IP Library Granted Patent US 7,789,617
Granted Patent B2
US 7,789,617 · App. 11/580,158 · Granted Sep 7, 2010

Impeller and diffuser with a rotating and converging hub

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Quick Facts
Patent No.
US 7,789,617
App. No.
11/580,158
Granted
Sep 7, 2010
Kind
B2
Abstract

A suction stage for a pump with a centrifugal wheel, the suction stage including a rotational impeller equipped with a hub and arranged upstream of the centrifugal wheel, the suction stage further including a diffuser arranged between the impeller and the centrifugal wheel, the diffuser including a plurality of blades. The hub has a downstream surface extending axially so as to converge toward the centrifugal wheel, and the blades of the diffuser have free ends, the blades protruding radially toward the downstream surface.

Claims (31)

1. A pump for liquefied gas comprising:

a suction stage having at least one centrifugal wheel,

the suction stage comprising:

a rotational impeller equipped with a hub having a downstream surface extending axially toward the centrifugal wheel, the hub being arranged upstream of the centrifugal wheel, and

a diffuser comprising a plurality of blades surrounding the downstream surface,

wherein the hub further has a median portion and axial ends, the hub having a greater diameter in its median portion than at its axial ends so that the downstream surface converges toward the centrifugal wheel,

wherein the blades of the diffuser have free ends, said blades protruding radially toward said downstream surface of the hub, and

wherein the downstream surface and an outer shell of the diffuser radially define an annular duct which allows a drawn-in fluid to pass, the annular duct having a substantially constant radial height over the axial length of the downstream surface.

2. The pump according to claim 1 , wherein the diffuser surrounds the downstream surface of the hub of the impeller.

3. The pump according to claim 1 , wherein the blades of the diffuser are fixed to the outer shell which converges axially toward an inlet of the centrifugal wheel.

4. The pump according to claim 1 , wherein the axial length of the diffuser is substantially equal to the axial length of the downstream surface of the hub of the impeller.

5. The pump according to claim 1 , wherein the downstream surface has a radial section which diminishes toward the centrifugal wheel.

6. The pump according to claim 1 , wherein the hub further has an upstream surface having an axial length and wherein the outer shell presents a constant diameter along the axial length of the upstream surface.

7. The pump according to claim 1 , wherein the hub further includes an upstream surface carrying paddles, and wherein the hub is a one-piece element.

8. A pump for liquefied gas comprising:

a suction stage having at least one centrifugal wheel,

the suction stage comprising:

a rotational impeller equipped with a hub having a downstream surface extending axially toward the centrifugal wheel, the hub being arranged upstream of the centrifugal wheel,

a diffuser comprising a plurality of blades surrounding the downstream surface wherein the hub further has a median portion and axial ends, the hub having a greater diameter in its median portion than at its axial ends so that the downstream surface converges toward the centrifugal wheel, and

an outer shell which surrounds the hub,

wherein the blades of the diffuser have free ends, said blades protruding radially toward said downstream surface of the hub and wherein the axial length of the diffuser is substantially equal to the axial length of the downstream surface of the hub of the impeller.

9. The pump according to claim 8 , wherein the hub further has an upstream surface having an axial length and wherein the outer shell presents a constant diameter along the axial length of the upstream surface.

10. A pump for liquefied gas comprising:

a suction stage having at least one centrifugal wheel,

the suction stage comprising:

a rotational impeller equipped with a hub having a downstream surface extending axially toward the centrifugal wheel, the hub being arranged upstream of the centrifugal wheel, and

a diffuser comprising a plurality of blades surrounding the downstream surface wherein the hub further has a median portion and axial ends, the hub having a greater diameter in its median portion than at its axial ends so that the downstream surface converges toward the centrifugal wheel, and

an outer shell which surrounds the hub,

wherein the blades of the diffuser have free ends, said blades protruding radially toward said downstream surface of the hub, and

wherein the hub further has an upstream surface having an axial length and wherein the outer shell presents a constant diameter along the axial length of the upstream surface.

11. The pump according to claim 10 , wherein the downstream surface and the outer shell radially define an annular duct which allows a drawn-in fluid to pass, the annular duct having a substantially constant radial height over the axial length of the downstream surface.

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 18, 2007
From: WAHL, FABIEN; N GUYEN DUC, JEAN-MICHEL; TESSIER, FABIEN; BOUFFLERT, SEBASTIEN
To: SNECMA
Reel/Frame 018812/0855 →