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