The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 25, 2022

Filed:

Jun. 29, 2020
Applicant:

Rolls-royce Plc, London, GB;

Inventor:

Jonathan P Bradley, Derby, GB;

Assignee:

ROLLS-ROYCE PLC, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 15/10 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); F01D 25/162 (2013.01); F01D 25/166 (2013.01);
Abstract

An aircraft gas turbine engine () comprises a main engine spool () and a bearing arrangement () configured to rotatably support the main engine spool (). The bearing arrangement () includes a damper () comprising a static element () and a moveable element (). The gas turbine engine further comprises an electric machine () comprising a rotor () and a stator (). The rotor () is mounted to the main engine spool (), and the stator () is mounted to the moveable element () of the damper to be moveable with the moveable element ().


Find Patent Forward Citations

Bradley, Jonathan. (2022). Gas turbine engine electrical generator (U.S. Patent No. 11230941). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11230941

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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