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.
Patent No.:
Date of Patent:
Apr. 04, 2023
Filed:
Jun. 29, 2021
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); B64D 27/10 (2006.01); B64D 29/00 (2006.01); F04D 27/02 (2006.01); B64D 13/06 (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 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, a first thermal bus, and a turbomachine including a compressor, a rotary pump, and a first turbine, with the compressor and rotary pump in serial flow arrangement and the rotary pump being fluidly coupled to the first thermal bus.