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:
Jun. 16, 2026

Filed:

Nov. 06, 2020
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:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/18 (2006.01); F02C 5/12 (2006.01); F02C 7/143 (2006.01);
U.S. Cl.
CPC ...
F02C 5/12 (2013.01); F02C 7/143 (2013.01); F02C 9/18 (2013.01); F05D 2220/323 (2013.01); F05D 2240/35 (2013.01); F05D 2260/606 (2013.01);
Abstract

A combustion engine including at least one combustion chamber, a first bleed air supply fluidly coupled to a portion of the combustion engine upstream the combustion chamber, a second bleed air supply fluidly coupled to a portion of the combustion engine downstream the combustion chamber, and a turbomachine comprising a first compressor, a second compressor, and a first turbine mounted to a common shaft, with the first and second compressors in serial flow arrangement. The turbomachine, further comprising an intercooler serially fluidly coupling a portion of the first compressor to a portion of the second compressor.


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