Programmed oleo-pneumatic shock absorber
AssigneeLockheed Corporation
InventorWilliam C. Cook
Life of this patent
Estimating the term…
Abstract
An improved air/oil shock absorber (16) especially adapted for aircraft landing gears (11) is provided whereby the rate of strut (14) compression is programmed separately for the landing impact and for rollout after the landing. During the landing impact, increased tail clearance is achieved by temporarily delaying the last few inches of compression. After the aircraft rotates on to the nose landing gear, the shock absorber (16) slowly compresses to its static position where it then functions in a conventional manner. The shock absorber assembly (16) may be oriented in any position with respect to the aircraft (10) by virtue of two internal air/oil separator pistons (24 and 29).
Claims5
A programmed oleo-pneumatic shock absorber for the interconnection of two relatively movable members comprising:
- an outer cylindrical housing terminating at one end in a closure wall;
- a first hollow cylindrical piston slidably mounted in the other end of said outer cylindrical housing for telescoping movement internally thereof, said piston terminating at opposite ends in closure walls;
- attachment means carried by the opposite outer ends of said housing and said first piston, one said attachment means adapted for connection to one of said relatively movable members and the other said attachment means adapted for connection to the other of said relatively movable members;
- a pair of bearings, one carried internally by said housing adjacent its said other end and one carried externally by said piston adjacent its end internally of said housing to facilitate the movement of said housing and said piston and to define an annular chamber therebetween;
- at least one passage of predetermined size piercing the bearing carried by said piston end to establish communication between the interior of said housing and said annular chamber;
- a check valve associated with each said passage to restrict fluid flow between the interior of said housing and said annular chamber;
- a second hollow cylindrical piston transversely filling, and slidably mounted on and against the inner wall of, said first piston for movement relative to said first piston and said housing, said second piston terminating at opposite ends in closure walls;
- a slidable bulkhead mounted internally of said second piston;
- a predetermined quantity of relatively incompressible fluid within said housing, said annular chamber and the ends of said first and second pistons on the side of said slidable bulkhead adjacent said one housing end;
- a predetermined quantity of relatively compressible fluid within the ends of said first and second pistons on the other side of said slidable bulkhead;
- and
- an orifice of predetermined size in the closure wall adjacent the aforesaid telescoping end of said first piston and an orifice of small size relative to said predetermined size in each of said closure walls of said second piston, whereby an initial displacement of said second piston occurs with virtually no displacement of said bulkhead relative to said second piston upon movement of said two relatively movable members and subsequently a measurable displacement of said bulkhead relative to said second piston occurs allowing additional movement of said two relatively movable members.
Dependencies are inferred from the claim text.