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:
Feb. 23, 2021

Filed:

Sep. 14, 2017
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Marko Bacic, Oxford, GB;

Benjamin J. Sellers, Bath, GB;

Rory D. Stieger, Derby, GB;

Assignee:

ROLLS-ROYCE PLC, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 13/04 (2006.01); F04D 27/02 (2006.01); B64D 27/16 (2006.01); F02C 7/32 (2006.01); F04D 25/02 (2006.01); F04D 27/00 (2006.01); B64D 13/06 (2006.01);
U.S. Cl.
CPC ...
B64D 13/04 (2013.01); B64D 27/16 (2013.01); F02C 7/32 (2013.01); F04D 25/02 (2013.01); F04D 27/002 (2013.01); F04D 27/0261 (2013.01); B64D 2013/0603 (2013.01); F05D 2220/323 (2013.01); F05D 2260/40 (2013.01); F05D 2270/101 (2013.01); F05D 2270/30 (2013.01); Y02T 50/60 (2013.01);
Abstract

A control system for use in controlling a cabin blower system. The cabin blower system includes a gas turbine engine spool, a cabin blower compressor powered by the spool and arranged in use to compress fluid used in a cabin of an aircraft, and one or more control mechanisms via which the control system controls the power extracted by the cabin blower compressor from the spool. The control system is arranged in use to control the power extracted from the spool by the cabin blower compressor in accordance with one or more primary control parameters. The control system is arranged in use to alter the spool power extracted by the cabin blower compressor by comparison with the power that would have been extracted in accordance with the primary control parameters alone, in response to modifications in a secondary control parameter indicative of the commencement or occurrence of an engine transient.


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