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:
Apr. 30, 2019

Filed:

Mar. 06, 2017
Applicants:

Rolls-royce Corporation, Indianapolis, IN (US);

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

Inventors:

Jonathan S. Sands, Clayton, IN (US);

Ryan C. Humes, Indianapolis, IN (US);

Assignees:

Rolls-Royce Corporation, Indianapolis, IN (US);

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 35/08 (2006.01); B64D 31/06 (2006.01); B63H 23/12 (2006.01); B64D 31/00 (2006.01); F02B 63/04 (2006.01); F01D 15/10 (2006.01); F01D 15/12 (2006.01); F01D 21/00 (2006.01); B64D 27/24 (2006.01); B64D 35/04 (2006.01); F02D 25/04 (2006.01); B64D 27/02 (2006.01); B64D 31/14 (2006.01);
U.S. Cl.
CPC ...
B64D 35/08 (2013.01); B63H 23/12 (2013.01); B64D 27/02 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B64D 31/06 (2013.01); B64D 31/14 (2013.01); B64D 35/04 (2013.01); F01D 15/10 (2013.01); F01D 15/12 (2013.01); F01D 21/003 (2013.01); F02B 63/04 (2013.01); F02D 25/04 (2013.01); B64D 2027/026 (2013.01); F05D 2220/32 (2013.01);
Abstract

A propulsion system that includes a plurality of power units, a plurality of propulsors, where respective power units of the plurality of power units are controllably coupled to the plurality of propulsors, and a controller configured to receive a desired throttle value corresponding to a desired propulsive force, determine a number of power units of the plurality of power units to be coupled to the plurality of propulsors to achieve the desired propulsive force based on a respective power value associated with each respective power unit of the plurality of power units, and cause the number of power units of the plurality of power units to be coupled to the plurality of propulsors.


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