发明名称 Control manifold
摘要 A manifold controls the venting of pressurized gas from an ordnance launcher. A manifold block is provided with a number of passageways which communicate with a pair of recesses machined in the block. A high pressure gas valve is disposed in one of the recesses while a venting valve is rotatably positioned in the other recess. Ports are included in both of the valves so that when they are rotated a venting sequence of the launcher is effected. A specifically configured handle is secured to each of the valves and a spring biased pawl engages a number of teeth on the venting valve handle to allow only one direction of rotation. The configurations of the handles, the ratchet and pawl ensure a preestablished venting sequence and readying of the launcher for another shot.
申请公布号 US4181152(A) 申请公布日期 1980.01.01
申请号 US19780883752 申请日期 1978.03.06
申请人 U S OF AMERICA NAVY SECRETARY 发明人 NICOLOFF, NICHOLAS
分类号 F16K35/14;(IPC1-7):F16K35/14 主分类号 F16K35/14
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