Aircraft employ actuators for many types of functions, from opening and closing fan cowl hoods to thrust reversers. TRIUMPH Accessory Services - Grand Prairie has the capability to service ball-screw and hydraulic actuators.

Actuators

Heat Exchangers (Plate-Fin, Tube In-Shell, Conformal)

Thermal Solutions

Air Cycle Machine

Turbine Gearbox Assembly, Air Turbine Drive

Air Turbine Drive

TRIUMPH Mechanical Solutions manufactures latching devices for numerous industries and applications across the commercial, military, and industrial space. Our latches and keepers keep doors, cowls, and access panels closed and secured. We also manufacture latch mating keepers. 

Latches

TRIUMPH ACTUATION PRODUCTS & SERVICES - NORTH WALES

TRIUMPH ACTUATION PRODUCTS & SERVICES - SHELBYVILLE

TRIUMPH ACTUATION PRODUCTS & SERVICES - VILLENEUVE LE ROI, FRANCE

Provides mechanical solutions including design, development, manufacturer and support of highly engineered mechanical controls and components as well as production of complex mechanical assemblies using external designs for fixed wing and rotary commercial and military aircraft, naval vessels, military vehicles, nuclear power stations and industrial plants. Control cable applications include; vent, engine control, thrust reversers, and potable/waste water system controls.

TRIUMPH ACTUATION PRODUCTS & SERVICES- Heiligenhaus

Mechanical Control and Actuation Solutions

Flight Controls, PAX and Cargo doors, MLG & NLG Doors

Flight Controls and Airframe Structures

Toilet Assemblies, Vacuum Generators, Flush Valves

Blue Water Products

Reversers, Fan Cowls, Inlets, and Nozzles

Reversers, Fan cowls, Inlets and Nozzles

The TP85‐8 Air Drive Unit (ADU), also referred to as a Pneumatic Drive Turbine assembly, provides supplementary hydraulic power for the hydraulic system of an aircraft experiencing high load conditions. The turbine assemblies will also provide emergency hydraulic power should the engine‐driven hydraulic pumps onboard the aircraft fail to operate. The TP85‐8 ADU is driven by bleed air from the aircraft engine and is controlled by a three‐position control switch in the cockpit.

TP-85-8 Air Drive Unit

Air Drive Units

Based in West Hartford, Connecticut, TRIUMPH Systems, Electronics & Controls, is a leading independent aerospace fuel system supplier for the commercial, military, helicopter and business jet markets. Employing approximately 550 employees, the company’s key products and services include electronic engine controls, fuel metering units and main fuel pumps for both the OE and aftermarket/spares end markets.

TRIUMPH SYSTEMS ELECTRONICS & CONTROLS - WEST HARTFORD

Controls

TRIUMPH has manufactured over 100 Detector Drive Systems for PWR (pressure water reactor) and BWR (boiling water reactor) nuclear power stations worldwide and is committed to supporting the industry through innovative new system designs, retro-fit kits, spare parts, and on-going technical assistance.​ert text here. We also offer Mag-Iso valves which can be incorporated as an after-market addition to some DDS configurations or included as an à la carte offering for some DDS configurations of utilities considering a new installation(s).​

Nuclear Flus Mapping (Detector Drive Systems)

Detector Drive Units

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.

EMC-100 Electronic Control Unit

Electrical Control Units

Gear Boxes

A Plate Fin Heat Exchanger utilizes solid plates to conduct heat from one fluid flow path to heat transfer fins which then transfer heat to a second fluid. The heat transfer fin and plate construction add to the structural integrity of the heat exchanger, enabling it to withstand high pressures.

Hydraulics

Motors

Pumps

Anti-Ice Valves, Shut-off Valves, Check Valves, Temperature Control Valves

Valves

Wire ropes with customized end fitting, or MS Standard Wire Ropes

Bespoke wire rope solutions

Starter Generators, APU Generators, Main Generators (AC and DC), VSCF (Backup) Generators

Generators

Heat Exchangers, Oil Coolers, Precoolers, Reheaters, Condensers

Heat Transfer

The hydromechnical unit, HMU for short, is a critical component that functions to regulate fuel supplied to the fuel injectors based on the throttle position commanded and the state of operation of the engine.

Hydromechanical Unit (HMU)

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.

Power Transfer Unit (PTU)

Power Transfer Unit

Clemmons site designs, manufactures and supports hydraulic actuation and power generation products for the military and commercial aerospace industries.

