Product Catalog - Semco Aerospace

INSIDE
Interactive Cushions
Cable Control Systems
Pneumatic Systems
Motion Control Actuators
2015 Product
Catalog
1
Table of Contents
Table of Contents..............................................................1
Interactive Cushions Systems
Overview and Design Advantages....................2
CU-975-101-00...................................................3
CU-975-102-00...................................................3
CU-975-103-00...................................................4
Captain’s Seat Cushions
CU-975-018-00...................................................4
CU-975-101-05...................................................5
Other Seat Configuration Examples of Versatility
CU-975-092-00...................................................5
CU-975-097-00...................................................6
CU-976-002-00...................................................6
Cable Control Systems
Overview and Design Advantages....................7
ST-983-000-00.....................................................7
ST-983-001-00.....................................................8
ST-983-003-00.....................................................8
ST-983-017-00.....................................................9
ST-983-026-00.....................................................9
Pneumatic Systems
Overview and Design Advantages.................10
BL-920-001-00...................................................10
BL-980-006-00...................................................11
PS-935-001-00...................................................11
SC-925-013-00..................................................12
SC-925-018-00..................................................12
SC-925-100-00..................................................13
Motion Control Systems
Overview and Design Advantages.................13
Pax-Net Distribution System..........................14
Aeronautical Power Supply Unit.....................14
PA-989-000-00...................................................15
PA-989-200-00...................................................15
PA-989-500-15...................................................16
PA-989-550-17...................................................16
PA-989-600-00...................................................17
PA-989-700-00...................................................17
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2
Cushion Systems Overview
• a foam filled chamber with a push-button
valve allows air to escape or enter when
opened.
• when closed, the chamber is sealed and no
air may enter or escape.
• to adjust the contour, the seat occupant
leans on the cushion and opens the valve
causing the cushion to deform and fill all
the hollow spots of the occupants back and
relieve pressures on the bony protrusion of
the back i.e. the spine.
• To re-inflate the cushion, the occupant
merely leans forward, thereby removing
Design Advantages
pressue from the cushion, and simultaneously opens the valve.
• Almost any design can be achieved using
our construction method.
• The valve can mate with the Semco Aerospace cable controls which can be routed
to the armrest.
• Little to no weight or cost penalty over conventional fabricated seat foam.
• The finished device weighs nearly the same
as the foam it replaces, either in the seat
back or seat bottom.
Interactive Cushions
3
CU-975-101-00
• 3.5 inches of thickness for maximum adaptability.
• The valve configuration mates with
the Semco Aerospace Remote
Cable Control, ST-983-003 series
• Materials used exceed the requirements in FAR 25.853 (a)*.
CU-975-102-00
• Fits applications that have limited
back cushion thickness and require
adjustable lumbar contouring and
support.
• The valve mates with the Semco
aerospace Remote Cable Control
available in button or rocker style
inputs
• Materials used exceed the requirements in FAR 25.853 (a)*.
*
FAR 25.853 (a)
Interactive Cushions
4
CU-975-103-00
• Seat back cushion completely replaces the seat back foam.
• This unit, by itself, procides several
inches of recline when fully deflated.
This configuration could eliminate
the need for a recline lock and the
attendant strictural hardware for
close pitch seat systems.
• Materials used exceed the requirements in FAR 25.853 (a)*.
Captain’s Seats
• Originally desgined for MD-11 Captain’s seat
• Built in system designed to adapt to
each occupants back contours
• Materials used exceed the requirements in FAR 25.853 (a)*.
CU-975-018-00
*
FAR 25.853 (a)
Interactive Cushions
5
CU-975-101-05
• provides 3 inches of contour adjustment
with three valves.
• Each valve designed to maintain, decrease pressure or bleed the cushion
(depending on air pressure) with ease.
• The third valve also automatically reinflates the cushion over a period of ten
minutes after the occupant exits the seat.
• Materials used exceed the requiremetns
in FAR 25.853 (a)*.
Other Seat Configuration
examples of versatility
CU-975-092-00
• System comprised of two
chambers arranged vertically with interconnected tubing
relief to the spine as well as an
opening for seat trim anchor
points in the middle of the seat
back
• This configuration provides communication
between the two chambers so that if the
occupant leans against one chamber, the
air from that chamber will migrate to the
other and it will fill to “follow” the persons
back.
• Materials used exceed the requiremetns in
FAR 25.853 (a)*.
*
FAR 25.853 (a)
Interactive Cushions
6
CU-975-097-00
• Double vacuum form process which provides sculpted shapes on both front and
back surfaces.
• Versatility in desgin shapes
• Materials used exceed the requiremetns in
FAR 25.853 (a)*.
