Model: 6887113

Special Features:

30 blades equally spaced on outer periphery; tapered od, 7.51 min 7.512 max in. Largest od; 10 slots equally spaced on outer periphery; 1.159 min 1.1595 max in. Id

Properties:

A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the rotor, compressor, aircraft gas turbine engine and/or the rotor, fan, aircraft gas turbine engine through a shaft, turbine, aircraft gas turbine engine. It consists of disks, blades, hubs, and the like. It is the moving part of a turbine assembly, aircraft gas turbine engine. It has facilities for attaching to a shaft, turbine, aircraft gas turbine engine.