TRIUMPH ACTUATION PRODUCTS & SERVICES - CLEMMONS

Hydraulic Power Generation & Pumps

The Stator is the stationary part of the AC Motor. The rotor is the rotating electrical component. The Assembly provides electrical power to various systems within the engine.

Stator Rotor

The Thrust Reverser Cowl Actuator (inboard) is a single-acting actuator used to open the thrust reverser cowl door on the 737 MAX engine nacelle. It includes integral extend locks which hold the door open once the actuator is extended. The actuator has one port for extension with retraction being accomplished by the cowl door weight.

Thrust Reverser Cowl Actuator (inboard)

Cowl Opening Actuator

The Alternate Landing Gear Extension Power Pack includes two separate channels of hydraulic power generation, each fed by independent DC electric motors, motor controllers, and hydraulic gear pumps. An integral manifold (containing various simple valves) and a spring loaded hydraulic reservoir are also included.

Power Pack, Alternate Landing Gear Extension

The Landing Gear Bypass Selector Valve controls the landing gear on the 737MAX Aircraft. The valve directs hydraulic pressure to the landing gear actuators, which extend or retract the landing gear, and bypasses flow from the retract chambers of the main and nose landing gear actuators when the manual extension system is operated. The valve contains 3 solenoid valves and 2 spool and sleeve valves.

Landing Gear Bypass Selector Valve

TRIUMPH is a recognized provider of telescoping hold open rods as well as fixed-length struts. These products range from simple rods to complex assemblies with single- or dual-action release collars, hydraulic damping in one or both directions, and fixed mono balls, or universal joint fittings. These products are mainly used to keep fan cowls, radomes, doors, thrust reversers, and maintenance panels in the open position.

Hold Open Rods

Landing Gear Systems (Struts, Actuation, Gear Door Control, Rolling Stock, Steering Systems, Plumbing and Wiring )

Landing Gear and Actuation Systems

Landing Gear & EMA-Systems Engineering, Design, Development, Test, Manufacture and Assembly

TRIUMPH ACTUATION PRODUCTS & SERVICES - SEATTLE

Landing Gear Actuation

Rotary Electromechanical Actuator and Controller High Frequency Response Motion Control

Electrical Mechanical Actuation

Steering Actutators

We Design, Manufacture, Assemble and Test Hydraulic Actuation Components for the Aerospace Industry.

TRIUMPH ACTUATION PRODUCTS & SERVICES - VALENCIA

Landing Gear Retract

Landing Gear Actutator

Body Main Landing Gear Truck Positioner 

Wing Main Landing Gear Truck Positioner

Truck Positioner

Ground Spoilers

Ground Spoiler Actuator

Arresting Hook System 

End of Stroke Damper

End of Stroke Damper

Upper Boost Actuators

Systems Electronics & Controls in Windsor, CT is a leading aerospace supplier for the commercial, military, helicopter and business jet markets. Employing approximately 110 employees, the company’s key products and services include nose wheel steering units, actuator assemblies, shimmy/lag dampers, and shock/strut assembles for both the OE and aftermarket/spares end markets. 

TRIUMPH SYSTEMS ELECTRONICS & CONTROLS - WINDSOR

Helicopter Actuation

Mission Systems Actuators 

- Weapons Trapeze & Ejection Actuators 
- Drag Chute Deploy and Release Actuators 
- RCM & EW Door Actuators 
- Arresting Hook Actuator/Dampers 
- Helicopter Gun 
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- Extend and/or Retract Lock 
- Shuttle valves for alternate system operation 
- Hydraulic/Pnuematic Operation 
- High Speed / High Performance Operation

Mission Systems Utility Actuators

Industry leader in aerospace hydraulic landing gear, landing gear door, and utility system actuation, as well as the industry leader in hydraulic fuses.

TRIUMPH ACTUATION PRODUCTS & SERVICES - YAKIMA

Nose Wheel Steering Systems - Linear Actuation

Landing Gear & Landing Gear Door Actuation 
- Push/Pull Actuators 
- Extend and/or Retract Locking Actuators 
- Retract Actuators 
- Sidestay Actuators 
- Drag Brace Actuators 
- Unlock / Alternate Extension System actuators 
- Bogie/Truck Position Actuators 
- Landing Gear Door Actuators

Landing Gear and Landing Gear Door Actuators

Engine Fuel Oil Heat Exchanger

Based in Forest, OH, with a satellite shop in Shelbyville, IN, TRIUMPH SEC, engineers, manufactures, tests and qualifies mission critical thermal and fluid management products, and provides aftermarket services for the most demanding aerospace and defense applications. Established in 1929, we are a worldwide manufacturer who believes in partnering with our Customers to integrate Advanced designs that meet or exceed their requirements and expectations. 

