发明名称 PROPORTIONAL PRESSURE DIFFERNCE ACTUATOR
摘要 Actuation of a pressure actuator is manifested solely when the pressures from two separate systems exceed a predetermined differential or the absence of pressure is evidenced by including a piston having one face sensitive to one of the pressures and the opposing face sensitive to the other pressure, and a pair of smaller pistons slidably mounted on connecting shaft of the piston, each having a face adapted to subtract a force from the total force when the pressure acting on one face of the sensing piston is at a predetermined value. The piston is spring loaded in an actuating position when no pressure is acting on the piston.
申请公布号 US3668349(A) 申请公布日期 1972.06.06
申请号 USD3668349 申请日期 1971.03.12
申请人 UNITED AIRCRAFT CORP. 发明人 JEROME G. DUCHESNEAU;ROBERT A. SCHWARTZ
分类号 H01H35/38;(IPC1-7):H01H35/38;F01B7/04 主分类号 H01H35/38
代理机构 代理人
主权项
地址