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:
Dec. 21, 2021

Filed:

Aug. 11, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Edward Brinson, Mason, OH (US);

Paul Robert Gemin, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 15/00 (2006.01); F01D 15/12 (2006.01); F02C 7/32 (2006.01); F02C 7/12 (2006.01); F02C 7/36 (2006.01); B64D 13/06 (2006.01); B64D 27/10 (2006.01); F01D 5/02 (2006.01); F01D 11/24 (2006.01); F01D 13/00 (2006.01); F01D 13/02 (2006.01); F04D 29/32 (2006.01); F04D 29/58 (2006.01); F25B 9/00 (2006.01); F25B 9/10 (2006.01); F25B 9/14 (2006.01);
U.S. Cl.
CPC ...
F01D 15/12 (2013.01); B64D 13/06 (2013.01); B64D 27/10 (2013.01); F01D 5/02 (2013.01); F01D 11/24 (2013.01); F01D 13/003 (2013.01); F01D 13/006 (2013.01); F01D 13/02 (2013.01); F02C 7/12 (2013.01); F02C 7/32 (2013.01); F02C 7/36 (2013.01); F04D 29/321 (2013.01); F04D 29/5826 (2013.01); F25B 9/004 (2013.01); F25B 9/008 (2013.01); F25B 9/10 (2013.01); F25B 9/14 (2013.01); B64D 2013/0618 (2013.01); F05D 2220/323 (2013.01); F05D 2240/24 (2013.01); F05D 2240/60 (2013.01); F05D 2260/213 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/606 (2013.01); F25B 2309/004 (2013.01); F25B 2309/005 (2013.01); Y02T 50/60 (2013.01);
Abstract

The present disclosure is directed to an aircraft power generation system including a reverse Brayton cycle system, a gas turbine engine, and a gearbox. The gas turbine engine includes a compressor section, a turbine section, and an engine shaft. The compressor section is arranged in serial flow arrangement with the turbine section. The engine shaft is rotatable with at least a portion of the compressor section and with at least a portion of the turbine section. The reverse Brayton cycle system includes a compressor, a driveshaft, a turbine, and a first exchanger. The driveshaft is rotatable with the compressor or the turbine, and the compressor, the first heat exchanger, and the turbine are in serial flow arrangement. The gearbox is configured to receive mechanical energy from the engine shaft and transmit mechanical energy to the reverse Brayton cycle system through the driveshaft.


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