IP Library Granted Patent US 7,686,572
Granted Patent B2
US 7,686,572 · App. 11/580,159 · Granted Mar 30, 2010

Pump comprising an axial balancing system

View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 7,686,572
App. No.
11/580,159
Granted
Mar 30, 2010
Kind
B2
Abstract

A pump for the drawing-in of a fluid, including at least one centrifugal wheel having a fluid inlet edge and a fluid outlet edge, the pump further including an axial balancing system with a high-pressure flow space defined between the housing and an upstream face of the centrifugal wheel. The axial balancing system further includes a device for substantially increasing the hydrostatic pressure of the fluid circulating in the high-pressure flow space during operation of the pump.

Claims (10)

1. A pump for the drawing-in of a fluid, comprising at least one centrifugal wheel having a fluid inlet edge and a fluid outlet edge, the centrifugal wheel being driven in rotation by a shaft mounted so as to be able to rotate relative to a housing of the pump, the pump further comprising an axial balancing system comprising a high-pressure flow space defined between the housing and an upstream face of the centrifugal wheel, a low-pressure flow space defined between the housing and a downstream face of the centrifugal wheel, the high-pressure flow space comprising an inlet arranged in proximity to the outlet edge of the centrifugal wheel and an outlet arranged in proximity to the inlet edge of the centrifugal wheel, said outlet of the high-pressure flow space being equipped with first flow restriction means, the low-pressure flow space comprising an inlet arranged in proximity to the outlet edge of the centrifugal wheel, said inlet of the low-pressure flow space being equipped with second flow restriction means, the low-pressure flow space further comprising an outlet having an annular passage forming an axially variable flow restriction and opening radially onto an annular discharge space defined around said shaft radially internally relative to the annular passage, the annular space communicating with a region in which the pressure is lower than that in the low-pressure flow space, wherein the axial balancing system further comprises a plurality of vanes formed on the housing, said vanes extending radially and in a centripetal direction immediately adjacent the outlet edge of the centrifugal wheel.

2. The pump according to claim 1 , wherein said vanes are angularly set apart about the axis of rotation of the pump.

3. The pump according to claim 1 , wherein two adjacent vanes delimit a groove, which opens axially internally into the high-pressure flow space.

4. The pump according to claim 1 , wherein the axial balancing system further comprises at least one reinjection channel extending between the annular discharge space and a fluid region located upstream of the inlet edge of the centrifugal wheel.

5. The pump according to claim 4 , wherein the reinjection channel is provided in the centrifugal wheel.

6. The pump according to claim 1 , wherein the annular passage is defined between a first annular rib formed on the downstream face of the centrifugal wheel and a second annular rib formed on the housing.

7. The pump according to claim 1 , wherein the first and/or the second flow restriction means comprise an annular seal.

8. The pump according to claim 7 , wherein the annular seal is a labyrinth seal.

9. The pump according to claim 1 , wherein the vanes are disposed circumferentially around the axis of rotation of the pump and within said high-pressure flow space.

10. The pump according to claim 1 , wherein the vanes are configured to obstruct a tangential flow of a fluid surging from the centrifugal wheel into the high-pressure flow space.

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 19, 2007
From: WAHL, FABIEN; DANGUY, FRANCOIS; LAFFITE, STEPHANE; BOURDIN, PHILIPPE
To: SNECMA
Reel/Frame 018824/0792 →