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.
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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 |
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代理人 |
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主权项 |
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地址 |
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