Centre seeking actuator

Patent metadata

Field	Value
Publication number	US-10794407-B2
Application number	US-201715834800-A
Country	US
Kind code	B2
Filing date	Dec 7, 2017
Priority date	Dec 19, 2016
Publication date	Oct 6, 2020
Grant date	Oct 6, 2020

Abstract

A centre seeking actuator having an outer cylinder, a slave cylinder slidably disposed within the outer cylinder, and a rod assembly having a piston slidably disposed within the slave cylinder and a rod extending from the piston to a point outside the outer cylinder. One or more first dynamic seals are arranged to act on a side wall of the rod to inhibit working fluid leaking from the outer cylinder, and one or more second dynamic seals are arranged to act on a sidewall of the slave cylinder to inhibit working fluid leaking from the outer cylinder.

First claim

The invention claimed is:

1. An assembly comprising a centre seeking actuator, the centre seeking actuator comprising:
an outer cylinder;
a slave cylinder slidably disposed within the outer cylinder;
a rod assembly having a piston slidably disposed within the slave cylinder and a rod extending from the piston to a point outside the outer cylinder;
one or more first dynamic seals arranged to act on a sidewall of the rod to inhibit working fluid leaking from the outer cylinder; and
one or more second dynamic seals arranged to act on a sidewall of the slave cylinder to inhibit working fluid leaking from the outer cylinder, the one or more second dynamic seals being mounted on an inner wall of the outer cylinder;
wherein the centre seeking actuator is configured to bias a first part of the assembly to assume a predetermined position relative to a second part of the assembly, the assembly being arranged, in use, to force the actuator to assume the first condition when in a first state and having a second state in which the actuator moves the first part of the assembly to assume the predetermined position relative to the second part; and
wherein the assembly comprises an aircraft landing gear assembly.

2. The assembly according to claim 1 , wherein at least some of the sidewall of the slave cylinder that, in use, comes into contact with the second dynamic seals is provided with a coating.

3. The assembly according to claim 2 , wherein the coating comprises a high velocity oxygen fuel (HVOF) coating comprising metal, metal alloy, ceramic, plastic or composite materials.

4. The assembly according to claim 2 , wherein the coating comprises chrome or tungsten carbide.

5. The assembly according to claim 1 , wherein the outer cylinder comprises a first axial face and a second axial face connected by one or more first sidewalls to define a primary chamber, the first axial face having a first through-hole.

6. The assembly according to claim 5 , wherein the slave cylinder is slidably disposed within the primary chamber, the slave cylinder comprising a third axial face and a fourth axial face connected by one or more second sidewalls to define a slave cylinder chamber, the third axial face having a second through-hole, the slave cylinder being constrained to move only between first and second extremities within the primary chamber so as to leave at least one free portion of the primary chamber, the outer cylinder including a venting port in fluid communication with the free portion of the primary chamber.

7. The assembly according to claim 6 , wherein the piston is slidably disposed within the slave cylinder chamber and the rod can extend though the second and first through-holes so as to project a free end of the rod from the outer cylinder.

8. The assembly according to claim 7 , wherein the one or more first dynamic seals are mounted at or adjacent to the first through hole and arranged to act on an external surface of the rod to inhibit working fluid within the chamber passing though the firsts through-hole.

9. The assembly according to claim 7 , wherein the one or more second dynamic seals are mounted on the one or more first sidewalls of the outer cylinder and arranged to act on an external surface of the one or more second sidewalls of the slave cylinder to inhibit working fluid within the chamber passing to the free portion of the primary chamber.

10. The assembly according to claim 1 , provided with end stops arranged to define the first and second extremities to which the slave cylinder can move.

11. The assembly according to claim 1 , wherein the outer cylinder has a length and the one or more second dynamic seals are located closer to the middle of the outer cylinder than to either end of it.

12. The assembly according to claim 1 , wherein the first part comprises a bogie beam and the second part comprises a main strut.

13. The assembly according to claim 12 , wherein the main strut comprises a main fitting or a sliding tube of a shock absorbing strut.

14. The assembly according to claim 1 , wherein the outer cylinder comprises a mounting structure within a sidewall of the outer cylinder and the one or more second dynamic seals are coupled to the mounting structure.

15. The assembly according to claim 1 , wherein the one or more second dynamic seals are fixed relative to the outer cylinder.

16. The assembly according to claim 1 , wherein the one or more second dynamic seals are free to move relative to the outer surface of the slave cylinder.

Assignees

• Safran Landing Systems Uk Ltd

Inventors

• Simonneaux Yann

Classifications

• B64C25/58 Primary

  Arrangements or adaptations of shock-absorbers or springs (shimmy-dampers B64C25/50) · CPC title

• F16F9/06

  using both gas and liquid {(F16F9/486 take precedence; self-pumping fluid springs B60G17/044)} · CPC title

• B64C25/60

  Oleo legs · CPC title

• B64C25/22

  fluid · CPC title

• B64C2025/345

  Multi-wheel bogies having one or more steering axes · CPC title