Nonaircraft Gas Turbine Engine Compressor Disk And Hub

Nonaircraft Gas Turbine Engine Compressor Disk and Hub are components used in gas turbine engines that are not intended for aircraft applications. These components are part of the compressor section of the engine and play a crucial role in the compression of air before it enters the combustion chamber.

The compressor disk is a rotating component that contains multiple blades or vanes attached to it. As the disk rotates, the blades compress the incoming air, increasing its pressure and temperature. This compressed air is then directed to the combustion chamber for the combustion process.

The hub, on the other hand, is the central part of the compressor disk that connects it to the engine shaft. It provides support and stability to the rotating disk and ensures that it operates smoothly and efficiently.

These components are classified under the supply class Gas Turbines and Jet Engines, specifically in the category of Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, and Components. This supply group encompasses various engines, turbines, and their associated components used in non-aircraft applications, such as power generation, industrial processes, and marine propulsion.