Electrohydraulic pitch-control system with a valve pump in a rotating reference frame

Patent metadata

Field	Value
Publication number	US-12397901-B2
Application number	US-202218564446-A
Country	US
Kind code	B2
Filing date	May 20, 2022
Priority date	May 28, 2021
Publication date	Aug 26, 2025
Grant date	Aug 26, 2025

Abstract

The present invention relates to a pitch-change mechanism for a turbine engine propeller, said turbine engine comprising a stator portion and a rotor portion, said pitch-change mechanism comprising an electrohydraulic actuator comprising: —a cylinder for actuating the propeller, comprising a first chamber and a second chamber; —a hydraulic pump suitable for selectively supplying the first chamber or the second chamber of the cylinder with pressurized hydraulic fluid; —a hydraulic fluid reservoir configured to store a pressurized hydraulic fluid; —a valve controlled between a first position in which the valve places the first chamber of the cylinder in fluid communication with the hydraulic pump, and a second position in which the valve places the first chamber of the cylinder in fluid communication with the hydraulic fluid reservoir.

First claim

The invention claimed is:

1. A pitch change mechanism for a propeller, said pitch change mechanism comprising an electrohydraulic actuator comprising:
a jack for actuating the propeller comprising a first chamber and a second chamber;
a hydraulic pump adapted to selectively supply the first chamber or the second chamber with a pressurized hydraulic fluid;
a hydraulic fluid tank configured to store the pressurized hydraulic fluid;
a valve configured to move between a first position, in which the valve puts the first chamber in fluid communication with the hydraulic pump, and a second position in which the valve puts the first chamber in fluid communication with the hydraulic fluid tank; and
an additional hydraulic fluid tank, the valve being controlled by a pressure from the additional hydraulic fluid tank;
wherein a pressure of the hydraulic fluid tank is greater than the pressure of the additional hydraulic fluid tank.

2. The pitch change mechanism according to claim 1 , wherein the valve is configured to move from the first position to the second position when the pressure of the additional hydraulic fluid tank is below a predetermined threshold.

3. The pitch change mechanism according to claim 1 , wherein the additional hydraulic fluid tank is mounted in a rotating reference frame of a turbine engine.

4. The pitch change mechanism according to claim 1 , further comprising at least one of a pressure relief valve and an additional valve configured to put the second chamber in fluid communication with the additional hydraulic tank.

5. The pitch change mechanism according to claim 4 , wherein the at least one of the pressure relief valve and the additional valve is controlled by the pressure of the additional fluid tank.

6. The pitch change mechanism according to claim 1 , further comprising an additional pressure relief valve configured to put the first chamber in fluid communication with the additional hydraulic fluid tank when the pressure of the first chamber is above a predetermined threshold.

7. The pitch change mechanism according to claim 1 , wherein the hydraulic fluid tank is mounted in a rotating reference frame of a turbine engine.

8. The pitch change mechanism according to claim 1 , wherein the hydraulic pump comprises a body, an inclined plate and a barrel, wherein the body of the hydraulic pump is in a rotating reference frame of a turbine engine, and one of the inclined plate and the barrel of the hydraulic pump is in a fixed reference frame of the turbine engine.

9. The pitch change mechanism according to claim 8 , wherein absent any rotation between the fixed reference frame and the rotating reference frame, a flow rate of the pump is null.

10. The pitch change mechanism according to claim 1 , further comprising a flow rate reversal valve configured to selectively put the hydraulic pump in fluid communication with the first chamber or the second chamber.

11. The pitch change mechanism according to claim 1 , wherein the hydraulic pump is reversible.

12. A turbine engine comprising a propeller and a pitch change mechanism according to claim 1 configured to actuate a cylinder which is mechanically connected to the propeller.

13. An aircraft comprising at least one turbine engine according to claim 12 connected on the aircraft via a pylon.

14. The turbine engine according to claim 12 , further comprising an additional hydraulic fluid tank mounted in a rotating reference frame of the turbine engine, the valve being controlled by a pressure from the additional hydraulic fluid tank.

15. The turbine engine according to claim 12 , wherein the hydraulic fluid tank is mounted in a rotating reference frame of the turbine engine.

16. The turbine engine according to claim 12 , wherein the hydraulic pump comprises a body, an inclined plate and a barrel, wherein the body of the hydraulic pump is in a rotating reference frame of the turbine engine and one of the inclined plate and the barrel of the hydraulic pump is in a fixed reference frame of the turbine engine.

17. A pitch change mechanism for a propeller, said pitch change mechanism comprising an electrohydraulic actuator comprising:
a jack for actuating the propeller comprising a first chamber and a second chamber;
a hydraulic pump adapted to selectively supply the first chamber or the second chamber with a pressurized hydraulic fluid; a hydraulic fluid tank configured to store the pressurized hydraulic fluid; and
a valve configured to move between a first position, in which the valve puts the first chamber in fluid communication with the hydraulic pump, and a second position in which the valve puts the first chamber in fluid communication with the hydraulic fluid tank;
wherein the hydraulic pump comprises a body, an inclined plate and a barrel, wherein the body of the hydraulic pump is in a rotating reference frame of a turbine engine, and one of the inclined plate and the barrel of the hydraulic pump is in a fixed reference frame of the turbine engine;
wherein absent any rotation between the fixed reference frame and the rotating reference frame, a flow rate of the pump is null.

18. A pitch change mechanism for a propeller, said pitch change mechanism comprising an electrohydraulic actuator comprising:
a jack for actuating the propeller comprising:
a first chamber and a second chamber;
a hydraulic pump adapted to selectively supply the first chamber or the second chamber with a pressurized hydraulic fluid;
a hydraulic fluid tank configured to store the pressurized hydraulic fluid;
a valve configured to move between a first position, in which the valve puts the first chamber in fluid communication with the hydraulic pump, and a second position in which the valve puts the first chamber in fluid communication with the hydraulic fluid tank; and
a flow rate reversal valve configured to selectively put the hydraulic pump in fluid communication with the first chamber or the second chamber.

Assignees

• Safran Aircraft Engines

Inventors

• De Wergifosse Huguette
• Auriol Jacques

Classifications

• F15B1/033

  with electrical control means · CPC title

• F15B9/09

  with electrical control means · CPC title

• F15B2211/31535

  having multiple pressure sources and a single output member · CPC title

• F15B2211/30565

  having multiple valves for a single output member, e.g. for creating higher valve function by use of multiple valves like two 2/2-valves replacing a 5/3-valve · CPC title

• F15B2211/212

  the pressure sources being accumulators · CPC title