 Amp Lamp.
kRated 100,000 operations electrical and mechanical life. Auxiliary switch rated 1.25 Amp Res. & 0.75 Amp Ind.
lRated 50 g shock.
mThese ratings for 115 V 400 Hz only.
nSee MS Sheets for details.
oIntermittent duty ratings for general applications (see chart below).
qRatings for 50/60 Hz only @ 115/200 Vac.
5-10 CPS
.08 DA
10-5 CPS
.06 DA
55-200CPS
10 g’s
250-500 CPS
5 g’s
500-1500 CPS
3 g’s
Intermittent Duty Ratings:
Continuous
100%
15 Minutes
130%
5 Minutes
150%
1 Minute
200%
Max. Inrush
600%
In general, these power relays can withstand the above intermittent duty overcurrent.
Options:
Internal Coil Suppression
Catalog
Number
Continuous
Ampere
Contact Rating
Poles
and
Throw
Operating
Coil
Voltage
Number
Aux.
Contacts
Dimension
Drawing
Figure
Number
Wiring
Diagram
Figure
Number
Government
Type
Number
Temp
Class/
Note
Power Contact Ratings —
Continuous Dutyo
Max. Time In
Seconds
Coil Data
Volts
28 Vdc
Amperes
115/200 Vac 400 Hz
Amperes
Max. Coil
Power
Max.
Volts
Pick-
up @
Res. Ind. Motor Res. Ind. Motor Operate Release Amps Volts Amb
Temp.
Hold Drop
Out
6042H159-2
6042H160-2
6042H166-2
100
SPST 28 Vdc
—
1
—
—
1
—
1
—
—
1
—
1
—
1
1
1
1
2
2
2
2
1
1
1
1
1
1
1
9
10
9
6
8
8
6
9
10
9
9
10
9
10
MS24141-D1
MS24141-D2
MS24182-D1
MS24168-D1
MS24168-D2
MS24168-A4
MS24168-A3
MS24142-D1
MS24142-D2
MS24183-D1
MS24184-D1
—
—
—
B
B
D
B
B
D
D
B
B
D
D
D
D
D
100
100
100
100
100
100
100
200
200
200
300
300
400
400
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
100
200
200
200
250
250
250
250
100 m
100 m
100 m
100 m
100
100
100
200
200
200
300
300
400
400
—
—
—
50q
50q
50q
50q
—
—
—
—
—
—
—
75m
75m
75m
100 m
100
100
100
150
150
150
150
150
150
150
0.025
0.025
0.02
0.06
0.06
0.06
0.06
0.035
0.035
0.03
0.035
0.035
0.035
0.01
0.01
0.01
0.015
0.025
0.11
0.08
0.015
0.015
0.01
0.015
0.015
0.015
0.5
0.5
0.5
0.6
0.6
0.25
0.25
0.6
0.6
0.5
0.6
0.6
0.6
0.6
29 dc
29 dc
29 dc
29 dc
29 dc
120 ac
120 ac
29 dc
29 dc
29 dc
29 dc
29 dc
29 dc
29 dc
18 dc
18 dc
18 dc
18 dc
18 dc
90 ac
90 ac
18 dc
18 dc
18 dc
18 dc
18 dc
18 dc
18 dc
7 dc
7 dc
7 dc
7 dc
7 dc
40 ac
40 ac
7 dc
7 dc
7 dc
7 dc
7 dc
7 dc
7 dc
1.5 dc
1.5 dc
1.5 dc
1.5 dc
1.5 dc
10 ac
10 ac
1.5 dc
1.5 dc
1.5 dc
1.5 dc
1.5 dc
1.5 dc
1.5 dc
6042H161-2
6042H162-2 3PST
6042H286-2
6042H289-2 115 Vac
6042H151-2
6042H152-2
6042H167-2
200
SPST 28 Vdc
6042H153-2
6042H154-2 300
SM400H2-2
SM400H3-2 400
LABINAL POWER SYSTEMS TF300-9E 3534 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — HERMETICALLY SEALED
Figure 1 Figure 2
Catalog
Number
Ampere
Rating
Dimensions
in Inches
Dimensions in Inches Net Term. Stud Dia. G Weight Dimensions in Millimeters Weight
Wide High Deep Mounting Hole Lbs. Wide High Deep Mounting Hole Grams
A B C D E F Power Coil A B C D E F
6042H110-2
6042H141-2
6042H142-2
6042H145-2
6042H146-2
6042H147-2
6042H148-2
6042H151-2
6042H152-2
6042H153-2
6042H154-2
6042H155-2
6042H156-2
6042H159-2
6042H160-2
6042H161-2
6042H162-2
6042H166-2
6042H167-2
6042H285-2
6042H286-2
6042H288-2
