RTX Corporation
Turbofan engine bearing and gearbox arrangement
Last updated:
Abstract:
A turbofan engine comprising a fan shaft configured to rotate about an axis of the engine. A fan drive gear system is configured to drive the fan shaft. A first spool comprises a high pressure turbine and a high pressure compressor. A second spool comprises a lower pressure turbine, a lower pressure compressor, and a shaft coupling the lower pressure turbine to the intermediate pressure compressor. The engine has a plurality of main bearings. The lower pressure compressor has a plurality of disks and a forward hub mounted to a forwardmost disk.
Status:
Grant
Type:
Utility
Filling date:
19 Dec 2018
Issue date:
10 Nov 2020