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:
Aug. 22, 2017

Filed:

May. 02, 2014
Applicant:

Techspace Aero S.a., Herstal (Milmort), BE;

Inventors:

Alain Derclaye, Couthuin, BE;

David Depaepe, Liege, BE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/54 (2006.01); F01D 5/14 (2006.01); F01D 9/04 (2006.01); F04D 29/68 (2006.01);
U.S. Cl.
CPC ...
F01D 5/142 (2013.01); F01D 5/146 (2013.01); F01D 9/041 (2013.01); F04D 29/542 (2013.01); F04D 29/544 (2013.01); F04D 29/681 (2013.01); Y02T 50/672 (2013.01); Y02T 50/673 (2013.01);
Abstract

The present application relates to the compressor stator of an axial turbomachine. The stator comprises an annular row of main stator blades and auxiliary blades each of which are associated with a main blade. The auxiliary blades are located at the trailing edges of the main blades and are in the vicinity of the pressure faces of the main blades. The auxiliary blades are aligned to generate a low-pressure area at the trailing edges of the main blades. Thus, a flow bypassing a main blade by its suction face is sucked in by the low-pressure area when it approaches the trailing edge of the main blade. Stalling is thus avoided and the efficiency of the machine is improved.


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