CU-976-002-00
• This configuration provides communication between the
two chambers so that if the occupant leans against one
chamber, the air from that chamber will migrate to the other
and it will fill to “follow” the persons back.
• Materials used exceed the requiremetns in FAR 25.853
(a)*.
*
FAR 25.853 (a)
Interactive Cushions
7
Cable Control Systems
Overview
• Our back support system is remotely adjusted with a cable type control with a variety of
customer interface inputs.
• Our traditional button type input has been
designed to require less than 1” clearance
from the outer panel surface.
Design Advantages
• the output mates directly with the Semco
Aerospace Lumbar Cushion valve.
• Can be routed around tight bends with no
loss of motion
• Adjuster can be located anywhere along the
conduit
• Several different styles of input
- Anodized push button
- Nylon rocker style
- Lever style for long stroke requirements
• Materials used exceed the requiremetns in
FAR 25.853 (a)*.
ST-983-000-00
• Connents to hydraulic lock or gas
lock.
• Designed to complement the ST-983003-00 remote lumbar control with
the snap-in, rocker style input.
• Materials used exceed the requiremetns in FAR 25.853 (a)*.
*
FAR 25.853 (a)
Cable Control Systems
8
ST-983-001-00
• Maintains a long stroke and increased mechanical Advantage to
minimize button/lever loads.
• Provides up to .50” of stroke
• Designed to complement Semco
Aerospace’s rocker type styling.
Materials used exceed the requiremetns in FAR 25.853 (a)*.
ST-983-003-00
• Connects to Semco Aerospace’s Interactive Cushions.
• Connects to snap-in, rocker style
input.
• Materials used exceed the requiremetns in FAR 25.853 (a)*.
*
FAR 25.853 (a)
Cable Control Systems
9
ST-983-017-00
• Low profile push button input
• Provides up to .170 in. of output
stroke.
• Has an in-line adjuster to move the
conduit adjustment away from the
hydraulic or gas actuator.
• Designed to accept the M10 thread of
the gas lock or the conventional hydraulic lock rod thread.
• Materials used exceed the requiremetns in FAR 25.853 (a)*.
*
FAR 25.853 (a)
Cable Control Systems
• Low Profile push button input end.
• Push to release excutcheon for easy
installation.
• Output mates with hydraulic or gas
recline locks.
• Materials used exceed the requiremetns in FAR 25.853 (a)*.
ST-983-026-00
10
Pneumatics Systems Overview
• A system comprised of a pressure source
(pump) and one or more bladders
• Bladder - A sealed chamber or chambers
configured in such a way to inflate to a
desired shape when air pressure is introduced.
• Pump - Electric powered compressor utilized either a piston or diaphragm method of
providing air pressure.
• Control - A switch capable of selecting an
air circuit connected to a bladder. If an electric pump is utilized in the system the switch
is also capable of closing electrical contact
to energize the pump motor. When released, the switch rocker centers and simultaneously breaks electrical contact with the
pump and seals the circuit thereby keeping
the bladder at the selected pressure level.
Design Advantages
• Significant weight savings compared to mechanical systems, manual or powered.
• Bladder shapes can be varied to achive
support and or relief of pressure in critical
areas.
• Low power requirements.
• With the use of Semco Aerospace’ “Air
Wave” air sequencer, multiple bladders can
provide continuous changing of pressures
under the seat occupant greatly enhancing
comfort.
• Great versatility is possible through multiple
bladders and switches.
Pneumatics
11
BL-920-001-00
• Originally designed and produced
for the 1984 through 1994 Chevrolet
Sport Seats as the powered three
chamber lumbar support
• It allows individual adjustment of lumbar pressures in all three chambers
• Manufactured from high strength urethane sheet
• Mates with the Semco Aerospace
CT-920-001-02 lumbar switch/valve
assembly
BL-980-006-00
• This bladder assembly has a two
chambered accordion style providing
over four inches of inflated movement
for greater adjustment capability
• Easy mounting to the seat by means
of a semi-rigid bacvker plate.
• Manufactured from high strength urethane sheet
Pneumatics
12
PS-935-001-00
• 12-volt powered piston pump capable
of long continuous operation with low
current requirements and low heat
generation.
• The design provides a maximum
pressure of 8-10 psi.
SC-925-013-00
• Opens a pneumatic path from a pressure source as an accumulator to a
recieving chamber such as any of
Semco Aerospace’s Bladders.
• Actuating the switch rocker in one
direction will connect the pressure
source to the bladder.
