作者: George Harold Bailey , William Darnell Ramsey
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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.