TRIUMPH SYSTEMS ELECTRONICS & CONTROLS - FOREST

The Cargo Ramp Lift Actuator has integral retract locking capabilities and is used to lift the CH47 Cargo Ramp.

Cargo Ramp Lift Actuator

Cargo Ramp Actuation

At TRIUMPH Geared Solutions, we offer proven experience and expertise in aircraft utility actuation components and systems. This diverse experience includes engine thrust reverser deployment, landing gear deployment, cargo and passenger door operation, radar antenna drives and in-flight refueling boom positioning. Other applications developed by TRIUMPH Geared Solutions include pilot seat positioning, fighter canopy opening and wing-fold systems for carrier aircraft.

Utility Actuation Components and Systems

Utility Actuation

Door Snubber

Nose Wheel Steering Unit and Steering Collar

Nose Wheel Steering (Push Pull and 360 Degree Turn)

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.

AFU 300 Auto Feather Unit

Autofeathering prop controls

Electrical Control Solutions

A fuel/oil heat exchanger and associated equipment is provided to maintain the hot engine oil in heat exchange relationship with the cool engine fuel.

Fuel Heat Exchanger

Hydraulic Cooling System

The reservoir is a tank in which an adequate supply of fluid for the system is stored. Fluid flows from the reservoir to the pump, where it is forced through the system and eventually returned to the reservoir.

Hydraulic Oil Tank

The system reservoir hold enough fluid for use in operation of the system and to replace fluid lost through minor leakage or evaporation. Reservoirs may also be Installed to provide a space for increase in fluid volume over the original amount, such as that which might occur through thermal expansion or foaming They also provide a place of escape for air trapped in the system.

Hydraulic Systems Overflow

It contains the oil pump, the scavenge and pressure inlet strainers, scavenge return connection, pressure outlet ports, an oil filter, and mounting bosses for the oil pressure gauge and temperature bulb connections.

Engine Oil Tank

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.

Cockpit Controls

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. 

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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​.

Cable Controls

Handles, quadrant, controls boxes. Tailor made solutions to fit in customers cockpit.

Control Boxes

Roller bearing controls, delivering linear motion between two points thru complex Airframe

Flexible captured ball bearing control cables

Complete Landing Gear System Design, Build and Test

Vehicle Landing Gear System Design and Build

Sliding Controls to deliver linear motion on short distances. Sustain high temperature and demanding environnement

Sliding Controls

The Hydraulic Start Motor is used to provide the output torque and shaft speed required for starting the V-22 Tiltrotor Aircraft main engines. The starter is comprised of a variable-displacement hydraulic motor with an integrally housed flow control valve and sprag clutch.

Hydraulic Start Motor

This hydraulic motor (also known as “Hydrive”) is a bi-directional, fixed displacement axial piston device which extracts energy from high pressure hydraulic fluid and transforms it into torque available at the output shaft. It is used on the General Dynamics Ordnance and Tactical Systems (GD-OTS) JSF gun system.

Hydraulic Motor

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.

Engine Driven Pumps

The EFP-630 or Engine Fuel Pump, is a combined high speed centrifugal main fuel pump and afterburner fuel pump system which delivers both gas generator and afterburner fuel flow. The main fuel pump consists of two centrifugal impellers in series for supplying gas generator flow. The afterburner fuel pump consists of a single centrifugal impeller and modulating throttle valve for supplying afterburner flow.

EFP-630 Engine Fuel Pump

Engine Fuel Pump

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.

Airframe Mounted Gearboxes (AMAD)

Airframe Mounted Gearboxes

TRIUMPH Geared Solutions is the premier independent supplier for the design and manufacture, as well as aftermarket spare parts and repair/overhaul support, of commercial & defense aerospace gearing components and Integrated gearboxes for fixed wing, rotorcraft, aircraft engine and ground vehicle applications. We collaborate with customers to provide a full array of capabilities including design, engineering and manufacturing of complex mechanical assemblies and build-to-print for highly specialized applications.

TRIUMPH GEARED SOLUTIONS - Park City

Gearbox System Design, Build, Overhaul

Accumulators 

Hydraulic Equipment

The Directional Control Valve is a 3-Way, 2-Position spool sleeve valve that is normally biased control (C1) to return (RTN). The valve is commanded to route flow/pressure from the PRS port to C1 by energizing a 28 Vdc nominal solenoid.

