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. 03, 2019

Filed:

Jan. 25, 2017
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Glenn A Knight, Belper, GB;

Alan R Maguire, Derby, GB;

Richard Sharpe, Leek, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 13/00 (2006.01); F01D 13/00 (2006.01); F01D 17/16 (2006.01); F02C 7/277 (2006.01); F02C 7/32 (2006.01);
U.S. Cl.
CPC ...
B64D 13/00 (2013.01); F01D 13/00 (2013.01); F01D 17/16 (2013.01); F02C 7/277 (2013.01); F02C 7/32 (2013.01); F05D 2220/323 (2013.01); F05D 2260/406 (2013.01); F05D 2260/85 (2013.01);
Abstract

An aircraft cabin blower system is described having a hydraulic circuit comprising a first hydraulic device and a second hydraulic device. The first hydraulic device is mechanically coupled to a cabin blower compressor and the second hydraulic device is arranged in use to be mechanically coupled to a spool of a gas turbine engine. The first hydraulic device is capable of performing as a hydraulic motor and the second hydraulic device is capable of performing as a hydraulic pump. When, in use, the system is operating in a cabin blower configuration, a driving force supplied by the spool of the gas turbine causes the second hydraulic device to pump liquid provided in the hydraulic circuit and thereby to drive the first hydraulic device, which in turn rotates the cabin blower compressor.


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