Device for concomitant opening or closing of two flaps of a landing gear door

Patent metadata

Field	Value
Publication number	US-9499258-B2
Application number	US-201414567527-A
Country	US
Kind code	B2
Filing date	Dec 11, 2014
Priority date	Dec 16, 2013
Publication date	Nov 22, 2016
Grant date	Nov 22, 2016

Abstract

A device for concomitant opening or closing of two flaps of a door of an aircraft retractable landing gear. The device comprises a single actuating means for the opening or the closing of the two flaps under the effect of its extension or of its retraction. The actuating means comprises a first end linked to the structure of the aircraft, and a movable part. The device comprises a swinging arm comprising a first end linked by a pivot to the structure, and a second end linked to the movable part of the actuating means by a link having a degree of rotational freedom about an axis parallel to the axis of the pivot. The second end of the swinging arm is furthermore respectively linked to a first tie rod linked to a first of the two flaps, and to a second tie rod linked to a second of the two flaps.

First claim

What is claimed is:

1. A device for concomitant opening or closing of two flaps of a door of an aircraft retractable landing gear, the two flaps pivoting about two approximately parallel longitudinal pivot axes that define a closing plane of the two flaps, the device comprising:
a single actuating means having a length, that is able to open and close the two flaps by modification of the length, the actuating means comprising a fixed end linked at a force-absorbing point to a structure of the aircraft, the actuating means furthermore comprising a movable part that moves substantially orthogonally to the closing plane of the two flaps; and
a swinging arm comprising a first end pivotably linked to the structure of the aircraft, and a second end opposite the first end and pivotably linked by a second link to the movable part of the actuating means, the first end pivotably linked about an arm pivot axis and the second link having a degree of rotational freedom about an axis parallel to the arm pivot axis, the device being configured such that the second end of the swinging arm moves away from the closing plane of the two flaps during the extension of the actuating means to close the two flaps, and such that the second end of the swinging arm moves toward the closing plane of the two flaps during retraction of the actuating means to open the two flaps, the second end of the swinging arm furthermore being respectively linked to a first tie rod linked to a first of the two flaps, and to a second tie rod linked to a second of the two flaps.

2. The device of claim 1 , wherein the movable part of the actuating means is linked to the swinging arm by a universal joint.

3. The device according to claim 1 , wherein the movable part of the actuating means comprises a movable end linked to the swinging arm.

4. The device of claim 3 , wherein the actuating means is a cylinder.

5. The device of claim 4 , wherein the device is symmetrical about either side of a longitudinal plane orthogonal to the closing plane.

6. The device of claim 5 , wherein each tie rod is linked to a respective one of the two flaps at a distance from the pivot axis of the respective one of the two flaps.

7. The device of claim 6 , wherein each tie rod is linked to a respective one of the two flaps by a ball joint link.

8. The device of claim 7 , wherein each flap comprises a panel and an actuating part rigidly linked to the panel, a respective one of the first tie rod or the second tie rod being linked to the actuating part.

Assignees

• Airbus Operations Sas
• Airbus Operations Sas

Inventors

• Reynes Didier
• Phalippou Jerome

Classifications

• B64C25/16

  Fairings movable in conjunction with undercarriage elements · CPC title

• B64C25/20 Primary

  mechanical · CPC title

• Y10T74/18888

  Reciprocating to or from oscillating · CPC title