Directional Control Valve

TRIUMPH Mechanical Solutions is a leading provider of Remote Mechanical Valve Actuator (RMVA) Systems used in the Naval Defense industry. The purpose of a mechanical Remote Valve Operation (RVO) system is to provide a means of valve operation without the requirement of having a person physically located at the valve. A mechanical Remote Valve Operator system allows the remote valve operator to safely operate a valve located in a hazardous or hard-to–reach location. 

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Remote Mechanical Valve Actuators (RMVA) can be applied to a broad range of quarter or multi-turn applications. Remote Vent Valve Operators (RVVO) are designed specifically for quarter-turn ventilation applications. Remote Trip Valve Actuators (RTVA) are designed specifically for fast acting linear motion valves. ​

Remote Valve Operation

Brake Valve Assembly

Cargo Door System 

Ramp Door Control Valve

Control Valves

Landing Gear System 

Nose Landing Gear Steering Valve

Steering Valves

Arresting Hook System 

Hydraulic Isolation Valve

Hydraulic Isolation Valves

Gearbox

Ejection Seat Pitch Stabilization Control

Rudder, Aileron, and Elevator Booster Assembly

Rudder, Aileron and Elevator Booster Assembly

Hydraulic Rate Fuses 737 NG, 737 Max, 777/777X, 767, 747,KC-390

Hydraulic Fuses

Pneumatics Drive Units

Modern machining center for piece part fabrication and component repair capabilities including: 
- Fusion Welding and Brazing of exotic alloys 
- Heat Treatment 
- Precision Machining 
- Metal finishing 
- Non Destructive Tests

Machine Shop

Landing Gear Kinematics

Landing Gear Structure

Landing Gear Door Actuation

The Accessory Gearbox produces Hydraulic and Electrical power. Other Engine accessories such as starters, generators, fuel pumps, hydraulic pumps, oil pumps, speed sensors, etc. are also driven by the AGB. The Transfer and Inlet Gearboxes work in conjunction to provide power to the engine.

Accessory, Transfer and Inlet Gearbox

Includes Heat Exchangers, Landing Gear components, Power Transfer Units (PTU), Actuators, Precooler Covers, Mufflers, Engine Mounts, etc.

Aircraft Components

- Manufacturer: Zeiss 
- Measurement System: Renishaw PH10 
- Working Bed Volume: 1,5 meters by 1,2 meters by 0,9 meters (5 feet by 4 feet by 3 feet)

Fuel flow transmitters measure the flow rate of fuel through the component. As more fuel is flowed, more torque is applied to a turbine assembly. This torque creates distance between two magnetic pick-off’s which in turn creates distance between the electrical signal generated. The electrical signal is interpreted by a computer and a fuel flow rate is calculated.

Fuel Flow Transmitter

Aircraft fuel pumps are designed to move a significant volume of fuel from the tanks to the engine by way of the fuel system. They are shaft powered, employ a variety of motive means and require specialized test equipment to verify proper flow rates and volumes.

Fuel Pump

The Forward and Aft Engine Mounts are the components that attach and secure the Engine to the Wing Pylon. These Mounts are comprised of critical subcomponents that ensure the safety and reliability of the entire assembly.

FWD and AFT Engine

Integrated Drive Generator

Modern aircraft employ a wide range of types and sizes of bearings. Many ball and roller bearings can be inspected for defects and returned to service.

Main Engine, Gearbox, APU and Accessory Bearings

The air turbine engine starter is designed for direct attachment to and starting of the engine. Compressed air rotates the starter turbine and through its reduction gears and output section, sufficient torque is generated to accelerate the engine to starting speed.

Pneumatic Starter

Aircraft pneumatic valves control a wide range of engine and aircraft functions. The pneumaticaly operated starter valve controls the air upstream of the starter.

Starter Control Valve and IDG Shutoff Valve

Starters

The Turbine Clearance Control Valves are hydraulically actuated units that supply variable air flow to numerous components.

Turbine Clearance Control Valve

TRIUMPH Geared Solutions is a world leader in flight trim control, with a special focus on horizontal stabilizer trim actuation. Since 1955, TRIUMPH Gear Systems has designed, verified, manufactured and supported horizontal stabilizer trim actuators for six out of ten of the large commercial transport aircraft developed in the United States, including every large U.S. military transport. We are highly experienced in applying the key functional and structural elements that make horizontal stabilizer trim actuators some of the most challenging and critical items on an aircraft.

GEAR SOLUTIONS

GEARBOX SYSTEM DESIGN, BUILD, OVERHAUL

BUILD TO PRINT SOLUTIONS