Shock absorber with elastomeric strip

Spring devices – Elastic extension devices

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267 72, F16F 100

Patent

active

057721882

ABSTRACT:
A suspension component (300) has a pair of elongated slidably coupled in a telescoping arrangement. A pair of attachment plates (305, 306) are fixed to the respective suspension components (311, 314) inside an outer tube of one of the suspension components (314). An elastomeric section (303) is bonded to attachment plates (305, 306), so that collapsing the suspension components (311, 314) results in an extension of the elastomeric section (303). An adjustment mechanism is provided in the form of a rotatable threaded boss (316) mounted on one of the suspension components (314) and rotatably journaled to one of the attachment plates (306). Rotation of the suspension components causes attachment plate (306) to move axially along the length of the suspension component (314).

REFERENCES:
patent: 3653677 (1972-04-01), Feser
patent: 3917426 (1975-11-01), Wohlwend et al.
patent: 4389066 (1983-06-01), Weir et al.
patent: 4600216 (1986-07-01), Burkholder
patent: 4819956 (1989-04-01), Campbell
patent: 5054800 (1991-10-01), Christensen et al.
patent: 5242176 (1993-09-01), Hendrickson
patent: 5259597 (1993-11-01), Fredheim
patent: 5613665 (1997-03-01), Lund
Subject: Landing Gear Shock Disc Retrofit; Service Bulletin No. M20-139A, Mooney Aircraft Corporation, dated Jan. 10, 1967 and revised Mar. 10, 1982 .

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