Aircraft Gas Turbine Engine Compressor Frame
Item Name Code (INC) 52339
Additional Information for Aircraft Gas Turbine Engine Compressor Frame
The Aircraft Gas Turbine Engine Compressor 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 compressor frame is a structural component of a gas turbine engine that houses the compressor stages. It provides support and stability to the compressor blades and other internal components. The compressor frame is typically made of high-strength materials such as titanium or steel to withstand the high temperatures and pressures experienced in the engine.
The compressor stages within the frame are responsible for compressing incoming air, increasing its pressure and temperature before it enters the combustion chamber. This compressed air is then mixed with fuel and ignited to produce the high-temperature, high-pressure gases that drive the turbine and ultimately provide thrust or power for the aircraft.
The compressor frame plays a crucial role in the overall performance and efficiency of the gas turbine engine. It must be designed and manufactured to strict tolerances to ensure proper alignment and sealing of the compressor stages. Any deviations or damage to the compressor frame can lead to reduced engine performance or even failure.
In summary, the Aircraft Gas Turbine Engine Compressor Frame is a vital component of a gas turbine engine, providing support and stability to the compressor stages. It is part of the larger supply class Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components in the supply group Engines, Turbines, And Components.
Related Item Names for INC 52339 Aircraft Gas Turbine Engine Compressor Frame
NATO Stock Numbers with Item Name 52339 Aircraft Gas Turbine Engine Compressor Frame Page 1 of 1
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