6042H289-2
6042H290-2
6042H291-2
SM400H2-2
SM400H3-2
12
25
25
50
50
50
50
200
200
300
300
50
50
100
100
100
100
100
200
50
100
50
100
25
25
400
400
2
2
2
2
2
2
2
1
1
1
1
1
1
1
1
2
2
1
1
2
2
2
2
2
2
1
1
3.305
3.305
3.305
3.305
3.305
3.305
3.305
3.640
3.640
3.640
3.640
2.700
2.700
3.640
3.640
4.250
4.250
3.640
3.672
3.305
4.235
3.305
4.235
3.305
3.305
3.640
3.640
4.485
3.250
4.513
3.200
4.485
3.200
4.485
3.700
4.972
3.700
4.973
2.665
3.947
3.250
4.532
4.280
5.615
3.063
3.282
4.485
5.553
3.200
4.280
3.250
4.513
3.700
4.973
3.700
3.700
3.700
3.700
3.700
3.700
3.700
3.315
3.315
3.315
3.315
2.835
2.835
2.925
2.925
4.220
4.220
2.925
2.957
3.700
4.218
3.700
4.218
3.700
3.700
3.315
3.315
3.250
3.250
3.250
3.250
3.250
3.250
3.250
—
—
—
—
—
—
—
—
3.697
3.697
—
—
3.250
3.697
3.250
3.697
3.250
3.250
—
—
2.687
2.687
2.687
2.687
2.687
2.687
2.687
3.000
3.000
3.000
3.000
2.188
2.188
3.000
3.000
3.510
3.510
3.000
3.000
2.687
3.510
2.687
3.510
2.687
2.687
3.000
3.000
0.218
0.218
0.218
0.218
0.218
0.218
0.218
0.266
0.266
0.266
0.266
0.218
0.218
0.266
0.266
0.218
0.218
0.266
0.266
0.218
0.218
0.218
0.218
0.218
0.218
0.266
0.266
.190-32 UNF-2B
.190-32 UNF-2B
.190-32 UNF-2B
.190-32 UNF-2B
.190-32 UNF-2B
.19O-32 UNF-2B
.190-32 UNF-2B
.375-24 UNF-2B
.375-24 UNF-2B
.375-24 UNF-2B
.375-24 UNF-2B
.190-32 UNF-2B
.190-32 UNF-2B
.250-28 UNF-2B
.250-28 UNF-2B
.250-28 UNF-2B
.250-28 UNF-2B
.250-28 UNF-2B
.375-24 UNF-2B
.190-32 UNF-2B
.250-28 UNF-2B
.190-32 UNF-2B
.250-28 UNF-2B
.190-32 UNF-2B
.190-32 UNF-2B
.375-24 UNF-2B
.375-24 UNF-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
.138-32 UNC-2B
1.60
1.50
1.60
1.60
1.70
1.70
1.82
2.30
2.50
2.40
2.50
0.90
1. 10
1.40
1.60
3.30
3.45
1. 10
1.70
1.90
3.70
1.80
3.60
1.70
1.90
2.40
2.50
83.95
83.95
83.95
83.95
83.95
83.95
83.95
92.46
92.46
92.46
92.46
68.58
68.58
92.46
92.46
107.95
107.95
92.46
93.27
83.95
107.57
83.95
107.57
83.95
83.95
92.46
92.46
113.92
82.55
114.63
81.28
113.92
81.28
113.92
93.98
126.29
93.98
126.31
67.69
100.25
82.55
115 .11
107.57
142.62
77.80
83.36
113.92
141.05
81.28
108.71
82.55
114.63
93.98
126.31
93.98
93.98
93.98
93.98
93.98
93.98
93.98
84.20
84.20
84.20
84.20
72.01
72.01
74.30
74.30
107.19
107.19
74.30
75.11
93.98
107.14
93.98
107.14
93.98
93.98
84.20
84.20
82.55
82.55
82.55
82.55
82.55
82.55
82.55
—
—
—
—
—
—
—
—
93.90
93.90
—
—
82.55
93.90
82.55
93.90
82.55
82.55
—
—
68.25
68.25
68.25
68.25
68.25
68.25
68.25
76.20
76.20
76.20
76.20
55.58
55.58
76.20
76.20
89.15
89.15
76.20
76.20
68.25
89.15
68.25
89.15
68.25
68.25
76.20
76.20
5.54
5.54
5.54
5.54
5.54
5.54
5.54
6.76
6.76
6.76
6.76
5.54
5.54
6.76
6.76
5.54
5.54
6.76
6.76
5.54
5.54
5.54
5.54
5.54
5.54
6.76
6.76
727.27
681.82
727.27
727.27
771.11
771.11
825.54
1043.26
1133.98
1088.62
1133.98
408.23
498.95
635.03
727.27
1496.86
1568.18
498.95
771.11
861.83
1678.29
816.47
1636.36
771.11
861.83
1088.62
1133.98
NOTE: All coils and auxiliary terminals are 6-32. Dimensions are approximate and should not be used for construction purposes.
