Lubrication device for a turbine engine

Patent metadata

Field	Value
Publication number	US-10677095-B2
Application number	US-201515316751-A
Country	US
Kind code	B2
Filing date	Jun 11, 2015
Priority date	Jun 11, 2014
Publication date	Jun 9, 2020
Grant date	Jun 9, 2020

Abstract

The invention relates to a lubrication device for a turbine engine, comprising an oil intake pipe (23) provided with a pump (24) for supplying oil and control means (25) located downstream from the supply pump (24), a supply pipe (26) intended for supplying oil to a member to be lubricated and a recirculation pipe (27), the control means (25) making it possible to direct all or part of the flow of oil from the intake pipe (23) towards the supply pipe (26) and/or towards the recirculation pipe (27), the pump (24) being driven by at least one rotary member of an accessory gearbox of the turbine engine.

First claim

What is claimed is:

1. A lubrication device for a turbine engine, comprising an oil intake pipe provided with a supply pump for supplying oil and control means located downstream from the supply pump, a supply pipe intended for supplying oil to a member to be lubricated and an oil recirculation pipe, with the control means configured to direct all or part of the flow of oil from the intake pipe towards the supply pipe and/or towards the recirculation pipe, with the supply pump being driven by at least one rotary member of an accessory gearbox of the turbine engine, wherein the control means comprise a controlled metering valve having an inlet connected to the intake pipe and an outlet connected to the supply pipe, with the control means further comprising a control valve comprising an inlet connected to the intake pipe and an outlet connected to the recirculation pipe, with the position of the control valve being controlled by first and second oil pressures from the inlet and the outlet of the metering valve respectively, and wherein the control valve comprises a variable position piston, the position of which affects the oil flow at the outlet of the control valve, with said piston being adapted to be subjected to a first pressing force generated by applying the first oil pressure in a first pressure chamber of the control valve and a second pressing force, opposite the first pressing force, generated by applying the second oil pressure in a second pressure chamber of the control valve; and
wherein the metering valve comprises a mobile member, the position of which affects the oil flow at the outlet of said metering valve, with said position of the mobile member being measured by a sensor, the control means further configured to control said position of the mobile member by using a control law establishing a relationship between a set oil flow at the outlet of the metering valve, the measured position of the mobile member, and a temperature of the oil flow going through the metering valve as measured by a means for measuring the temperature of the oil flow through the metering valve.

2. The lubrication device according to claim 1 , further comprising a first tapping pipe connecting the intake pipe or the inlet of the metering valve and the first pressure chamber, and a second tapping pipe connecting the supply pipe or the outlet of the metering valve and the second pressure chamber.

3. The lubrication device according to claim 1 , wherein the control valve comprises a return spring adapted to generate a return force on the piston.

4. The lubrication device according to claim 1 , wherein the metering valve comprises at least one metering slot.

5. The lubrication device according to claim 1 , wherein the control valve is so dimensioned and controlled as to maintain a constant pressure difference between the outlet and the inlet of the metering valve.

6. The lubrication device according to claim 1 , wherein the recirculation pipe opens into the intake pipe upstream from the supply pump.

7. The lubrication device according to claim 1 , further comprising an oil recovery pipe adapted to recover the oil from the member to be lubricated, with said recovery pipe being provided with a recovery pump, with the recirculation pipe opening into the recovery pipe downstream from the recovery pump.

8. A turbine engine comprising the lubrication device according to claim 1 , a first and a second counter-rotating impellers driven into rotation by a low pressure turbine, through an epicyclic speed reduction gear, with the supply pipe being intended to supply the speed reduction gear with oil.

9. The turbine engine according to claim 8 , further comprising a high pressure body comprising a high pressure compressor and a high pressure turbine rotationally coupled by a first shaft, and an additional body comprising a low pressure compressor and an intermediate pressure turbine, rotationally coupled by a second shaft, with the speed of rotation of the at least one rotary member of the accessory gear box depending on the speed of rotation of the first shaft of the high pressure body.

Assignees

• Safran Aircraft Engines

Inventors

• Vielcanet Jérémy
• Frantz Caroline
• Simon David

Classifications

• F05D2260/40311

  of the epicyclical, planetary or differential type · CPC title

• F16N27/00

  Proportioning devices (liquid meters G01F) · CPC title

• F05D2220/325

  to drive unshrouded, high solidity propeller · CPC title

• F01D15/12

  Combinations with mechanical gearing (driven by multiple engines F01D13/00) · CPC title

• F05D2220/30

  in turbines · CPC title