System and method for supplying lubrication fluid to at least one member of an aircraft propulsion assembly

Patent metadata

Field	Value
Publication number	US-10934889-B2
Application number	US-201615775653-A
Country	US
Kind code	B2
Filing date	Nov 18, 2016
Priority date	Nov 19, 2015
Publication date	Mar 2, 2021
Grant date	Mar 2, 2021

Abstract

A feed system for feeding lubricating oil to members of a turbine engine including a reduction gearbox, the feed system including a nonpositive-displacement pump device for connecting upstream to an oil tank and driven in rotation at a speed that is not correlated with an operating speed of the turbine engine; a separator node connected to the outlet of the nonpositive-displacement pump device; a first delivery branch for lubricating the RGB connected to the nonpositive-displacement pump device via the separator node; a second delivery branch for lubricating other members connected to the nonpositive-displacement pump device via the separator node, the second delivery branch including a positive-displacement pump; and at least one fluid metering device having a metering slot fed by the nonpositive-displacement pump device via the separator node for the purpose of feeding the RGB.

First claim

The invention claimed is:

1. A feed system for feeding lubricating oil to members of a turbine engine including a reduction gearbox (RGB), the feed system comprising:
a nonpositive-displacement pump device for having an inlet connected to an oil tank and driven in rotation at a speed that is not correlated with an operating speed of the turbine engine, and comprising a nonpositive-displacement pump or at least two nonpositive-displacement pumps connected in a series fluid-flow connection;
a separator node connected to the outlet of the nonpositive-displacement pump device;
a first delivery branch for lubricating at least the RGB, which branch is connected to said nonpositive-displacement pump device via the separator node;
a second delivery branch for lubricating other members, which branch is connected to said nonpositive-displacement pump device via the separator node and includes a positive-displacement pump; and
at least one fluid metering device having a metering slot and fed by the nonpositive-displacement pump device via the separator node for the purpose of feeding the RGB.

2. The feed system according to claim 1 , further comprising a drive device for driving the positive-displacement pump device in rotation at constant speed.

3. The feed system according to claim 2 , wherein the device for driving the nonpositive-displacement pump device in rotation comprises a pneumatic actuator.

4. The feed system according to claim 2 , wherein the device for driving the nonpositive-displacement pump device in rotation comprises an electric motor.

5. The feed system according to claim 1 , further comprising a drive device for driving the positive-displacement pump device at a speed of rotation that can vary between a minimum speed and a maximum speed, said maximum speed being not less than 1.2 times the minimum speed and not greater than twice the minimum speed.

6. The feed system according to claim 5 , wherein the device for driving the nonpositive-displacement pump device in rotation comprises a drive shaft coupled to a turbine shaft of the turbine engine via an automatic gearbox having a plurality of transmission ratios.

7. The feed system according to claim 1 , further comprising a monitor device for monitoring the fluid flow rate delivered at the outlet from the fluid metering device.

8. The feed system according to claim 7 , wherein the monitor device for monitoring the fluid flow rate comprises a measurement sensor for measuring the pressure difference between the upstream and downstream sides of the fluid metering device, said measurement sensor being coupled to a sensor for sensing the position of a movable member for controlling the flow section of the metering slot of the fluid metering device.

9. The feed system according to claim 1 , wherein said nonpositive-displacement pump device comprises at least one centrifugal pump.

10. The feed system according to claim 1 , wherein the first delivery branch between the separator node and the RGB does not have a fluid recirculation loop.

11. A method of using the feed system according to claim 1 , the method comprising a step of regulating the flow rate of the lubricating oil by controlling the position of the movable member for controlling the flow section of the fluid metering device.

12. An aircraft propulsion assembly including a feed system according to claim 1 , for feeding lubricating oil to a reduction gearbox of a turbine engine.

Assignees

• Safran Aircraft Engines

Inventors

• Chalaud Sebastien Christophe

Classifications

• F16H57/0435

  Pressure control for supplying lubricant; Circuits or valves therefor · CPC title

• F16N25/00

  Distributing equipment {with or without proportioning devices} · CPC title

• F05D2260/98

  Lubrication · CPC title

• F16N2270/70

  Supply · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title