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
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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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Landing Gear And Actuation Systems
Landing Gear Systems (Struts, Actuation, Gear Door Control, Rolling Stock, Steering Systems, Plumbing and Wiring).
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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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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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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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Nose Wheel Steering Unit And Steering Collar
Nose Wheel Steering Unit and Steering Collar for the V-22 Osprey.
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Control Cables
TRIUMPH specializes in cable controls which are mechanical connections between controls and actuation systems used in a variety of applications. Our systems provide higher reliability, lighter weight, and greater control box selection. Current controls include wire rope, push-pull controls, sliding friction controls, ball-bearing controls and low-resistance and backlash mechanical control system cables. Wire Rope Controls: Wire Rope is used in applications where weight is critical, and the system operates in tension only. Assemblies are built to your required standards with unlimited configuration capabilities. Sliding Friction Controls: High load capacity in tension and compression. Flexible in any direction, wide temperature range and easy installation. No adjustment or lubrication needed during the life of the control. Ball Bearing Controls: Ball Bearing controls are a self-contained system that performs linear motion under tension or compression loads.Precise and accurate movement with high load capacity offering weight savings, low friction and high efficiency. Quick disconnect ends available.
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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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Power Transfer Unit
The PTU is a bi-directional, back to back, variable/fixed displacement unit, with a differential pressure compensated displacement control. Displacement of the variable displacement unit is varied to maintain the required running and breakout pressure differential between the yellow and green systems.
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Cockpit Controls
TRIUMPH Mechanical Solutions produces cockpit controls and quadrants specifically designed to meet unique customer requirements. Our Electro-Mechanical Cockpit modules are frequently married to our push/pull controls to produce combined output devices. For example, a throttle quadrant with switch/transducer outputs and mechanical cable connections to an engine control system.
