IP Library Granted Patent US 8,764,385
Granted Patent B2
US 8,764,385 · App. 13/001,155 · Granted Jul 1, 2014

Axial-centrifugal compressor having system for controlling play

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Quick Facts
Patent No.
US 8,764,385
App. No.
13/001,155
Granted
Jul 1, 2014
Kind
B2
Abstract

In an axial-centrifugal compressor, the rotor of which includes an impeller, axial play is controlled by a special air ventilation to the rotor, by a circuit including two parallel arms, flow rates of which are both controlled by respective veins, and moreover the temperature in one of them is changed by a heat exchanger. The ventilation air is thus controlled, both in terms of temperature and flow rate.

Claims (19)

1. An axial centrifugal compressor comprising:

a rotor including an axial portion and a spread-out portion, the spread-out portion including an impeller of the rotor; and

a stator, separated from the rotor by a flow vein, and including an axial portion and a spread-out portion, the axial portions of the rotor and stator being concentric with an axis line and spaced apart by an amount of radial play, and the spread-out portions of the rotor and stator being aligned along the axis line and spaced apart by an amount of axial play, and

a ventilation circuit that adjusts the amount of axial play between the spread-out portions of the rotor and stator, the ventilation circuit extending from the stator into a cavity inside the rotor and including:

a first arm having a first valve that adjusts an opening amount of the first arm, and

a second arm having a heat exchanger and a second valve that adjusts an opening amount of the second arm.

2. The axial centrifugal compressor according to claim 1 , wherein the first arm and the second arm have a common origin, in a cavity of the stator adjacent the flow vein.

3. The axial centrifugal compressor according to claim 1 , wherein the second arm is disposed radially outward of the first arm.

4. The axial centrifugal compressor according to claim 1 , wherein the heat exchanger of the second arm is provided by a section of the second arm passing through an outer cavity of the stator.

5. The axial centrifugal compressor according to claim 1 , further comprising control circuitry that opens the second valve at a stable cruising speed of the axial centrifugal compressor.

6. The axial centrifugal compressor according to claim 1 , wherein the cavity extends between a bearing supporting the rotor and the spread-out portion of the rotor.

7. The axial centrifugal compressor according to claim 1 , wherein the ventilation circuit extends in a radial arm supporting the rotor.

8. The axial centrifugal compressor according to claim 1 , wherein the amount of axial play between the spread-out portions of the rotor and stator is greater at startup as compared to during cruising.

9. The axial centrifugal compressor according to claim 1 , wherein other than a common origin in a cavity of the stator, no part of the first arm is included as part of the second arm.

10. The axial centrifugal compressor according to claim 1 , wherein the first arm and the second arm originate in a cavity of the stator and terminate in the cavity inside the rotor.

11. The axial centrifugal compressor according to claim 1 , wherein the ventilation circuit adjusts the amount of axial play between the spread-out portions of the rotor and stator by controlling an air flow rate of each of the first arm and the second arm.

12. The axial centrifugal compressor according to claim 1 , wherein, during startup, the second valve is completely closed so as to prevent air from flowing through the second arm having the heat exchanger.

13. The axial centrifugal compressor according to claim 1 , wherein the first arm and the second arm include at least one common conduit portion shared therebetween.

14. The axial centrifugal compressor according to claim 1 , wherein the ventilation circuit originates in a cavity of the stator and terminates in the cavity inside the rotor.

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 Jan 4, 2011
From: BEHAGHEL, LAURENT DONATIEN; FONTANEL, EDDY STEPHANE JOEL; PEGOUET, BENJAMIN PHILIPPE PIERRE
To: SNECMA
Reel/Frame 025576/0760 →