Device for coupling an actuator for controlling the landing gear of an aircraft

Patent metadata

Field	Value
Publication number	US-9511852-B2
Application number	US-201214238534-A
Country	US
Kind code	B2
Filing date	Sep 7, 2012
Priority date	Sep 9, 2011
Publication date	Dec 6, 2016
Grant date	Dec 6, 2016

Abstract

A device for coupling an actuator for operating an aircraft undercarriage to an aircraft structure. The device comprises a lever having a first end for hinging to the structure of the aircraft, and a second end to which the actuator is hinged, a pre-loading structure acting on the lever to urge it towards a stable rest position that is occupied by the lever in the absence of any force transiting through the actuator; and an abutment structure defining at least one working position for the lever when the actuator is activated.

First claim

The invention claimed is:

1. A device for coupling an actuator for operating an aircraft undercarriage to an aircraft structure, the device comprising:
a lever having a first end for hinging to the structure of the aircraft, and a second end to which the actuator is hinged;
pre-loading means acting on the lever to urge it towards a stable rest position that is occupied by the lever in the absence of any force transiting through the actuator; and
abutment means for defining at least one working position wherein the lever contacts said abutment means when the actuator is actuated.

2. A device according to claim 1 , wherein the pre-loading means are arranged to define said stable rest position and the abutment means are arranged to define said at least one working positions distinct from said stable rest position.

3. A device according to claim 2 , wherein the pre-loading means comprise two pushers arranged on either side of the lever to co-operate therewith and to urge the lever towards said stable rest position situated between two working positions defined on either side of said stable rest position by the abutment means.

4. A device according to claim 1 , wherein said abutment means are arranged to define a first working position for the lever and a second working position for the lever, and wherein the pre-loading means urge the lever towards the abutment means so that said stable rest position and said first working position coincide.

5. A device according to claim 1 , wherein said device further comprises:
a crank hinged to the structure of the aircraft; and
a connecting rod;
wherein the pre-loading means further comprises:
a spring acting on said crank; and

wherein the crank is coupled to the lever by means of said connecting rod.

6. An aircraft having a device according to claim 1 for coupling an actuator for operating an aircraft undercarriage.

7. An aircraft having a device according to claim 2 for coupling an actuator for operating an aircraft undercarriage.

8. An aircraft having a device according to claim 3 for coupling an actuator for operating an aircraft undercarriage.

9. An aircraft having a device according to claim 4 for coupling an actuator for operating an aircraft undercarriage.

10. An aircraft having a device according to claim 5 for coupling an actuator for operating an aircraft undercarriage.

Assignees

• Blanpain Thierry
• Ducos Dominique
• Campbell Edouard
• Messier Bugatti Dowty

Inventors

• Blanpain Thierry
• Ducos Dominique
• Campbell Edouard

Classifications

• B64C25/26

  Control or locking systems therefor · CPC title

• B64C25/58

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

• B64C25/62

  Spring shock-absorbers; Springs · CPC title

• B64C25/20 Primary

  mechanical · CPC title