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. 11, 2017

Filed:

May. 15, 2012
Applicants:

Jérôme Yves Félix Gilbert Porodo, Pau, FR;

Laurent Pierre Tarnowski, Pau, FR;

Assignee:

TURBOMECA, Bordes, FR;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/44 (2006.01); F04D 29/68 (2006.01); F04D 27/02 (2006.01);
U.S. Cl.
CPC ...
F04D 29/441 (2013.01); F04D 29/444 (2013.01); F04D 29/682 (2013.01); F04D 29/684 (2013.01); F04D 27/023 (2013.01); F04D 27/0238 (2013.01); F05D 2240/122 (2013.01); F05D 2250/52 (2013.01);
Abstract

A diffuser of a compressor of centrifugal or mixed type includes two end plates which enclose a plurality of regularly distributed circumferential blades, and at least one transverse upstream passage produced in lower or upper surfaces of the blades. An injection/withdrawal coupling is achieved by a recirculation of a stream in an air passage of the diffuser on the basis of injection of air from at least one point in a leading edge zone of an upstream side of the diffuser. Blowing of air is then effected in at least one groove formed along a lateral flank of each blade by withdrawal of the air stream in a region of a trailing edge. Thereby, effectively separation of the air in a boundary layer in a gas turbine compressor diffuser is realized by re-energizing the boundary layer with air at a higher pressure by a suction/re-injection coupling.


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