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. 23, 2022

Filed:

Jul. 03, 2019
Applicant:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Inventor:

Adam Woods, Suffield, CT (US);

Assignee:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/00 (2006.01); F02C 9/18 (2006.01); B64D 13/02 (2006.01); B64D 13/06 (2006.01); B64D 13/08 (2006.01); B64D 15/04 (2006.01); B64D 27/14 (2006.01);
U.S. Cl.
CPC ...
F02C 9/18 (2013.01); B64D 13/02 (2013.01); B64D 13/06 (2013.01); B64D 13/08 (2013.01); B64D 15/04 (2013.01); B64D 27/14 (2013.01); B64D 2013/0607 (2013.01); B64D 2013/0618 (2013.01); F05D 2220/323 (2013.01);
Abstract

An architecture for powering systems on an aircraft has a gas turbine engine including a main compressor, a combustor, and a turbine. The turbine powers the main compressor, and further powers a propulsor. The turbine is operably connected to drive a generator. The generator is connected to store generated power at a battery. The battery is connected to provide power to a motor from the propulsor such that the propulsor can be selectively driven by both the motor and the turbine. A bleed air control system and a tap for selectively tapping compressed air from the main compressor, and a control valve for delivering at least one of the tapped compressed air or a compressed alternative air to bleed systems on an associated aircraft. An electric bleed compressor selectively compresses the compressed alternative air. The electric bleed compressor is powered by the battery. A control for controlling the control valve to selectively deliver at least one of the tapped compressed air and the compressed alternative air to the bleed systems. An aircraft is also disclosed.


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