Approximate Dimensions and Weights
LABINAL POWER SYSTEMS TF300-9E 3534 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — HERMETICALLY SEALED
Typical Wiring Diagrams (See Selection Table for Diagram No. Reference)
Dia. No. 7 Dia. No. 8
Dia. No. 9 Dia. No. 10
Dia. No. 6
Dia. No. 2
Dia. No. 1
X2
X1
T3
L3
T2
L2
T1
L1
X2
X1
A2
A1
B2
B1
C2
C1
X2
X1
T3
L3
T2
L2
T1
L1
NC
NC
NO
NO
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
14
13
12
11
X2
X1
A2
A1
X2
X1
CA2
A1
CB2
B1
CC2
C1
14
13
12
11
X2
X1
T3
L3
T2
L2
T1
L1
X2
X1
A2
A1
B2
B1
C2
C1
X2
X1
T3
L3
T2
L2
T1
L1
NC
NC
NO
NO
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
14
13
12
11
X2
X1
A2
A1
X2
X1
CA2
A1
CB2
B1
CC2
C1
14
13
12
11
X2
X1
T3
L3
T2
L2
T1
L1
X2
X1
A2
A1
B2
B1
C2
C1
X2
X1
T3
L3
T2
L2
T1
L1
NC
NC
NO
NO
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
14
13
12
11
X2
X1
A2
A1
X2
X1
CA2
A1
CB2
B1
CC2
C1
14
13
12
11
X2
X1
T3
L3
T2
L2
T1
L1
X2
X1
A2
A1
B2
B1
C2
C1
X2
X1
T3
L3
T2
L2
T1
L1
NC
NC
NO
NO
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
14
13
12
11
X2
X1
A2
A1
X2
X1
CA2
A1
CB2
B1
CC2
C1
14
13
12
11
X2
X1
T3
L3
T2
L2
T1
L1
X2
X1
A2
A1
B2
B1
C2
C1
X2
X1
T3
L3
T2
L2
T1
L1
NC
NC
NO
NO
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
B2
B1
C2
C1
14
13
12
11
X2
X1
A2
A1
14
13
12
11
X2
X1
A2
A1
X2
X1
CA2
A1
CB2
B1
CC2
C1
14
13
12
11
LABINAL POWER SYSTEMS TF300-9E 3736 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — TERMINAL COVERS FOR HERMETICALLY SEALED POWER RELAYS
Specifications
• Molded of unbreakable nylon
• Ambient temperature ranges:
-70°C to 125°C
• Secured by coil terminal
hardware
• Part number molded into
cover
• Positive protection between
power stubs
Part No. 49-2667
MS27243-3
Part No. 49-2672
MS27243-5
Part No. 49-2661
MS27243-1
Part No. 49-2665
MS27242-1
Part No. 49-2670
MS27243-4
LABINAL POWER SYSTEMS TF300-9E 3736 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — TERMINAL COVERS FOR HERMETICALLY SEALED POWER RELAYS
Terminal Covers Application Approximate Dimensions and Weights
Figure 1
Figure 2
Labinal Power
Systems Relays
Relay
MS Numbers
Terminal Cover Part
Number
MS27243
6042H110-2 MS24143-D3 49-2661 -1
26042H141-2 MS24143-D1 49-2661 -1
6042H142-2 MS24143-D2 49-2661 -1
6042H145-2 MS24376-D1 49-2661 -1
6042H146-2 MS24376-D2 49-2661 -1
6042H147-2 MS24376-A1 49-2661 -1
6042H148-2 MS24376-A2 49-2661 -1
6042H151-2 MS24142-D1 49-2672 -5
6042H152-2 MS24142-D2 49-2672 -5
6042H153-2 MS24184-D1 49-2672 -5
6042H154-2 MS24184-D2 49-2672 -5
6042H155-2 MS24140-D1 49-2667 -3
6042H156-2 MS24140-D2 49-2667 -3
6042H159-2 MS24141-D1 49-2665 -2
6042H160-2 MS24141-D2 49-2665 -2
6042H161-2 MS24168-D1 49-2670 -4
6042H162-2 MS24168-D2 49-2670 -4
6042H166-2 MS24182-D1 49-2667 -3
6042H167-2 MS24183-D1 49-2665 -2
6042H286-2 MS24168-A4 49-2670 -4
6042H288-2 MS24376-A3 49-2661 -1
6042H289-2 MS24168-A3 49-2670 -4
6042H290-2 MS24143-A3 49-2661 -1
6042H291-2 MS24143-A4 49-2661 -1
SM400H2-2 — 49-2672 -5
SM400H3-2 — 49-2672 -5
Part
Number
Figure
Number
Dimensions in In./Mill. Ship Wt. Lbs./
gm
A B C
49-2661 1 2.32/58.93 0.75/19.05 2.94/74.68 .025/11.31
49-2665 1 2.56/65.02 1.17/29.72 2.12/53.85 .026/11.77
49-2667 1 2.66/67.56 1.11/28.19 2.05/52.07 .027/12.22
49-2670 1 2.75/69.85 1.06/26.92 3.81/96.77 .044/19.91
49-2672 1 3.00/76.20 1.17/29.72 2.50/63.50 .030/13.57
NOTE: Dimensions are approximate and should not be used for construction purposes.
LABINAL POWER SYSTEMS TF300-9E 3938 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — HERMETICALLY SEALED LIGHT-WEIGHT - SM100H1
Engineering Data
• MIL-R-6106 Type I
- Hermetically Sealed
- Continuous Duty
• Weight - 11.3 oz. (320 grams)
• Seal - 1x10-6 STD CC/SEC
Max
• Altitude: 80,000 Feet
• Double Break Contacts
Selection Table
(4) #8 (.164) - 32UNJC-3A SCREW
CAPTIVE, HEX HEAD
(4) RETAINING RING, CRIMP-ON STYLE
• SM100H1
• M6106/48-001
• SM100H15
• M6106/48-002
Application Notes
The curve shows a typical motor/generator requirement. The
SM100H1 can withstand up to 400 Amps for several seconds
during motor start - dropping to 100 Amps within 5 seconds. The
SM100H1 can withstand the generator output up to 200 Amp for
several minutes - dropping to 100 Amps within 3.5 minutes. These
cycles can be repeated once every 90 seconds. The SM100H1 will
meet applications requiring a reliable and robust contactor.
