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.:

US 7721554 B1

PDF
Full Text
Expired
Date of Patent:
May. 25, 2010

Filed:

Feb. 02, 2006
Applicants:

Chellappa Balan, Niskayuna, NY (US);

Karl Edward Sheldon, Rexford, NY (US);

Inventors:

Chellappa Balan, Niskayuna, NY (US);

Karl Edward Sheldon, Rexford, NY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/04 (2006.01);
U.S. Cl.
CPC ...
Abstract

A non-aircraft-propelling auxiliary gas turbine engine installable in an aircraft having a cabin adapted to be pressurized. The auxiliary gas turbine engine includes an auxiliary-gas-turbine-engine compressor having an inlet, wherein the inlet is adapted to receive pressurized air from the cabin. A method for operating a non-aircraft-propelling auxiliary gas turbine engine of an aircraft includes providing pressurized air from the cabin of the aircraft to an inlet of a compressor of the auxiliary gas turbine engine. The method includes providing compressed air from the compressor to a combustor of the auxiliary gas turbine engine and includes providing combustion gases from the combustor to a turbine of the auxiliary gas turbine engine, wherein the turbine is mechanically coupled to the compressor.


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Balan, Chellappa. (2010). Aircraft auxiliary gas turbine engine and method for operating (U.S. Patent No. 7721554). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/7721554

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