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:
Oct. 06, 2020

Filed:

Mar. 15, 2017
Applicants:

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

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

Inventors:

Mat French, Avon, IN (US);

John T. Alt, Zionsville, IN (US);

Mark J. Blackwelder, Plainfield, IN (US);

Assignees:

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

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02P 9/48 (2006.01); F02C 9/00 (2006.01); F02C 7/32 (2006.01); H02K 7/18 (2006.01); F01D 15/10 (2006.01); F02C 7/36 (2006.01); H02J 9/06 (2006.01); F02C 7/268 (2006.01); B81B 7/02 (2006.01); B81C 1/00 (2006.01); F02K 3/06 (2006.01); F02N 11/08 (2006.01); H02P 101/30 (2015.01); H02P 101/25 (2016.01); H02J 1/10 (2006.01); H02J 3/30 (2006.01); H02J 3/32 (2006.01); H02J 1/16 (2006.01); H02J 3/38 (2006.01);
U.S. Cl.
CPC ...
H02P 9/48 (2013.01); B81B 7/02 (2013.01); B81C 1/00158 (2013.01); B81C 1/00301 (2013.01); F01D 15/10 (2013.01); F02C 7/268 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F02C 9/00 (2013.01); F02K 3/06 (2013.01); F02N 11/0862 (2013.01); H02J 9/061 (2013.01); H02K 7/1823 (2013.01); B81B 2201/0257 (2013.01); B81B 2201/0264 (2013.01); F05B 2220/706 (2013.01); F05D 2220/76 (2013.01); F05D 2270/62 (2013.01); H02J 1/102 (2013.01); H02J 1/16 (2013.01); H02J 3/30 (2013.01); H02J 3/32 (2013.01); H02J 3/38 (2013.01); H02P 2101/25 (2015.01); H02P 2101/30 (2015.01);
Abstract

A gas turbine engine includes first and second electrical machines coupled to the gas turbine engine, each of the first and second electrical machines electrically coupled to both a primary electrical bus and a secondary electrical bus. The gas turbine includes a first controller configured to control operation of the gas turbine engine, and a second controller coupled to the first controller, the second controller configured to respond to control inputs from the first controller and control an electrical output of the first and second electrical machines to the primary and secondary electrical busses. A converter controller is coupled to an energy storage system, the second controller, the primary electrical bus, and the secondary electrical bus.


Find Patent Forward Citations

Loading…