Vibration Random 15 Minutes Each
Plane
M6106/48-001
Frequency (Hz) Level (g^2/Hz)
10 - 125 0.037
125 - 250 +4 dB
250 - 1000 0.1
1000 - 2000 -3 dB
Vibration Random 15 Minutes Each Plane
M6106/48-002
Frequency (Hz) Level (g^2/Hz)
15 - 50 0.012
120 - 200 0.364
250 - 400 0.194
600 - 1000 0.060
1300 - 2000 0.097
Test to be performed with 5 ampere load on main contact.
DC - Motor start (seconds)
Normally twice per flight
400
300
AMPERES
200
100
510
SECONDS / MINUTES
15
0
Battery charge (minutes)
Normally twice per flight
LABINAL POWER SYSTEMS TF300-9E 3938 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — HERMETICALLY SEALED LIGHT-WEIGHT - SM100H1
Engineering Data
• Meets MIL-R-6106/48
Type I Hermetically Sealed Continuous Duty
• Power Contacts SPST:
- 28 Vdc
- Load Ratings:
Resistive: 100 Amps
Inductive: 100 Amps (10,000 cycles)
Motor: 50 Amps -001; 25 amps -002
Lamp: 50 Amps (25,000 cycles)
Minimum: 10 Amps
Overload: 800 Amps (See application curve)
Rupture: 1000 Amps
- Contact Voltage Drop:
Initial 0.100 V
After Test - 0.150 V
• Life:
- Electrical: 50,000 cycles
- Mechanical: 100,000 cycles
• Auxiliary Contacts SPDT Form "Z":
- Voltage: 28 Vdc
- Resistive: 5 Amps
- Inductive: 5 Amps (10,000 cycles)
- Lamp: 1 Amp (25,000 cycles)
- Minimum: 2 MA at 28 Vdc.
- Contact Voltage Drop: Maximum: 5 MV +/- 100 MA and 6V
• Current above 125 MA negates minimum current capability.
• Operating Temperature: -55°C to 125°C
• Shock: ½ Sine 50 g's 6-9 MS:
- Contact Opening: 2 millisec. max.
• Insulation Resistance Minimum:
- Initial: 100 Megohms
- After Test: 50 Megohms
• Vibration: Sinusoidal (-001 only)
- 5 to 10 Hz 0.08 DA
- 10 to 55 Hz 0.05 DA
- 55 to 2000 Hz 10 g's
• Vibration (Gun Fire) 15 minutes each plane:
- 0.0375 g/Hz for 10 to 125 Hz
- 4DB/Octave inc 125 to 250 Hz
- 0.1 g/Hz for 250 to 1000 Hz
- 3DB/Octave decrease 1000 to 2000 Hz
• Dielectric Strength Sea Level 2-5 sec. Voltage=VRMS 60 Hz:
- All points: 1250 V Initial, 1000 V After Tests
• Dielectric Strength Altitude 1 min. 60 Hz:
- Coil & contacts: 500 V Initial & After Test
- All other points: 500 V Initial & After Test
• Duty Cycle: Continuous
• Maximum Voltage: 30 Vdc
• Pick up: 18 Vdc (15 Vdc at 25°C)
• Hold-in: Unit must drop out
at 1.5 Vdc & below and can
drop out at any voltage below
7 Vdc.
• Operate Time: 30 MS maximum
Release Time: 20 MS maximum
• Contact Bounce: 3 MS
maximum main and auxiliary
contacts.
• Coil Resistance:
@-25°C; 100 Ohms minimum
(- 002); 90 Ohms Minimum
(-001).
• Coil Suppression: 0.42 V max.
Peak Inverse Voltage.
Dimensions
Schematic
Coil Data
.250-28 UNF-2A
.090
22.86
INTERNAL COIL
SUPRESSOR
AUXILIARY
CONTACTS
X2 X1A1 13 11
A2 14 12
2.90
77.66
.656
16.66
2.000
50.80
.170
4.31
2.000
50.80
2.430
61.72
2.430
61.72
2.016
51.21
LABINAL POWER SYSTEMS TF300-9E 4140 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — ENVIRONMENTALLY SEALED LIGHTWEIGHT - SM15 SERIES
Engineering Data
• Meets MIL-R-6106 Type IV
• Weight: 10.5 ounces (284 g)
• Altitude:
-Rated: 50,000 feet
-Extended: 80,000 feet
with encapsulated terminals
• Ratings:
-Voltage: 115/200 V, 400 Hz, 3Æ
-Load Ratings:
Resistive: 60 Amps
Inductive: 60 Amps
Motor: 40 Amps
Minimum Current: 4 Amps
Rupture: 400 Amps
• Environmental Seal: MIL-STD-
202, METHOD 112 Test
Condition C Procedure IV
• Seal: 6 x 10-4 STD CC/SEC
• Economizer Coil: 30 Vdc
- Inrush: 1.25 Amps
(20 milliseconds max)
-Steady State: 0.25 Amps
Typical Wiring Digrams
3 P.S.T. - N.C.
Auxiliary Contact
115/200 Vac 400 Hz 28 Vdc
• Resistive 60 A. 20 A.
