Dual chamber shock absorbers for aircrafts and the like

Details Dual chamber shock absorbers for aircrafts and the like Dual chamber shock absorbers for aircrafts and the like

1983-10-17

1985-03-26

Butler, Douglas C.

Spring devices

Vehicle

Comprising compressible fluid

188269, 188279, 188299, 18832221, 244104FP, 267 6416, 267 6425, 267 6428, 364424, B60G 1704, B64C 2560, F16F 906, F16F 943

Patent

active

045068690

ABSTRACT:
The shock absorber is characterized by the fact that it comprises a rod (1) sliding in a cylinder (2) through a piston (3) to determine at least two variable-volume chambers (4,6), ports (40,41) for placing the two chambers in communication, one of the two chambers (4) comprising first elastic fluid (44) at a first given pressure, the other chamber (6) comprising second elastic fluid (10) at a second given pressure, controllable according to at least one parameter, corresponding to a force to be absorbed.

REFERENCES:
patent: 2196089 (1940-04-01), Wallace
patent: 2769632 (1956-11-01), de Carbon
patent: 3019029 (1962-01-01), Sampietro
patent: 3164381 (1965-01-01), Tuczek
patent: 3201112 (1965-08-01), Wossner
patent: 3250526 (1966-05-01), Kress
patent: 3292919 (1966-12-01), Lindley et al.
patent: 3540683 (1970-11-01), Foster
patent: 3962895 (1976-06-01), Rydell
patent: 4065078 (1977-12-01), Jenkins et al.
patent: 4334600 (1982-06-01), Palitto
patent: 4468739 (1984-08-01), Woods et al.

Affiliated with

Also associated with

Rating

Dual chamber shock absorbers for aircrafts and the like does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Dual chamber shock absorbers for aircrafts and the like, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Dual chamber shock absorbers for aircrafts and the like will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-1290644