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:
Feb. 02, 2021

Filed:

Apr. 30, 2019
Applicant:

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

Inventors:

Stephen Andrew Long, Carmel, IN (US);

Dwayne Bevis, Bloomington, IN (US);

Graham Burkholder, Indianapolis, IN (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 15/10 (2006.01); F02C 7/36 (2006.01); B64D 27/02 (2006.01); B64D 31/06 (2006.01); B64D 27/10 (2006.01); F02C 6/00 (2006.01); F01D 17/24 (2006.01);
U.S. Cl.
CPC ...
F01D 15/10 (2013.01); B64D 27/02 (2013.01); B64D 27/10 (2013.01); B64D 31/06 (2013.01); F01D 17/24 (2013.01); F02C 6/00 (2013.01); F02C 7/36 (2013.01); B64D 2027/026 (2013.01); F05D 2220/323 (2013.01); F05D 2270/13 (2013.01); F05D 2270/20 (2013.01);
Abstract

A method for operation of a hybrid propulsion system is provided that includes providing a hybrid propulsion system including a gas turbine engine, an electrical system, and a controller configured to cause the gas turbine engine to produce a first mechanical power output and to cause the electrical system to produce a second mechanical power output. The method further includes causing the gas turbine engine to produce the first mechanical power output and causing the electrical system to produce the second mechanical power output, which causes a drive shaft of the gas turbine engine to rotate. The method further includes decreasing production of the first mechanical power output when a combination of the first mechanical power output and the second mechanical power output for take-off or climb is a predetermined percentage of a predetermined parameter of the gas turbine engine.


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