Aircraft Gas Turbine Engine Front Frame

The Aircraft Gas Turbine Engine Front 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 front frame of an aircraft gas turbine engine is a structural component that houses various important components of the engine, including the compressor, combustion chamber, and accessory gearbox. It provides support and structural integrity to these components, ensuring their proper functioning and alignment.

The front frame also plays a crucial role in directing the airflow through the engine, optimizing the engine's performance and efficiency. It is designed to withstand high temperatures, pressures, and vibrations that are typical in gas turbine engines.

Overall, the front frame of an aircraft gas turbine engine is a critical component that contributes to the reliable and efficient operation of the engine.