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:
Oct. 19, 2021

Filed:

Sep. 19, 2017
Applicant:

Siemens Energy Global Gmbh & Co. KG, Munich, DE;

Inventor:

Senthil Krishnababu, Lincoln, GB;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/68 (2006.01); F04D 27/02 (2006.01); F04D 29/54 (2006.01);
U.S. Cl.
CPC ...
F04D 29/684 (2013.01); F04D 27/0238 (2013.01); F04D 29/542 (2013.01); F05D 2240/122 (2013.01); F05D 2240/123 (2013.01); F05D 2270/101 (2013.01);
Abstract

A technique for controlling a rotating stall in a compressor of a gas turbine engine. In the technique a flow injection is introduced into an axial air flow path of the compressor via a flow-injection opening located at a pressure side of a guide vane in the compressor and directed towards a leading edge of a compressor rotor blade located adjacently downstream of the guide vane. The flow injection is introduced when the rotating stall is detected and/or when the compressor is being operated at a speed lower than full load speed. The flow injection reduces an angle of incidence of compressor air on the leading edge of the downstream rotor blade and hence the rotor sees a more favorable velocity. The favorable velocity results into an increase in the operating range of the rotor and hence of the compressor by mitigating and/or reducing the rotating stalls.


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