IP Library Granted Patent US 9,752,575
Granted Patent B2
US 9,752,575 · App. 14/750,121 · Granted Sep 5, 2017

Two stage pump, particularly provided as main pump for supplying an aircraft engine with fuel

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 9,752,575
App. No.
14/750,121
Granted
Sep 5, 2017
Kind
B2
Abstract

A two stage pump ( 2′, 4′ ), where the high pressure stage ( 4 ′) is a gear pump ( 11, 12 ), comprises a driving of the other stage ( 2 ′) by a support shaft ( 74 ), mounted in the driven pinion ( 12 ), the shaft ( 74 ) being driven by the drive shaft ( 21 ), by means of a pair of toothed wheels ( 77, 79 ) adjacent to the rest of the stage ( 4 ′), which can allow different rotation speeds between the two stages ( 2′, 4′ ). The support shaft ( 74 ) may be supported by stops and hydrodynamic bearings, directly integrated and lubricated in the driven pinion, which make the design lighter and more compact. The shaft ( 74 ) and the toothed wheels ( 77, 79 ) ingeniously transmit the loads from the stage ( 2 ′) to the stage ( 4 ′) in such a way as to cancel out the usual hydraulic loads, stemming from pressure, and mechanical, forces stemming from rotational drivings on the driven pinion ( 12 ).

Claims (13)

1. Two stage pump including a first pump having a rotating pumping element driven by a support shaft, a second pump including two pumping pinions meshing together, the two pumping pinions including a driving pinion and a driven pinion, a drive shaft of the driving pinion extending along a longitudinal axis, and a transmission connecting the driving pinion to the support shaft, the transmission being contained in the second pump, the support shaft being coaxial to the driven pinion, wherein the support shaft is partially contained in a reaming passing through the driven pinion, and in that it comprises a first bearing supporting the support shaft in the reaming, formed between the support shaft and the driven pinion.

2. Two stage pump according to claim 1 , wherein the first bearing comprises a first axial stop, and the support shaft and the reaming are provided with radial projections having opposite faces that are either flat, or, preferably, conical.

3. Two stage pump according to claim 2 , wherein the first axial stop is hydrodynamic and maintained by re-circulations of a fluid pumped in one of the two pumps.

4. Two stage pump according to claim 1 , wherein it includes a sealing gasket arranged around the support shaft, separating the pumping element of the first pump from the second pump, the sealing gasket forming a second bearing supporting the support shaft.

5. Two stage pump according to claim 4 , wherein the second bearing is hydrodynamic and maintained by re-circulations of a fluid pumped in one of the two pumps.

6. Two stage pump according to claim 4 , wherein the transmission consists of a first toothed wheel and a second toothed wheel, respectively integral with the driving pinion and the support shaft and meshing together.

7. Two stage pump according to claim 6 , wherein the sealing gasket is arranged between a flange of a casing of the two stage pump and the second toothed wheel, the flange separating respective chambers of the first pump and the second pump.

8. Two stage pump according to claim 1 , wherein the transmission consists of a first toothed wheel and a second toothed wheel, respectively integral with the driving pinion and the support shaft and meshing together.

9. Two stage pump according to claim 8 , wherein the second toothed wheel and a support bearing of the driven pinion have respective elements which cooperate to form a second axial stop.

10. Two stage pump according to claim 9 , wherein the second axial stop is hydrodynamic and maintained by re-circulations of a fluid pumped in one of the two pumps.

11. Two stage pump according to claim 8 , whrein the transmission further includes a sleeve integral with the first toothed wheel and sunk into a reaming of the driving pinion.

12. Two stage pump according to claim 1 , wherein the first bearing is hydrodynamic and maintained by re-circulations of a fluid pumped in one of the two pumps.

13. Two stage pump according to claim 1 , wherein the rotating pumping element includes a fluid outlet volute of changing shape, which is arranged so as to exert on the support shaft a load of constant orientation towards the driving pinion.

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 Sep 17, 2015
From: VERTENOEUIL, PHILIPPE
To: SNECMA
Reel/Frame 036585/0813 →