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. 09, 2021

Filed:

Oct. 24, 2017
Applicant:

GE Aviation Systems Limited, Cheltenham, GB;

Inventors:

Michael David Bailey, Tewkesbury, GB;

Colin John Halsey, Tewkesbury, GB;

Assignee:

GE Aviation Systems Limited, Cheltenham, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02J 7/00 (2006.01); H01M 10/44 (2006.01); H01M 10/46 (2006.01); B64D 41/00 (2006.01); H01M 8/0612 (2016.01); H01M 8/0656 (2016.01); H01M 8/04082 (2016.01); H01M 8/04828 (2016.01); H01M 16/00 (2006.01); H01M 8/086 (2016.01); H01M 8/1018 (2016.01); H01M 8/124 (2016.01); H01M 8/083 (2016.01); H01M 8/14 (2006.01); H01M 8/18 (2006.01);
U.S. Cl.
CPC ...
B64D 41/00 (2013.01); H01M 8/0494 (2013.01); H01M 8/04201 (2013.01); H01M 8/0612 (2013.01); H01M 8/0618 (2013.01); H01M 8/0656 (2013.01); H01M 16/003 (2013.01); B64D 2041/005 (2013.01); B64D 2221/00 (2013.01); H01M 8/083 (2013.01); H01M 8/086 (2013.01); H01M 8/184 (2013.01); H01M 2008/1095 (2013.01); H01M 2008/1293 (2013.01); H01M 2008/147 (2013.01); H01M 2250/20 (2013.01); Y02E 60/50 (2013.01); Y02T 50/50 (2013.01); Y02T 90/40 (2013.01);
Abstract

Systems and methods for providing power to one or more loads on an aircraft are provided. A power system for an aircraft can include a first fuel cell configured to provide base power to one or more loads on the aircraft. The power system can further include a second fuel cell configured to provide peak power to the one or more loads on the aircraft. The peak power can be a power exceeding the base power. The power system can further include an energy storage device configured to provide transient power to the one or more loads on the aircraft. The transient power can be a power exceeding the peak power. The power system can further include a controller configured to control delivery of power from the first fuel cell, the second fuel cell, and the energy storage device to the one or more loads on the aircraft.


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