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:
May. 14, 2024

Filed:

Aug. 14, 2023
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Paul R Davies, Bristol, GB;

David A Jones, Bristol, GB;

Alexander T Joyce, Derby, GB;

Richard G Mochrie, Guildford, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/16 (2006.01); F25B 27/02 (2006.01); F02C 6/18 (2006.01);
U.S. Cl.
CPC ...
F02C 7/16 (2013.01); F25B 27/02 (2013.01); F02C 6/18 (2013.01); F05D 2220/323 (2013.01); F05D 2260/213 (2013.01);
Abstract

A thermal management system for an aircraft comprises a first gas turbine engine, a first thermal bus, a first heat exchanger, and a chiller. The first thermal bus comprises a first heat transfer fluid, with the first heat transfer fluid being in fluid communication, in a closed loop flow sequence, between the first gas turbine engine, the first heat exchanger, and the chiller. Waste heat energy generated by the first gas turbine engine, is transferred to the first heat transfer fluid. The chiller is configured to lower a temperature of the first heat transfer fluid prior to the first heat transfer fluid being circulated through the gas turbine engine. The first heat exchanger is configured to transfer the waste heat energy from the first heat transfer fluid to a dissipation medium.


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