发明名称 Wing fold frangible valve
摘要 A reconnectable frangible coupling wherein at least one coupling part includes an operating valve and a safety valve. The operating valve utilizes the relative axial movement of the coupling parts during coupling and uncoupling to open and close, respectively, and the spring biased safety valve is engaged and retained in an open position by a valve retainer interposed between the valves. Frangible portions maintain the valve retainer in engagement with the safety valve and upon the coupling being subjected to severe impact, such as an aircraft crash, the frangible portions fracture permitting the valve retainer to disengage from the safety valve allowing the safety valve to close.
申请公布号 US4971096(A) 申请公布日期 1990.11.20
申请号 US19890418239 申请日期 1989.10.06
申请人 AEROQUIP CORPORATION 发明人 PERRINE, NEILL D.
分类号 F16L37/23;F16L37/35 主分类号 F16L37/23
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