Landing gear arrangement with passive shock strut shrink actuator

Patent metadata

Field	Value
Publication number	US-10486802-B2
Application number	US-201715483788-A
Country	US
Kind code	B2
Filing date	Apr 10, 2017
Priority date	Sep 19, 2016
Publication date	Nov 26, 2019
Grant date	Nov 26, 2019

Abstract

A landing gear arrangement may comprise a shock strut, a retraction actuator, and a shrink actuator. The retraction actuator may move the shock strut between a stowed position and a deployed position. The shrink actuator may move between a shrink position and an unshrink position in response to the shock strut moving between the stowed position and the deployed position.

First claim

What is claimed is:

1. A landing gear arrangement comprising:
a shock strut;
a retraction actuator; and
a shrink actuator;
wherein the retraction actuator moves the shock strut between a stowed position and a deployed position, and
the shrink actuator moves between a shrink position and an unshrink position in response to the shock strut moving between the stowed position and the deployed position,
wherein the shock strut is in fluid communication with the shrink actuator.

2. The landing gear arrangement of claim 1 , wherein the shrink actuator is driven by the retraction actuator.

3. The landing gear arrangement of claim 2 , wherein
the retraction actuator drives the shock strut, and
the shrink actuator is driven in response to the retraction actuator driving the shock strut.

4. The landing gear arrangement of claim 3 , wherein the shrink actuator is driven by the retraction actuator, via the shock strut.

5. The landing gear arrangement of claim 3 , wherein the shrink actuator is coupled between the shock strut and a first pivot.

6. The landing gear arrangement of claim 5 , wherein the retraction actuator is coupled between the shock strut and a second pivot.

7. A shrink actuator for a landing gear comprising:
a piston housing defining a cavity;
a piston comprising:
a piston rod; and
a piston head;

a first port disposed in the piston housing;
a second port disposed in the piston housing;
a valve coupled to the piston housing, wherein the valve is configured to actuate in response to the piston moving between an unshrink position and a shrink position;
a piston ring disposed within the cavity; and
a first spring member operatively coupled to the piston ring,
wherein the valve comprises:
a valve housing;
a plunger; and
a second spring member operatively coupled to the plunger, wherein the piston head is configured to engage the piston ring, and the piston ring is configured to engage the plunger to actuate the valve.

8. The shrink actuator of claim 7 , wherein the piston head separates the cavity into a first chamber and a second chamber.

9. The shrink actuator of claim 8 , wherein the first chamber and the second chamber are in fluid communication in response to the valve moving to an open position.

10. The shrink actuator of claim 9 , wherein the valve is configured to be in the open position in response to the landing gear moving to a deployed position.

11. The shrink actuator of claim 9 , wherein the piston head comprises a ramp surface configured to engage the plunger.

12. The shrink actuator of claim 8 , wherein the first port is in fluid communication with the first chamber and the second port is in fluid communication with the second chamber.

13. The shrink actuator of claim 12 , wherein the first port is configured to be in fluid communication with a strut hydraulic fluid chamber and the second port is configured to be in fluid communication with a strut shrink chamber.

14. The shrink actuator of claim 8 , wherein the piston head comprises a slot,
wherein in response to the piston head engaging the piston ring, the slot partially defines a flow path between the first port and the second port.

15. A method comprising:
actuating a retraction actuator of a landing gear arrangement;
moving a landing gear to at least one of a deployed position and a stowed position in response to the actuating;
moving hydraulic fluid between a landing gear strut shrink chamber and a shrink actuator chamber of a shrink actuator in response to the moving, wherein the shrink actuator is driven by the retraction actuator; and
causing a shock strut to at least one of shrink and unshrink in response to the moving the hydraulic fluid.

16. The method according to claim 15 , further comprising:
engaging a piston ring of the shrink actuator to at least one of open and close a valve of the shrink actuator; and
causing an overflow chamber to be in fluid communication with the shrink actuator chamber in response to the valve opening.

17. The method according to claim 15 , further comprising:
pivoting the shrink actuator in response to the actuation of the retraction actuator; and
causing, by the retraction actuator, a piston of the shrink actuator to at least one of retract and extend in response to the pivoting.

Assignees

• Goodrich Corp

Inventors

• Luce William E

Classifications

• B64C25/10

  retractable, foldable, or the like · CPC title

• B64C25/22 Primary

  fluid · CPC title

• B64C25/34

  wheeled type, e.g. multi-wheeled bogies · CPC title

• F16F2230/183

  fluid actuated · CPC title

• F16F2230/16

  used in a strut, basically rigid · CPC title