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:
Jul. 09, 2024

Filed:

Mar. 24, 2023
Applicant:

GE Aviation Systems Llc, Grand Rapids, MI (US);

Inventors:

Kevin P. Hallisey, Ave Maria, FL (US);

Dominique Patrick Sautron, Chicago, IL (US);

Assignee:

GE Aviation Systems LLC, Grand Rapids, MI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); B64D 13/06 (2006.01); B64D 27/10 (2006.01); B64D 29/00 (2006.01); F04D 27/02 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); B64D 13/06 (2013.01); B64D 27/10 (2013.01); B64D 29/00 (2013.01); F04D 27/0207 (2013.01); B64D 2013/0618 (2013.01); F05D 2260/606 (2013.01);
Abstract

A combustion engine including a combustion chamber, a first bleed air supply, a second bleed air supply, a thermal bus and a turbomachine. The first bleed air supply being fluidly coupled to a first fluid from a portion of the combustion engine upstream of the combustion chamber. The second bleed air supply being fluidly coupled to a second fluid portion of the combustion engine downstream of the combustion chamber. The turbomachine having a compressor and a turbine. The compressor being fluidly coupled to the first bleed air supply. The turbine being fluidly coupled to the second bleed air supply.


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