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:
Apr. 05, 2022

Filed:

Apr. 23, 2019
Applicant:

Rolls-royce Plc, London, GB;

Inventors:

David P. Scothern, Derby, GB;

Steven P. Culwick, Derby, GB;

Shane Perera, Derby, GB;

Edward J. Spalton, Derby, GB;

Assignee:

Rolls-Royce plc, London, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/00 (2006.01); F02C 7/047 (2006.01); F02C 9/18 (2006.01); B64D 33/02 (2006.01); F01D 25/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/047 (2013.01); F02C 9/18 (2013.01); B64D 2033/0233 (2013.01); F01D 25/02 (2013.01); F05D 2270/101 (2013.01); F05D 2270/303 (2013.01);
Abstract

A gas turbine engine comprising: an engine core comprising a compressor; a compressor bleed valve in communication with the compressor and configured to release bleed air from the compressor; at least one component provided at the inlet of the engine core having a de-icing conduit, configured to receive the bleed air; and a flow controller, configured to provide bleed air to the de-icing conduit of the at least one component in response to either or both of a requirement to de-ice the component and a requirement to release bleed air from the compressor to optimise operation of the core.


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