IP Library Granted Patent US 8,182,209
Granted Patent B2
US 8,182,209 · App. 12/128,988 · Granted May 22, 2012

Air reinjection compressor

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Quick Facts
Patent No.
US 8,182,209
App. No.
12/128,988
Granted
May 22, 2012
Kind
B2
Abstract

Reinjecting air to the inlet of a compressor in order to improve its pumping margin. The inlet stator of the compressor includes injection holes passing through at least some of the vanes in the vicinity of their pivots.

Claims (10)

1. A compressor comprising a casing housing a plurality of compression stages, each comprising a bladed rotor wheel driven in rotation, the first stage being preceded by an inlet stator presenting stationary vanes of adjustable pitch, having pivots that pass through said casing, and an air reinjection circuit,

wherein said air reinjection circuit includes injection holes passing through at least some of the vanes of said inlet stator, and opening out internally in the vicinity of their pivots, into the inlet stream of the compressor substantially tangentially relative to the casing,

wherein each of said stationary vane includes a base of circular outline with the pivot projecting outwards from a center thereof, wherein said base is housed in a housing in an outer shroud of the casing, wherein said injection holes extend in an inclined manner through the base,

wherein holes in the outer shroud of said casing open out in an annular cavity defined around said pivot and limited by the radially external surface of the inlet stator, said outer shroud of the casing, a flat annular gasket and a bushing forming the bearing of the pivot, and

wherein said injection holes extend between said annular cavity and the inside of the casing.

2. A compressor according to claim 1 , wherein said injection holes are pierced in inlet stator vanes that are regularly distributed circumferentially.

3. A compressor according to claim 1 , wherein said injection holes open out into the inlet stream of the compressor on the suction sides of the vanes of the inlet stator.

4. A compressor according to claim 1 , wherein said injection holes open out into the inlet stream of the compressor at the pressure side of the vanes of the inlet stator.

5. A compressor according to claim 1 , wherein some of the injection holes open out into the inlet stream of the compressor at the suction side and others at the pressure side of the vanes of the inlet stator.

6. A turbomachine including a compressor according to claim 1 .

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 29, 2008
From: BRAULT, MICHEL GILBERT ROLAND; OBRECHT, THIERRY JEAN-JACQUES
To: SNECMA
Reel/Frame 021015/0893 →