• Inductive 60 A. 10 A.
• Motor 40 A. ….
• Minimum Current 4 A. ….
• Rupture 400 A. ….
• Contact Drop
- Initial 0.150 V Max. ….
- After Life Test 0.175 V. Max. ….
• Contact Bounce 2 Milliseconds
DC ratings are maximum overload capability. By wiring two poles in series, 28
Vdc rating can be increased to the same as the full AC ratings.
Options
• AC operated coils
• Encapsulated terminals
• Internal coil suppression
• Suitable for synchronized power supplied transfer
Power Contact Ratings (Continuous Duty)
Selection Table
3 P.S.T. - N.C.
Auxiliary Contact
3 P.D.T. Without
Auxiliary Contact
3 P.DT. With
Auxiliary Contact
3 P.S.T. N.O. Without
Auxiliary Contact With
Internal Coil Suppression
X1 (+)
X2 (-)
A3
B3
C3
A2
B2
C2
X1 (+)
X2 (-)
A3
B3
C3
A3
B3
C3
12
11
13
X1 (+)
X2 (-)
A3
A1 A2
B3
B1 B2
C3
C1 C2
X1 (+)
X2 (-)
A3
A1 A2
B3
B1 B2
C3
C1 C2
12
11
13
X1 (+)
X2 (-)
A1 A2
B1 B2
C1 C2
Poles and
Throw-Circuit
Number of Auxiliary
Contacts 1 P.D.T.
Government Type
Number M6106
Catalog
Number
3 P.S.T.-N.O. —
1
/10-001
/10-002
SM15AWD1
SM15AXD1
3 P.S.T.-N.C. —
1
/11-001
/11-002
SM15BWD1
SM15BXD1
3 P.D.T. —
1
/9-001
/9-002
SM15CWD1
SM15CXD1
3 P.S.T.-N.O. — 10-005* SM15AWD3
* Unit supplied with internal coil suppression. 45 V max. peak inverse voltage.
LABINAL POWER SYSTEMS TF300-9E 4140 LABINAL POWER SYSTEMS TF300-9E
POWER RELAYS — ENVIRONMENTALLY SEALED LIGHTWEIGHT - SM15 SERIES
Engineering Data
Specifications
• Meets MIL-R-6106/9, /10, /11 Type IV Environmentally Sealed
- Continuous Duty Operation
• Power Contacts 400 Hz:
- Voltage: 115 V Single Phase
115 V/ 200 V Three Phase
- Load Ratings per Pole:
Resistive: 60 Amps
Inductive: 60 Amps
Motor: 40 Amps
Minimum Current: 4 Amps
Overload: 320 Amps
Rupture: 400 Amps
- Electrical Life at Rated Loads: 100,000 operations (50,000 motor)
- Mechanical Life at 15 Amps: 200,000 operations
• Auxiliary Contacts 115 V 400 Hz/ 28 Vdc:
- Resistive: 3 Amps
- Inductive: 1.5 Amps
- Mechanical: 0.5 Amps
• Operating Temperature: -55°C to 71°C
• Shock: ½ Sine, 25 g's 6 to 9 MS
- Contact Opening: 1 millisecond maximum
• Acceleration: 15 g's
• Insulation Resistance Minimum
- Initial: 200 Megohms
- After Test: 100 Megohms
• Vibration:
- 5 to 10 Hz 0.08" DA
- 10 to 55 Hz 0.06" DA
- 55 to 400 Hz 10 g's
- 400 to 800 Hz 8 g's
- 800 to 2000 Hz 8 g's (-55°C to 25°C) 7 g's at 71°
• Dielectric Strength Sea Level 2-5 sec. 60 Hz:
- Coil & Auxiliary Contacts: 1250 V Initial, 1000 V After Test,
Across open power contacts: 1250 V Initial 625 V After Life.
- All Other Points: 1800 V Initial, 1350 V After Test
• Dielectric Strength Altitude 1 minute 60 Hz:
- Coil & Auxiliary Contacts: 500 V Initial & After Test
- All Other Points: 700 V Initial & After Test
Coil Data
• 28 Vdc: Inrush 1.25 Amps (20 MS Max); Steady State 0.25 Amps
• Pick-up: 17 Vdc. Hold in: 7.0 Vdc
Drop-out: 1.5 Vdc Unit must drop out at 1.5 Vdc and below and
can drop out at any voltage below 7 Vdc.
• Operate Time: 25 MS. Release Time: 25 MS
• Contact Bounce: 2 MS maximum main and auxiliary contacts
Dimensions Drawings
Top View - SM15CXD1 3PDT and Auxiliary Contacts
Top View - SM15AWD1 3 PST N.O. Contacts. Without
Auxiliary Contacts
Side View
X2
X1
1.375
(34.93)
A1 B1 C1
A2 B2 C2
.240 R.
(6.096)
2.313
(58.75)
NAMEPLATE CIRCUIT
PLATE
1.890
(48.01)
2.125
(53.98)
.475
(12.07)
UPPER AND
LOWER BARRIERS
2.500
(63.50)
3.032
(77.01)
A2
2.40
(60.96)
.60
(5.24)
A3 B3 C3
A1 B1 C1
13
12
11
.240 R.
