Triumph Aerospace Systems
Triumph Aerospace Systems - Newport News offers design, analysis, manufacture, instrumentation, assembly, and test support of aerospace prototype ground test and flight systems and components.
- (833) 359-9844
(610) 251-1000 - media@triumphgroup.com
- CustomerService@triumphgroup.com
- 555 E. Lancaster Avenue
Suite 400
Radnor, PA 19087
United States of America
Categories
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AFU 300 Auto Feather Unit
The Autofeather Unit (AFU), is mounted on the engine’s un-pressurized engine compartment, provides torque signal conditioning, automatic propeller feathering and remote engine uptrim command for Take-Off operations, as well as engine output torque indication to the aircraft cockpit during all engine operating conditions.
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Helicopter FADECs
The EMC-100 is dual channel Full Authority Digital Engine Control (FADEC) system, designed for helicopter turboshaft engines. The electronic control unit’s (ECU) primary channel provides precise engine power management and rotor speed control throughout the operational range of the engine. The reversionary backup channel provides full mission capability should a primary system failure occur.
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Engine Driven Pumps
This Engine Driven Pump is a variable displacement pump which extracts mechanical power from the gearbox accessory pad and converts it into hydraulic power available for use by the various actuators and other consumers on the AH-64 Apache aircraft. The maximum displacement of the pump is 0.182 CIPR and it is capable of providing 6 gpm of flow.
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Thurst Reverser Cowl Actuator
The Thrust Reverser Cowl Actuator is a single-acting telescoping actuator used to open the thrust reverser cowl doors on the A320neo engine nacelle. The actuator has one port for extension with retraction being accomplished by the cowl door weight. The inner piston includes a hydraulic lock feature that will stop the cowl door opening due to the wind load case of 40 knots pulling the door open.
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Electronic Engine Controls - FADEC
The EMC-100 is dual channel Full Authority Digital Engine Control (FADEC) system, designed for helicopter turboshaft engines. The electronic control unit’s (ECU) primary channel provides precise engine power management and rotor speed control throughout the operational range of the engine. The reversionary backup channel provides full mission capability should a primary system failure occur.
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MFP-570 Main Fuel Pump
The MFP-570 provides main engine burn flow as well as servo flow and engine actuator flow. This two-stage “cartridge type” fuel pump is designed to be inserted directly into the engine fuel metering unit.
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Flexible Captured Ball Bearing Control Cables
Roller bearing controls, delivering linear motion between two points thru complex Airframe.
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Airframe Mounted Gearboxes (AMAD)
Airframe mounted accessory drives (AMADs) — Every TRIUMPH Geared Solutions accessory drive is built to the highest standards of precision and reliability. The AMAD provides power for the aircraft’s hydraulic pumps, auxiliary fuel pumps and electrical generators. It also provides engine starting capability by transmitting power from auxiliary power units. Our AMADs incorporate carburized and ground gearing and, if the specification requires, AGMA Class 14 standards. Each drive is designed for high power density to minimize weight. Special features such as self-pressurizing lubrication systems assure proper operation at all altitudes within a given flight envelope. The AMADs also contain a disconnect feature which allows ground crews to disconnect the unit for maintenance and performance of electronic and hydraulic systems checks without the engine running.
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Cargo Ramp Lift Actuator
The Cargo Ramp Lift Actuator has integral retract locking capabilities and is used to lift the CH47 Cargo Ramp.
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Landing Gear And Actuation Systems
Landing Gear Systems (Struts, Actuation, Gear Door Control, Rolling Stock, Steering Systems, Plumbing and Wiring).
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