Landing gear mechanism including runway-roughness restrictor ass

Details Landing gear mechanism including runway-roughness restrictor ass Landing gear mechanism including runway-roughness restrictor ass

1984-11-13

1986-06-17

Barefoot, Galen

Aeronautics and astronautics

Landing gear

Wheel

188282, 188284, 188318, B64C 2560

Patent

active

045951594

ABSTRACT:
Landing gear mechanism includes a restrictor assembly containing a primary orifice for controlling the rate of instroke of the gear during landing and a taxi instroke bypass valve which provides for increased flow of hydraulic fluid within the gear whenever the gear engages a bump during taxiing to reduce the damping loads that would otherwise occur if all of the hydraulic fluid were required to flow through the primary orifice. The taxi instroke bypass valve assembly includes a bypass passage around the primary orifice, and a slide member which is axially movable relative to the orifice restrictor assembly for opening and closing the bypass passage.

REFERENCES:
patent: 3215283 (1965-11-01), Shaver
patent: 3605960 (1971-09-01), Singer
patent: 3991863 (1976-11-01), Lee
patent: 4273303 (1981-06-01), Somm
patent: 4524929 (1985-06-01), Gebhard
patent: 4552324 (1985-11-01), Hrusch

Affiliated with

Also associated with

Rating

Landing gear mechanism including runway-roughness restrictor ass does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Landing gear mechanism including runway-roughness restrictor ass, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Landing gear mechanism including runway-roughness restrictor ass will most certainly appreciate the feedback.

Rate now

Comments { 0 }

Profile ID: LFUS-PAI-O-2269374