System for supplying a turbine engine with fluid having a low pressure pumping assembly comprising two pumps in parallel

Patent metadata

Field	Value
Publication number	US-10526973-B2
Application number	US-201515316057-A
Country	US
Kind code	B2
Filing date	Jun 3, 2015
Priority date	Jun 5, 2014
Publication date	Jan 7, 2020
Grant date	Jan 7, 2020

Abstract

A system for supplying a turbine engine with fluid includes a first low-pressure pump, a downstream hydraulic resistance and a high-pressure volumetric pump located between the first low-pressure pump and the downstream hydraulic resistance. The downstream hydraulic resistance includes at least one element selected among a fluid proportioning unit, a filter, a flow meter, an exchanger, a cut-off valve and an injection system. The supply system includes a second low-pressure pump and a supply variator configured such as to vary the flow of fluid supplied to the second low-pressure pump, the second low-pressure pump and the supply variator being located parallel to the first low-pressure pump.

First claim

The invention claimed is:

1. A system for supplying a turbomachine with fluid, comprising:
a low pressure pumping assembly comprising a primary branch including a first low pressure pump,
a downstream hydraulic resistance comprising at least one element selected from a fluid metering system, a filter, a flow meter, an exchanger, a cut-off valve and an injection system, and
a high pressure volumetric pump located between the low pressure pumping assembly and the downstream hydraulic resistance,
wherein the low pressure pumping assembly comprises a secondary branch in parallel with the primary branch, the secondary branch comprising a second low pressure pump and a supply variator configured to vary a flow rate of fluid supplying the second low pressure pump,
and wherein the secondary branch branches from the primary branch at a location upstream of said first low pressure pump, and rejoins the primary branch at a location upstream of said high pressure volumetric pump.

2. The supply system according to claim 1 , wherein the system is configured to supply fuel.

3. The supply system according to claim 1 , wherein the supply variator comprises an obturator movable between an opening end position in which the supply variator allows fluid to flow to the second low pressure pump, and a closing end position in which the supply variator prevents at least partly the second low pressure pump from being supplied with fluid,
wherein an opening of the obturator is automatically controlled by at least one of electrical control and hydraulic control by a pressure upstream of the low pressure pumping assembly.

4. The supply system according to claim 3 , wherein an opening of the obturator is electrically or electro-mechanically controlled so as to allow fluid to flow to the second low pressure pump when a rotation speed of a high pressure body of a turbomachine exceeds a variable threshold.

5. The supply system according to claim 1 , wherein the supply variator is bistable with an opening stable state in which the supply variator allows fluid to flow to the second low pressure pump, and a closing stable state in which the supply variator prevents at least partly the second low pressure pump from being supplied with fluid.

6. The supply system according to claim 5 , wherein the supply variator is a valve comprising a non-return valve, a plug, a bushing or a spool.

7. The supply system according to claim 1 , wherein the first low pressure pump and the second low pressure pump are centrifugal pumps, the wheels of which are located head to foot.

8. The supply system according to claim 1 , wherein the first low pressure pump and the second low pressure pump are identical.

9. The supply system according to claim 1 , wherein the primary branch comprises a resistive element downstream of the first low pressure pump, the hydraulic resistance of the resistive element being equal to that of the supply variator.

10. The supply system according to claim 1 , wherein the downstream hydraulic resistance comprises a fluid metering system and an injection system, the fluid metering system being configured to control a flow rate towards the injection system and/or towards a fluid recirculation loop configured to convey fluid upstream of the high pressure pump.

11. A turbomachine comprising a fluid supply system according to claim 1 .

Assignees

• Safran Aircraft Engines

Inventors

• Waissi Bellal
• Vertenoeuil Philippe

Classifications

• F05D2240/40

  Use of a multiplicity of similar components · CPC title

• F02C7/236 Primary

  Fuel delivery systems comprising two or more pumps · CPC title

• F05D2260/98

  Lubrication · CPC title