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. 01, 2022

Filed:

May. 24, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Vasileios Kyritsis, Derby, GB;

Maurice Bristow, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 9/28 (2006.01); B64C 21/02 (2006.01); G01M 15/14 (2006.01); F02K 1/30 (2006.01); F02K 1/17 (2006.01);
U.S. Cl.
CPC ...
F02C 9/28 (2013.01); B64C 21/02 (2013.01); B64C 2230/06 (2013.01); F02K 1/17 (2013.01); F02K 1/30 (2013.01); F05D 2260/80 (2013.01); G01M 15/14 (2013.01);
Abstract

A control system operable includes a modified primary control parameter for an aircraft, the control system includes: a primary control parameter leg configured to output a demand in an aircraft primary control parameter; a primary control parameter compensation leg configured to receive a change in absolute levels and/or spatial distributions of swirl angle and/or fan pressure at a primary control parameter relative to a reference and convert the change into the primary control parameter; a processor adapted to receive the demand in the primary control parameter output from the primary control parameter leg and the change to the primary control parameter output from the primary control parameter compensation leg; compare the demand in the primary control parameter output from the primary control parameter leg and the change to the primary control parameter output from the primary control parameter compensation leg; and generate a modified primary control parameter for the aircraft.


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