Actuator

Patent metadata

Field	Value
Publication number	US-10190608-B2
Application number	US-201615213562-A
Country	US
Kind code	B2
Filing date	Jul 19, 2016
Priority date	Jul 21, 2015
Publication date	Jan 29, 2019
Grant date	Jan 29, 2019

Abstract

An actuator comprising: an inner cylinder received in an outer cylinder and a piston received in the inner cylinder that extends from the inner cylinder and the outer cylinder, the piston being slideable relative to the inner cylinder and the outer cylinder in response to the application of fluid pressure to cause the piston to extend further from the inner cylinder and the outer cylinder; and an auxiliary drive mechanism operable to cause the inner cylinder to extend from the outer cylinder, wherein the piston moves together with the inner cylinder relative to the outer cylinder.

First claim

The invention claimed is:

1. An actuator, comprising:
an inner cylinder received in an outer cylinder having a closed end, and a piston received in the inner cylinder that extends from the inner cylinder and the outer cylinder, the piston being slideable relative to the inner cylinder and the outer cylinder in response to the application of fluid pressure to cause the piston to extend further from the inner cylinder and the outer cylinder; and
an auxiliary drive mechanism operable to cause the inner cylinder to extend from the outer cylinder, wherein the piston moves together with the inner cylinder relative to the outer cylinder.

2. The actuator according to claim 1 , wherein the inner cylinder comprises an outer surface and the auxiliary drive mechanism includes a drive member in engagement with said outer surface to cause the inner cylinder to extend from the outer cylinder in response to rotation of said drive member.

3. The actuator according to claim 2 , wherein the outer surface comprises a helical thread, and the drive member comprises a rotatably mounted drive gear, the drive gear being in threaded engagement with said helical thread such that rotation of the drive gear causes the inner cylinder to extend from the outer cylinder.

4. The actuator according to claim 3 , wherein the auxiliary drive mechanism comprises a drive and the drive gear comprises drive engagement elements, wherein the drive cooperates with said drive engagement elements to rotate the drive gear in response to operation of said drive.

5. The actuator according to claim 4 , wherein the drive engagement elements comprise a series of recesses spaced circumferentially around an outside of the drive gear and the drive comprises a driven gear having teeth that cooperate with said recesses.

6. The actuator according to claim 4 , wherein the drive further comprises a motor or a manually operated crank which is connectable to the driven gear.

7. The actuator according to claim 1 , comprising an opening in the inner cylinder to allow fluid to flow into the inner cylinder to apply fluid pressure to the piston and cause it to move relative to the inner cylinder.

8. The actuator according to claim 7 , wherein the opening comprises a valve configured to close upon loss of fluid pressure.

9. The actuator according to claim 1 , wherein the auxiliary drive mechanism further comprises a brake configured to selectively prevent movement of the inner cylinder relative to the outer cylinder.

10. The actuator according to claim 1 , wherein the piston comprises a piston head received in the inner cylinder and a shaft extending out of the inner and outer cylinders through an orifice in an end wall of the inner cylinder.

11. An aircraft comprising an actuator according to claim 1 .

12. An actuator, comprising:
an inner cylinder received in an outer cylinder and a piston received in the inner cylinder that extends from the inner cylinder and the outer cylinder, the piston being slideable relative to the inner cylinder and the outer cylinder in response to the application of fluid pressure to cause the piston to extend further from the inner cylinder and the outer cylinder;
an auxiliary drive mechanism operable to cause the inner cylinder to extend from the outer cylinder, wherein the piston moves together with the inner cylinder relative to the outer cylinder; and,
wherein the inner and outer cylinders include cooperating elements to prevent rotation of the inner cylinder relative to the outer cylinder.

13. The actuator according to claim 12 , wherein the cooperating elements comprise a protrusion on the inner cylinder that is slideably received in an axially extending channel in the outer cylinder.

14. A method of controlling an actuator that comprises an inner cylinder received in an outer cylinder having a closed end, and a piston received in the inner cylinder that extends from the inner cylinder and the outer cylinder, the piston being slideable relative to the inner cylinder and the outer cylinder in response to the application of fluid pressure to cause the piston to extend further from the inner cylinder and the outer cylinder;
the method comprising operating an auxiliary drive mechanism to cause the inner cylinder to extend from the outer cylinder so that the piston moves together with the inner cylinder relative to the outer cylinder, in the absence of sufficient fluid pressure to cause the piston to slide relative to the inner cylinder.

15. The method of controlling the actuator according to claim 14 , wherein the auxiliary drive mechanism comprises a drive gear rotatable to cause the inner cylinder to extend from the outer cylinder, the method comprising preventing the drive gear from rotating when the fluid pressure is sufficient to cause the piston to slide relative to the inner cylinder.

Assignees

• Airbus Operations Ltd

Inventors

• Wildman Eric

Classifications

• F16H25/20

  Screw mechanisms (with automatic reversal F16H25/12) · CPC title

• F15B20/004 Primary

  Fluid pressure supply failure · CPC title

• Y02T50/145

  Cross-Sectional Technologies · mapped topic

• B64C13/42

  having duplication or stand-by provisions · CPC title

• F15B15/088 Primary

  the motor using combined actuation, e.g. electric and fluid actuation · CPC title