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:
Aug. 27, 2019

Filed:

Mar. 07, 2017
Applicant:

Rolls-royce Corporation, Indianapolis, IN (US);

Inventor:

Michael Abraham Karam, Plainfield, IN (US);

Assignee:

ROLLS-ROYCE CORPORATION, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/16 (2006.01); F02K 3/06 (2006.01); B64D 41/00 (2006.01); H02K 7/18 (2006.01);
U.S. Cl.
CPC ...
F02C 6/16 (2013.01); B64D 41/00 (2013.01); F02K 3/06 (2013.01); H02K 7/1823 (2013.01); F05D 2220/50 (2013.01); F05D 2220/76 (2013.01); F05D 2260/42 (2013.01); Y02E 60/15 (2013.01); Y02T 50/53 (2013.01);
Abstract

A system for providing auxiliary power in an aircraft. A propulsion core comprises a compressor, a combustor, a turbine, and a shaft. An accessory unit comprises an accessory combustor, an accessory turbine, and an accessory shaft. A tank is configured to hold high pressure air and operably connected to the accessory unit. An electric generator comprises an electrical output and a mechanical input, with the mechanical input operably connected to the accessory shaft and the electrical output operably connected to an electric motor operably connected to the shaft. The electrical output is operably connected to an auxiliary power consuming device in the aircraft.


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