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:
Mar. 29, 2022

Filed:

Sep. 14, 2018
Applicant:

Rolls-royce North American Technologies Inc., Indianapolis, IN (US);

Inventors:

Kyle Klein, Indianapolis, IN (US);

Michael Karam, Plainfield, IN (US);

Jonathan Sands, Clayton, IN (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/20 (2006.01); F02K 3/06 (2006.01); F02K 1/66 (2006.01);
U.S. Cl.
CPC ...
F02C 9/20 (2013.01); F02K 3/06 (2013.01); F02K 1/66 (2013.01); F05D 2220/323 (2013.01); F05D 2270/05 (2013.01); F05D 2270/07 (2013.01); F05D 2270/08 (2013.01); F05D 2270/101 (2013.01); F05D 2270/112 (2013.01); F05D 2270/333 (2013.01);
Abstract

A gas turbine engine includes a fan and an engine core that includes a compressor, a combustor, and a turbine. The fan and the compressor include variable pitch geometry. The gas turbine engine further includes a control system configured to adjust the variable pitch geometry of the fan and the compressor to optimize a performance characteristic of the gas turbine engine.


Find Patent Forward Citations

Klein, Kyle. (2022). Gas turbine engine with variable pitch fan and variable pitch compressor geometry (U.S. Patent No. 11286865). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/11286865

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

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