Nonaircraft Gas Turbine Engine Fan Disk And Hub

Nonaircraft Gas Turbine Engine Fan Disk and Hub are components used in gas turbine engines that are not designed for aircraft applications. These components are part of the fan section of the engine and are responsible for drawing in and compressing air before it enters the combustion chamber.

The fan disk is a circular component that houses the fan blades. It is typically made of a high-strength material, such as titanium, to withstand the high rotational speeds and loads experienced during operation. The fan blades are attached to the fan disk and are responsible for generating the airflow.

The hub is the central part of the fan disk that connects it to the engine shaft. It provides support and stability to the fan blades and ensures that they rotate in a synchronized manner. The hub is also designed to withstand the high centrifugal forces generated during operation.

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. They belong to the supply group Engines, Turbines, and Components, which includes various components and systems related to engines and turbines used in different applications.