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:
Jun. 26, 2018

Filed:

Apr. 16, 2015
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

Alasdair Gardner, Derby, GB;

Arthur Laurence Rowe, Derby, GB;

Mark David Taylor, Derby, GB;

Nicholas Howarth, Derby, GB;

Assignee:

ROLLS-ROYCE plc, London, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 9/22 (2006.01); F01D 17/16 (2006.01); F02C 9/20 (2006.01); F02C 9/54 (2006.01); F02C 6/00 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 9/22 (2013.01); F01D 17/162 (2013.01); F02C 6/00 (2013.01); F02C 7/36 (2013.01); F02C 9/20 (2013.01); F02C 9/54 (2013.01); F05D 2220/32 (2013.01); F05D 2220/76 (2013.01); F05D 2270/05 (2013.01); F05D 2270/06 (2013.01); F05D 2270/303 (2013.01); F05D 2270/304 (2013.01); Y02T 50/671 (2013.01);
Abstract

An engine that has, in axial flow series, booster compressor, core compressor, combustion equipment, core turbine, and low-pressure turbine. Core turbine drives core compressor via an interconnecting high-pressure shaft. Low-pressure turbine drives booster compressor via an interconnecting low-pressure shaft. Low-pressure turbine also drives external load having a defined speed characteristic that dictates speed of the low-pressure turbine and booster compressor. Booster compressor has one or more rows of variable stator vanes. The method includes: scheduling variation in the angle of variable stator vanes as a function of speed of the booster compressor wherein the vanes open as booster compressor speed increases; measuring or setting one or more operational parameters which are determinative of temperature at entry to core turbine; and biasing scheduling of angle variation of variable stator vanes as a function of operational parameter(s) to reduce variation in temperature at entry to core turbine.


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