(6.096)
1.06
(26.92)
.148
(3.76)
DIA.
4 MTG. HOLES
1.900
(48.26)
2.313
(50.75)
Power Terminals
.190-32 UNF-2A
SM15CXDI 3PDT
and Auxiliary
Contacts
LABINAL POWER SYSTEMS TF300-9E 4342 LABINAL POWER SYSTEMS TF300-9E
GENERATOR CONTACTORS — 40 KVA 135 AMPERES CONTACTORS - SM135B2
Approximate Dimensions
LABINAL POWER SYSTEMS TF300-9E 4342 LABINAL POWER SYSTEMS TF300-9E
GENERATOR CONTACTORS — 40 KVA 135 AMPERES CONTACTORS
SM135B2 POWER RELAY - 115/200 V 400 HZ
Electrical Characteristics
Engineering Data
Specifications
• Designed to MIL-R-6106/42
• All moving parts, contacts,
and magnet coil gasket
sealed & vented
• Operable at altitudes to
50,000 feet
• Operating Temperature:
-55°C to +71°C
• Altitude: 50,000 ft. Max.
• Vibration:
- Per MIL-E-5400
- Curve IV, 5-2000 Hz
• Shock: 30 g's, Half Sine, 11
MS Duration
• Acceleration: 6 g's
• Maximum weight: 3.15 Lbs/
1425.31 gm
• Overload Current: 1080 Amps
• Rupture Current: 1350 Amps
Insulation Resistance (Initial): 200 Megohms
After Life or Environmental Tests: 100 Megohms
Contact Voltage Drop (Initial): MAIN 0.175 V max. - .150 V avg
After Life Test 0.200 V max. - .175 V avg
Contact Voltage Drop (Initial) AUX 0.400 V max. - .300 V avg
After Life Test 0.450 V max. - .400 V avg
At 5 Amps
Overload Current (Main) 1080 amp
Rupture Current (Main) 1350 amp
Duty Rating Continuous
Coil Suppression to meet requirements of MIL-E-6051D(1)
Application Notes
Mechanically interlocked contact circuits prevent inadvertent opera-
tion of the alternate contact circuits. These units are suitable for
load transfer typically from ground support to on-board power.
Dielectric Strength
Test Voltage Vrms
Description At Sea Level (2-5 Sec.) At Altitude (60 Sec.)
Initial After Life
28 Vdc 115 Vac 28 Vdc 115 Vac 28 Vdc 115 Vac
Coil to Case 1250 — 1000 — 500 —
Aux. Contacts 1250 1500 1000 112 5 500 500
All Other
Points
NA 1800 NA 1350 NA 700
Operating Characteristics
Coil Data **
Drop-Out
Voltage
Time Milliseconds Max.
Nominal Max * Amp Pick-Up Volts
Volts Volt In
Rush Cont.
At
25°C
Hi
Temp
Count
Cur.
Coil Voltage Bounce Time
at 28 Vdc
18 Vdc 23 Vdc 30 Vdc
Operate Release Transfer Main Aux.
28DC 30 5 1 15DC 18DC 22.5 DC 7+0/-6 50 35 10 2 4
* Pick-Up: Coil will operate at the voltages shown and higher.
** Drop-Out: Coil will drop out at 1 Vdc and may drop out at any voltage from 7 Vdc and below.
Rated Contact Load — (Amps per pole) Case Grounded
Type
of
Load
Life
Operating
Cycles
X103
28 Vdc 115 Vac 1 Phase 400 Hz 115/200 Vac 3 Phase 400 Hz
Main Aux. Main Aux. Main Aux.
N.O. N.C. N.O. N.C. 400
Hz
60
Hz
400
Hz
60
Hz
400
Hz
60
Hz
400
Hz
60
Hz
Resistive 50 120* — 5 5 135 —5—135 —5—
Inductive 50 — — 3 3 135 —3—135 —3—
Motor 50 — — — — 80 — — — 80 — — —
Lamp — — — 2 2 — — 2 — — — 2 —
Transfer Load 10 ————135 ———135 ———
Mech. Life
Reduced Amps 100 — — 1.25 1.25 33.75 — 1.25 — 33.75 — 1.25 —
Interm.
Current
50 13.5 13.5 Per MIL-R-6106
* Room Ambient conditions 100,000 operations.
LABINAL POWER SYSTEMS TF300-9E 4544 LABINAL POWER SYSTEMS TF300-9E
FLAT PACKS — CUSTOM CAPABILITY
Engineering Data
• Construction: Gasket Sealed (vented) -
MIL - R - 6106 Type III, except as
noted
• Ratings:
- Main Contacts
Configuration: SPST N.O.
Voltage (Nominal): 28 Vdc
Current
Resistive: 400 Amp (Terminal Temperature
Rise 85°C above 71°C Ambient)
Inductive: 100 Amps
Motorload: 400 Amps
Overload: 2,000 Amps
Custom Motor Current: See Graph 20,000 cycles (Min.)
