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. 03, 2026

Filed:

Aug. 25, 2022
Applicant:

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

Inventors:

Stephen Andrew Long, Indianapolis, IN (US);

Michael Dougherty, Indianapolis, IN (US);

Tomasz Marek Lubecki, Singapore, SG;

Firman Sasongko, Singapore, SG;

Chandana Jayampathi Gajanayake, Singapore, SG;

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H01M 10/60 (2014.01); B64D 27/10 (2006.01); B64D 33/08 (2006.01); G05B 19/416 (2006.01); G05D 16/20 (2006.01); G05D 23/19 (2006.01); H01M 10/613 (2014.01); H01M 10/625 (2014.01); H01M 10/63 (2014.01); H01M 10/6568 (2014.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
H01M 10/60 (2015.04); B64D 27/10 (2013.01); B64D 33/08 (2013.01); G05B 19/416 (2013.01); G05D 16/2066 (2013.01); G05D 23/1917 (2013.01); H01M 10/613 (2015.04); H01M 10/625 (2015.04); H01M 10/63 (2015.04); H01M 10/6568 (2015.04); B64D 27/026 (2024.01); G05B 2219/37371 (2013.01); G05B 2219/49215 (2013.01); H01M 2220/20 (2013.01);
Abstract

A thermal management system for an energy storage system for an aircraft includes a pump circulating a thermal management fluid through the thermal management system and an energy storage device of the aircraft. A controller circuitry may control a variable pumping capacity of the pump based on sensing pressure or temperature of the thermal management fluid at the energy storage device. The controller circuitry may default operation of the pump to a first pumping capacity in response to the pressure or temperature being within a predetermined operating range and a predetermined failure condition or a power demand of an aircraft engine supply bus exceeding a predetermined threshold. The controller controlling operation of the pump to a second pumping capacity in response to absence of the power demand signal of the aircraft engine supply bus and the pressure or temperature being within the predetermined operating range.


Find Patent Forward Citations

Long, Stephen. (2026). Aircraft thermal management system for an energy storage system (U.S. Patent No. 12567613). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12567613

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

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