Aeronautics and astronautics – Aircraft control
Patent
1982-09-24
1985-02-05
Barefoot, Galen
Aeronautics and astronautics
Aircraft control
74526, 244213, B64C 1900
Patent
active
044974612
ABSTRACT:
A snubber (12) includes a fixed member (14) and a movable member (16). A variable volume chamber (20) is defined between these two members (14, 16). The chamber (20) includes an orifice (22). A body of extrusible material (26) substantially fills the chamber (20). A rotary actuator (6) carries a lug (28) that contacts the movable member (16) when the actuator (6) moves beyond a predetermined position. This contact pushes the movable member (16) against the extrusible material (26) to decrease the volume of the chamber (20) and to cause the extrusible material (26) to be extruded through the orifice (22). This stops the rotation of the actuator (6) and absorbs its kinetic energy. The snubber (12) is supported by a frame member (10). Preferably, the frame member (10) has a cavity (40) into which material extruded through the orifice (22) is received.
REFERENCES:
patent: 136040 (1873-02-01), Darrell
patent: 367742 (1887-08-01), Byrne
patent: 874150 (1907-12-01), Young
patent: 2516406 (1950-07-01), Moyer
patent: 2756951 (1956-07-01), Hanson et al.
patent: 2997325 (1961-08-01), Peterson
patent: 3039757 (1962-06-01), Barr
patent: 3209864 (1965-10-01), Boyd
patent: 3380557 (1968-04-01), Peterson
patent: 3398812 (1968-08-01), Peterson
patent: 3638767 (1972-02-01), Elsner et al.
patent: 3867750 (1975-02-01), Bleyker
patent: 4034958 (1977-07-01), Masclet
patent: 4121483 (1978-10-01), Sedlock
Barefoot Galen
Barnard Delbert J.
Pauly Joan H.
The Boeing Company
LandOfFree
Snubbing apparatus for an aircraft control surface actuator does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Snubbing apparatus for an aircraft control surface actuator, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Snubbing apparatus for an aircraft control surface actuator will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-2079716