Aircraft Gas Turbine Engine Rear Frame

The Aircraft Gas Turbine Engine Rear Frame is a component that is part of the supply class Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components in the supply group Engines, Turbines, And Components.

The rear frame of an aircraft gas turbine engine is a structural component that provides support and housing for various engine systems and components. It is typically located at the aft end of the engine and connects to the engine casing or nacelle.

The rear frame plays a crucial role in maintaining the structural integrity of the engine and supporting the loads generated during operation. It also helps to direct the flow of exhaust gases and provides attachment points for other engine components, such as the exhaust nozzle and thrust reverser.

In addition to its structural function, the rear frame may also house various systems and components, such as the engine control unit, fuel nozzles, and accessory gearbox. These systems and components are essential for the proper operation and performance of the gas turbine engine.

Overall, the Aircraft Gas Turbine Engine Rear Frame is an important component that contributes to the safe and efficient operation of aircraft gas turbine engines.