Self-adjusting slide assembly for weight on gear switch

作者: George Harold Bailey , William Darnell Ramsey

DOI:

关键词:

摘要: A self-adjusting slide assembly (10) is provided for mounting a weight on gear switch to an aircraft. The particularly adapted skid equipped helicopter (11) responding vertical oscillatory deflection of cross tube (14) the landing (12). bracket (16) attached underside supporting back plate (18) and pair clamp plates (20). C-shaped member (24) has flange (25) mounted between so as vertically. Take-off stresses cause exhibit upper arm (30) lower (26) member. microswitch (34) actuated when contacts bottom bumper (29) while fully gear.

参考文章(15)
Leo Franklin Geiger, Truck or trailer axle overload indicator ,(1974)
Oskar F. Vatterott, Actuator switch assembly ,(1981)
Charles D. Bateman, Helicopter weight measuring system ,(1983)
Mark I Curl, John R Steigerwald, Electrical anti-skid mechanism for brakes ,(1954)
Ervin Gordon Romero, Aircraft automatic braking system ,(1975)
Wesley L. Cresap, Alan W. Myers, Helicopter landing gear with crosstube pivot ,(1979)
Stephen W Salai, Jr Thomas B Meek, Helicopter landing gear unsafe warning system ,(1965)
Ray D. Leoni, Landing gear in-flight vibration dampener Journal of the Acoustical Society of America. ,vol. 73, pp. 1093- 1093 ,(1978) , 10.1121/1.389093
Billy H Dickson, Paul Eugene Darden, Landing gear load transducer ,(1987)