UNDERCARRIAGE SHOCK ABSORBER WITH POSITIVE RETENTION IN A RETRACTED POSITION AND WITH CRASH OVERTRAVEL

• US 20090218444A1
• Filed: 10/23/2006
• Published: 09/03/2009
• Est. Priority Date: 10/27/2005
• Status: Abandoned Application

• Current Assignee: Messier-Bugatti-Dowty
• Original Assignee: Messier-Dowty SA (Government of France)
• Inventors: Robuchon, Alain, Lahargou, Andre, Brune, Marc
• Application Number:
  US12/091,616
• Publication Number:
  US 20090218444A1
• Time in Patent Office: Days
• US Class Current: 244/102.SL
• CPC Class Codes: B64C 2025/008 Comprising means for modifying their length, e.g. for kneeling, for jumping, or for leveling the aircraft
• CPC Class Codes: B64C 25/60 Oleo legs

Abstract

The invention relates to a telescopic shock absorber for an aircraft undercarriage, the shock absorber comprising a strut (1) in which a rod (2) is mounted to slide, the shock absorber including controlled retraction means (41 . . . 43) for retracting the rod into the strut to a retracted position. The shock absorber includes positive retention means (27, 29) for retaining the rod in the strut and adapted to retain the rod in the retracted position when the rod is moved thereto by the retraction means, the positive retention means being arranged, at least in the event of a severe landing of the aircraft, to allow the rod to be pushed into the strut beyond the retracted position.

Claims

1. A telescopic shock absorber for an aircraft undercarriage, the shock absorber comprising a strut (1;

101;

201) in which a rod (2;

102;

202) is mounted to slide, the shock absorber including controlled retraction means (41 . . . 43) for retracting the rod into the strut to a retracted position,

the shock absorber including positive retention means (27, 29;

152, 153;

227, 229) for retaining the rod in the strut and adapted to retain the rod in the retracted position when the rod is moved thereto by the retraction means, the positive retention means being arranged, at least during a severe landing of the aircraft, to enable the rod to be pushed into the strut beyond the retracted position either by leaving the rod free to slide beyond the retracted position, or by yielding under thrust from the rod.

2. A shock absorber according to claim 1, in which the shock absorber includes an abutment (26;

226) defining the retracted position of the rod in the strut that is associated with means (25;

225) enabling it to be overridden by thrust from the rod against the abutment in the event of a severe landing of the aircraft.

3. A shock absorber according to claim 2, in which the means for overriding the abutment (26;

226) comprise a deformable structure (25;

225).

4. A shock absorber according to claim 2, in which the positive retention means comprise, on one of the rod and strut elements, a catch (27;

227) associated with a locking piston (29;

229), and on the other one of the rod and strut elements, a step (28;

228) adapted to co-operate with the catch to retain the rod positively in the retracted position.

5. A shock absorber according to claim 4, in which the catch (27) is mounted on the strut, being secured to the abutment (26), such that the catch follows the rod when the rod is pushed in beyond the retracted position.

6. A shock absorber according to claim 4, in which the catch (227) is mounted on the strut independently of the abutment (226) such that the catch remains stationary while the rod is being pushed in beyond the retracted position.

7. A shock absorber according to claim 1, in which the positive retention means comprise fingers (151) mounted to slide on the strut perpendicularly to a sliding direction of the rod, and urged by springs towards a latching position in which they are suitable for co-operating with a top end of the rod to retain it in the retracted position.

8. A shock absorber according to claim 7, in which the end of the rod comprises in succession:

a first conical portion (155);

a groove (156) for receiving the fingers when the rod is in the retracted position; and

a second conical portion (157) extending a surface defining a wall of the groove in such a manner that in the event of a severe landing, the fingers are pushed back by said second conical portion.