Motor Current test to be run 5 cycles per hour maximum
with 90 seconds off time between cycles
• Life:
Electrical: 50,000 Cycles Minimum
Mechanical: 100,000 Cycles
- Weight: (Max.): 2.25 Lbs/ 1020.58 gm
• Environmental Data
Ambient Temp: -55°C to +71°C
Altitude: 50,000 Feet Maximum
- Vibration: 5 to 14 Hz 0.2" Double Amplitude
14 to 33 Hz 2 g
33 to 52 Hz 0.036"
Double Amplitude
52 to 500 Hz 5 g (peak)
- Acceleration: 12 g Maximum (Steady State Load)
- Shock:
G-Level: 25 g's
Duration: 6 to 9 Milliseconds
- Max. Duration Contact 2 Milliseconds
Opening
• Coil Data:
- Duty Cycle: Continuous, Economizing
- Nom. Operating
- Voltage: 28 Vdc
- Pick-Up Voltage: 18 Vdc Max. at 25°C
- Drop-Out Voltage: 0.75-3.50 Vdc at 25°C
- Hold Voltage: 9 Vdc
- Operating Time: 35 Milliseconds Maximum
- Inrush Current: 3.0 Amps Max for 50 Milliseconds
Max. at 25°C
- Hold Current: 1.2 Amps Max. at 25°C
• Auxiliary Contacts:
- Voltage: 28 Vdc or 115 V, 400 Hz
- Current: 5 Amp Resistive
• Low Level Auxiliary Contacts
• Auxiliary Terminal Size and
Length
Options
Electronic Control will add
coil turns to compensate for
low battery voltage during
starter operation.
LABINAL POWER SYSTEMS TF300-9E 4544 LABINAL POWER SYSTEMS TF300-9E
FLAT PACKS — CUSTOM CAPABILITY
Typical Configurations — 400 Amp
12
11
+X1
-X2
ELECTRONIC
CONTROL
COIL
A1 A2
13 14
A2
A1
141312
11
-X2
+X1
INSTALLATION
RECOMMENDED
HIGH VOLTAGE TEST
SHORT +X1 TO -X2 BEF0RE
CAUTION
INSTALLATION
RECOMMENDED
TORQUE 19 in-lbs MAX
TORQUE 90 in-lbs MAX.
NAMEPLATE
4.56
115.82
4.06
103.12
.266
6.76
DIA.
2 MTG. HOLES
.88
22.35
.1.75
44.45
.1.28
32.51
2.56
65.02
1.25
31.75
2.00
50.80
1.13
28.70
A2
A1
-X2IND
+X1
INSTALLATION
RECOMMENDED
HIGH VOLTAGE TEST
SHORT +X1 TO -X2 BEF0RE
CAUTION
INSTALLATION
RECOMMENDED
TORQUE 19 in-lbs MAX
TORQUE 90 in-lbs MAX.
NAMEPLATE
4.56
115.82
3.13
79.50
.78
19.81
4.06
103.12
1.25
31.75
A2
A1
+X1
-X2
23
24
11 12 13
14
INSTALLATION
RECOMMENDED
HIGH VOLTAGE TEST
SHORT +X1 TO -X2 BEF0RE
CAUTION
INSTALLATION
RECOMMENDED
TORQUE 19 in-lbs MAX
TORQUE 90 in-lbs MAX.
NAMEPLATE
4.56
115.82
4.06
103.12
1.25
31.75
2.00
50.80
1.13
28.70
3.42
86.87
NAMEPLATE
400 AMP S.P. -S.T.
28 VDC RELAY
28 VDC COIL
NO. SM400D78
FSCM 81640
MADE IN
U.S.A.
VENT LOCATION
5.15
130.81
.50
12.70
6 X #10(.190)-32UNF-2A
GR835AAR
.06
1.52
.75
19.05
(2) .375-24UNF-2A
12
11
+X1
-X2
ELECTRONIC
CONTROL
COIL
A1 A2
13 14
+X1
-X2
ELECTRONIC
IND
SUPPLIES 28 Vdc POWER
FROM MOVEABLE CONTACTS
CONTROL
COIL
A1 A2
.266
6.76
DIA.
2 MTG. HOLES
.88
22.35
.1.75
44.45
.1.28
32.51
2.56
65.02
.266
6.76
DIA.
