Aircraft Gas Turbine Engine Front Frame Strut
Item Name Code (INC) 53246
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A rigid piece designed to resist pressure in the direction of its length. It is positioned between the inner and outer rings and is a main component of a FRAME, FRONT, AIRCRAFT GAS TURBINE ENGINE.
Additional Information for Aircraft Gas Turbine Engine Front Frame Strut
The Aircraft Gas Turbine Engine Front Frame Strut is a component that belongs to the supply class Gas Turbines And Jet Engines, Aircraft, Prime Moving; And Components in the supply group Engines, Turbines, And Components.
The front frame strut is a structural component that supports the front section of the gas turbine engine. It is typically made of high-strength materials such as titanium or steel to withstand the high loads and temperatures experienced during engine operation. The front frame strut connects the engine's front frame to the engine casing, providing stability and structural integrity to the engine assembly.
The front frame strut plays a crucial role in maintaining the alignment and balance of the engine components, ensuring smooth and efficient operation. It also helps to absorb and distribute the forces generated by the engine during operation, reducing vibrations and enhancing overall performance.
In summary, the Aircraft Gas Turbine Engine Front Frame Strut is an important component that provides structural support and stability to the front section of the gas turbine engine, contributing to its efficient and reliable operation.
Related Item Names for INC 53246 Aircraft Gas Turbine Engine Front Frame Strut
NATO Stock Numbers with Item Name 53246 Aircraft Gas Turbine Engine Front Frame Strut Page 1 of 1
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- JS30731
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