• Actuating the switch in the other direction will close the path to the pressure source and open the bladder to
atmosphere resulting in a deflated
bladder
Pneumatics
13
SC-925-018-00
• Opens a pneumatic path from a pressure source such as an accumulator
to a recieving chamber such as any
of Semco Aerospace’s bladders.
• Actuating the switch in one direction
will connenct the pressure source to
the bladder.
• Actuating the switch in the other direction will close the path to the pressure source and open the bladder to
atmosphere resulting in a deflated
bladder
SC-925-100-00
• Opens a pneumatic path from a compressor to a recieving chamber such
as any of Semco Aerospace’s bladders.
• Also incorporates a single pole single
throw electric power to the compressor thereby simultaneously energizing
the compressor as the path is opened
to the bladder.
• Removing pressure from the rocker
will allow the rocker to return to the
neutral position closing the path from
the compressor to the bladder and
simultaneously stopping electrical
power to the compressor.
• Actuating the rocker in the other direction opens a path from the bladder
to atmosphere thereby deflating the
bladder.
Pneumatics
14
Motion Control Systems
Overview
• Semco Aerospace in partnership with Innovage Microsystems Inc.
• We design, develop, qualify and manufacture advanced rotary and linear actuators,
electronic units, and rugged power supplies
for demanding applications.
• Industries include: commercial and military
aircraft, as well as unmanned Optionally
Piloted Aircraft (OPA) among other land and
sea vehicles.
• Additional uses include commercial aircraft
interiors.
Design Advantages
• Actuator designs incorporate the following
unique characteristics:
- Anti-backlash and Low Friction Design - 6.5 inches per Sec - 7.50 Hz BW
- OPV or Redundant release with
Absolute Positioning Intact (Back-Driv
able)
- High Reliability Position Sensor 100M Cycles 0 12 Bit Resolution
- Actuator testing past 12 Million cycles at 65 continuous load
- Digitally adjustable end limits and mid-
point, without loss of stroke resolution
- High Load and trunion mount, pass through mounting available.
Motion Control Systems
15
Pax-Net Distribution
System
Aeronautical Power
Supply unit
• 3-channels of integrated central universal motor port +2 PAX-NET Distributed motion control ports
• Wide frequency and voltage bandwidth, PFC and EMI Filtered aircraft
power supplies
• Motion control pads, test interface
box’s wire harness’s and sensors
Motion Control Systems
• Distribution of 28VDC
Power and Differential
Serial Control: Async RS485, (CAN/LIN) or
Sync - (FlexRay)
• Compact and Ruggedized Construction
• “Wild-Frequency”
compatible power
input
• Fault protected
• USB and RS-232 Programming Interface’s
• In curcuit programming of seat motion
and control
• RS485 ARINC interface
• AUTO-Calibration of
eachseat axis
16
PA-989-000-00
• Anti-Backlash and Low Friction Design - 6.5 inches per sec - 7.50 Hz
BW
• OPV or Redundant release with Absolute Postioning intact (Back-Drivable)
• High Reliability Position Sensor 100M
Cycles - 12 Bit Resolution.
• Actuator Testing Weight Design. 185
LB Peak Intermittent Loads.
• Closed Loop Velocity and Position.
Flat versus Velocity Response.
• Digitally adjustable end limits and
midpoint, without loss of stroke resolution
PA-989-200-00
• High force linear actuator.
• Will output 2200 lbs over 7 inches of
stroke at _ in/sec speed.
• Current application is nose wheel
extension/retraction for Unmanned
Aircraft.
Motion Control Systems
17
PA-989-500-15
• A trunion mounted pass through linear actuator.
• Provides 5 inches of stroke and has
linear position sensing as well as a
cable actuated disconnect. The disconnect action requires a light actuation load and re-connects automatically when the cable is released.
• The actuator is locked when not energized and the lock is a positive mechanical lock not a friction lock brake
PA-989-550-17
• An example of our trunion
disconnect and a positive memount high load pass through
chanical lock when not enerdesign which incorporates the
gized.
controllwe in line with the motor • The stroke is 17 inches and the
allowing distributed connecacme screw is a 5/8” diameter
tions to the power supply
providing considerable column
• As with all of our actuators it is
bending resistane under high
equipped with a cable actuated
loads.
Motion Control Systems
18
PA-989-600-00
• The PA-600-00 is a rotary actuator and as with all of our actuators
is equipped with a high resolution
position sensor, a cable actuated
disconnect and postive mechanical
lock when not energized.
PA-989-700-00
• An ultra torque rotary actuator with
a 3 stage gear box with a triple gear
reduction.
• Equipped with a high-resolution position sensor, a cable actuated disconnect and a positive mechanical
lock when not actuated.
Motion Control Systems