2 MTG. HOLES
.88
22.35
.1.75
44.45
.1.28
32.51
2.56
65.02
LABINAL POWER SYSTEMS TF300-9E 4746 LABINAL POWER SYSTEMS TF300-9E
QUALIFIED PRODUCTS UNDER MILITARY SPECIFICATION — MIL-PRF-6106 AND MIL-PRF-83383
MIL P/N Cross Reference
MIL P/N
Labinal Power
Systems P/N Page MIL P/N
Labinal Power
Systems P/N Page MIL P/N
Labinal
Power
Systems
P/N Page MIL P/N
Labinal
Power
Systems
P/N Page
M6106/9-001 SM15CWD1 36 M83383/02-06 SM600BA25A1 3 MS24166-D1 6041H200 19 MS24376-A2 6042H148 24/26
M6106/9-002 SM15CXD1 36 M83383/02-07 SM600BA35A1 3 MS24166-D2 6041H201 19 MS24376-A3 6042H288 24/26
M6106/10-001 SM15AWD1 36 M83383/02-08 SM600BA40A1 3 MS24168-A3 6042H289 24/26 MS24376-A4 6042H285 24/26
M6106/10-002 SM15AXD1 36 M83383/02-09 SM600BA50A1 3 MS24168-A4 6042H286 24/26 MS24376-D1 6042H145 24/26
M6106/10-005 SM15AWD3 36 M83383/02-10 SM600BA60A1 3 MS24168-D1 6042H161 24/26 MS24376-D2 6042H146 24/26
M6106/11-001 SM15BWD1 36 M83383/02-11 SM600BA75A1 3 MS24168-D2 6042H162 24/26 MS25030-D1B 6046H51 19
M6106/11-002 SM15BXD1 36 M83383/02-13 SM600BA100A1 3 MS24171-D1 6041H215 19 MS25031-D1B 6046H53 19
M6106/48-001 SM100H1 32 M83383/04-03 SM601BA10A1 3 MS24171-D2 6041H202 19 MS25032-D1 6046H46 19
M6106/48-002 SM100H15 32 M83383/04-04 SM601BA15A1 3 MS24172-D1 6041H216 19 MS27242-1 6042H181 24/26
M83383/01-01 SM600BA5N1 3 M83383/04-05 SM601BA20A1 3 MS24172-D2 6041H203 19 MS27242-2 6042H182 24/26
M83383/01-03 SM600BA10N1 3 M83383/04-07 SM601BA35A1 3 MS24178-D1 6041H219 19 MS27243-1 49-2661 23
M83383/01-04 SM600BA15N1 3 M83383/04-08 SM601BA40A1 3 MS24179-D1 6041H218 19 MS27243-2 49-2665 23
M83383/01-05 SM600BA20N1 3 M83383/04-10 SM601BA60A1 3 MS24179-D2 6041H206 19 MS27243-3 49-2667 23
M83383/01-06 SM600BA25N1 3 MS24140-D1 6042H155 24/26 MS24182-D1 6042H166 19 MS27243-4 49-2670 23
M83383/01-07 SM600BA35N1 3 MS24140-D2 6042H156 24/26 MS24183-D1 6042H167 19 MS27243-5 49-2672 23
M83383/01-08 SM600BA40N1 3 MS24141-D1 6042H159 24/26 MS24184-D1 6042H153 19 MS27243-6 49-3179 23
M83383/01-09 SM600BA50N1 3 MS24141-D2 6042H160 24/26 MS24184-D2 6042H154 19 MS27997-D1 6042H91 24/26
M83383/01-10 SM600BA60N1 3 MS24142-D1 6042H151 24/26 MS24185-D1 6041H217 19 MS27997-D2 6042H92 24/26
M83383/01-11 SM600BA75N1 3 MS24142-D2 6042H152 24/26 MS24185-D2 6041H205 19 AN3362 6041H209 19
M83383/01-13 SM600BA100N1 3 MS24143-A3 6042H290 24/26 MS24187-D1 6041H220 19 AN3372-1 6041H204 19
M83383/02-01 SM600BA5A1 3 MS24143-A4 6042H291 24/26 MS24187-D2 6041H230 19
M83383/02-03 SM600BA10A1 3 MS24143-D1 6042H141 24/26 MS24192-D1 9565H2 19
M83383/02-04 SM600BA15A1 3 MS24143-D2 6042H142 24/26 MS24193-D1 9565H94 19
M83383/02-05 SM600BA20A1 3 MS24143-D3 6042H110 24/26 MS24376-A1 6042H147 24/26
LABINAL POWER SYSTEMS TF300-9E 4746 LABINAL POWER SYSTEMS TF300-9E
ELECTRICAL SENSING & CONTROLS
Product Application
Information and Warranty
Disclaimer
It is buyer’s responsibility
to determine the suitability
of the particular device for
its application, and Labinal
Power Systems Aerospace
LLC. makes no warranties,
and assumes no liability as to
the suitability of sufficiency
for buyer’s application of
the device. Ratings and
switch performance are
valid only on devices which
have not been subjected to
unauthorized modifications or
misapplications. Dimensional
drawings are available upon
request.
Notice
The use of Labinal Power
Systems Aerospace
LLC. devices should be
in accordance with the
provisions of the National
Electric Code, U.L. and/
or other local, military or
industry standards that are
pertinent to the particular
end use. Installation or use
not in accordance with these
codes and standards could be
hazardous to personnel and/or
equipment.
Government Cage Code
The Government Cage Code
for products manufactured
by Labinal Power Systems
Aerospace Sensing & Controls
are 81640, 76374, 96182,
99145 and 27878.
Export Controls Compliance
Reminder to our catalog
customers, product in this
catalog, if exported, is subject
to United States
Export Control regulations.
Labinal Power Systems
Aerospace encourages our
customers to understand
the regulations and ensure
compliance, including
obtaining written U.S.
government authorizations
when applicable.
Need additional information
not contained in this
catalog? For technical
questions, application
assistance, or the name
of your local authorized
distributor, call 1-800-955-
7354.
LABINAL POWER SYSTEMS
Headquarters : 36 rue Raymond Grimaud 31700 BLAGNAC - FRANCE
Tél. +33 (0)5 34 60 00 00 - Fax +33 (0)5 34 60 01 99
www.labinal-power.com
Local contact (Sarasota, FL):
LABINAL POWER SYSTEMS
2250 Whitfield Avenue
Sarasota, FL 34243 USA
Tel. 1-800-955-7354 • Fax 941-751-7173