发明名称 Aviation fueling hydrant coupler with internal actuating collar lock
摘要 A hydrant coupling assembly includes a hydrant valve and a hydrant coupler, including a coupler body and a coupler actuating collar assembly having an actuating collar movable axially relative to the coupler body. The actuating collar includes at least one movable latching lug that is selectively moved into place around a mating feature on the hydrant valve adapter by lifting or lowering the actuating collar. A locking mechanism is installed within the coupler actuating collar and includes a coupler plunger, a collar plunger, a coupler plunger check ball, and a collar plunger cheek ball. The coupler plunger and the coupler plunger check ball are adapted to lock the actuating collar in a disconnected state and the collar plunger and the collar plunger check ball are adapted to lock the actuating collar in a connected state. A hydrant coupler for use in a hydrant coupling assembly is also disclosed.
申请公布号 US8006713(B2) 申请公布日期 2011.08.30
申请号 US20080211680 申请日期 2008.09.16
申请人 EATON CORPORATION 发明人 WONG TAK-YIU
分类号 G05D7/00 主分类号 G05D7/00
代理机构 代理人
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