发明名称 Acceleration sensitive switch
摘要 A switch structure detects acceleration in a preselected direction such as, for example, along the pitch axis of an aircraft. The switch has a spring supported mass urged toward a stable centered position within the switch housing. Acceleration displaces the mass such that it trips a spring wire switch mechanism for controlling such avionic devices as the autopilot system of the aircraft. A pair of solenoid coils are wound around the spring mass system on opposite sides of the centered position of the mass. The switch may be preflight tested by successively energizing the solenoid coils to attract the mass toward the centers of the solenoid fields, thereby artifically displacing the mass against the spring wire switches.
申请公布号 US4093836(A) 申请公布日期 1978.06.06
申请号 US19760700501 申请日期 1976.06.28
申请人 KING RADIO CORPORATION 发明人 EWY, ROBERT J.;MOORE, ROBERT P.
分类号 G01P21/00;H01H35/14;(IPC1-7):H01H35/14;H01H67/02 主分类号 G01P21/00
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