Hydraulic drag brake

Patent metadata

Field	Value
Publication number	US-12420913-B2
Application number	US-202418431859-A
Country	US
Kind code	B2
Filing date	Feb 2, 2024
Priority date	Feb 2, 2024
Publication date	Sep 23, 2025
Grant date	Sep 23, 2025

Abstract

A hydraulic drag brake is provided for use with a driveline. The hydraulic drag brake includes a fluid circuit including first and second loops, a first valve disposed along the first loop to allow a flow of fluid through the first loop in a first direction and to prevent a flow of the fluid through the first loop in a second direction, a second valve disposed along the second loop and a pump coupled to the driveline and configured to pump the fluid through the fluid circuit in the first direction and across the first valve with the driveline occupying a retracted position or engaging in an extend motion and in the second direction and over the second valve with the driveline occupying an extended position.

First claim

What is claimed is:

1. A hydraulic drag brake for use with a driveline, the hydraulic drag brake comprising:
a fluid circuit comprising first and second loops;
a first valve disposed along the first loop to allow a flow of fluid through the first loop in a first direction and to prevent a flow of the fluid through the first loop in a second direction;
a second valve disposed along the second loop; and
a pump coupled to the driveline and configured to pump the fluid through the fluid circuit in the first direction and across the first valve with the driveline occupying a retracted position or engaging in an extend motion and in the second direction and over the second valve with the driveline occupying an extended position.

2. The hydraulic drag brake according to claim 1 , wherein the flow of the fluid in the second direction is opposite the flow of the fluid in the first direction.

3. The hydraulic drag brake according to claim 1 , further comprising an accumulator configured to maintain pressure on a suction side of the pump.

4. The hydraulic drag brake according to claim 1 , wherein the first valve comprises a check valve and the second valve comprises a pressure regulating valve (PRV).

5. The hydraulic drag brake according to claim 4 , wherein fluid flow over the PRV generates drag above a predefined torque of the driveline and hydraulic lock below the predefined torque of the driveline.

6. An aircraft, comprising:
fuselage;
wings extending outwardly from the fuselage and comprising controllable surfaces;
a power distribution unit (PDU) disposed in the fuselage and configured to generate power for driving extensions and retractions of the controllable surfaces;
the driveline and the hydraulic brake according to claim 1 ; and
a torque tube comprising the driveline disposed to transmit torque from the PDU to the controllable surfaces,
wherein the hydraulic drag brake is disposed along the driveline of the torque tube.

7. The aircraft according to claim 6 , wherein the controllable surfaces are disposed at one or more of leading and trailing edges of the wings.

8. The aircraft according to claim 6 , wherein the controllable surfaces and the hydraulic drag brake are disposed at a distal end of the driveline of the torque tube.

9. The hydraulic drag brake according to claim 5 , further comprising:
an additional check valve disposed along the second loop to allow the flow of the fluid through the second loop in the second direction and to prevent the flow of the fluid through the second loop in the second direction, and
an additional PRV disposed along the first loop to generate drag above a second predefined torque of the driveline and hydraulic lock below the second predefined torque of the driveline.

10. The hydraulic drag brake according to claim 9 , wherein the flow of the fluid in the second direction is opposite the flow of the fluid in the first direction.

11. The hydraulic drag brake according to claim 9 , further comprising an accumulator configured to maintain pressure on a suction side of the pump.

12. An aircraft, comprising:
fuselage;
wings extending outwardly from the fuselage and comprising controllable surfaces;
a power distribution unit (PDU) disposed in the fuselage and configured to generate power for driving extensions and retractions of the controllable surfaces;
a torque tube comprising the driveline according to claim 9 disposed to transmit torque from the PDU to the controllable surfaces; and
the hydraulic drag brake according to claim 9 , which is disposed along the driveline of the torque tube.

13. The aircraft according to claim 12 , wherein the controllable surfaces are disposed at one or more of leading and trailing edges of the wings.

14. The aircraft according to claim 12 , wherein the controllable surfaces and the hydraulic drag brake are disposed at a distal end of the driveline of the torque tube.

15. A self-contained bi-directional hydraulic drag brake for use with a driveline, the self-contained bi-directional hydraulic drag brake comprising:
a fluid circuit;
a pressure regulating valve (PRV) disposed along the fluid circuit;
a hydraulic rectifier disposed along the fluid circuit downstream from the PRV; and
a pump coupled to the driveline and configured to pump fluid through the fluid circuit in a first direction and over the PRV and through the hydraulic rectifier with the driveline occupying a retracted position or engaging in an extend motion and in a second direction and over the PRV and through the hydraulic rectifier with the driveline occupying an extended position.

16. The hydraulic drag brake according to claim 15 , wherein fluid flow over the PRV in the first direction and the second direction generates drag above a predefined torque of the driveline and hydraulic lock below the predefined torque of the driveline.

17. The hydraulic drag brake according to claim 16 , wherein the flow of the fluid in the second direction is opposite the flow of the fluid in the first direction.

18. The hydraulic drag brake according to claim 16 , further comprising an accumulator configured to maintain pressure on a suction side of the pump.

19. An aircraft, comprising:
fuselage;
wings extending outwardly from the fuselage and comprising controllable surfaces;
a power distribution unit (PDU) disposed in the fuselage and configured to generate power for driving extensions and retractions of the controllable surfaces;
the driveline and the hydraulic brake according to claim 15 ; and
a torque tube comprising the driveline disposed to transmit torque from the PDU to the controllable surfaces,
wherein the hydraulic drag brake is disposed along the driveline of the torque tube.

20. The aircraft according to claim 19 , wherein:
the controllable surfaces are disposed at one or more of leading and trailing edges of the wings, and
the controllable surfaces and the hydraulic drag brake are disposed at a distal end of the driveline of the torque tube.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Ankney Darrell E
• Sievert Ryan

Classifications

• B64C9/323

  associated with wings · CPC title

• B64C13/42

  having duplication or stand-by provisions · CPC title

• F16D57/06

  comprising a pump circulating fluid, braking being effected by throttling of the circulation · CPC title

• B64C13/36 Primary

  fluid · CPC title

• B64C13/28 Primary

  mechanical · CPC title