发明名称 SHUT-OFF VALVE
摘要 A shut-off valve for a hydraulic system for an aircraft, which system includes a brake operation device, a pressure supply, a reservoir, the shut-off valve, and a wheel brake. The shut-off valve (20) is in fluid communication with and is disposed between the pressure supply and the brake valve. The shut-off valve includes a poppet (158), a first valve seat (182) and a second valve seat (190) . Movement of the poppet is controlled by operation of the brake operation device. The poppet is movable between a first position where the poppet acts against the first valve seat and a second position where the poppet acts against the second valve seat. In the first position, fluid flow is blocked between the pressure supply and the brake valve through the shut-off valve. In the second position, fluid flow is allowed between the pressure supply and the brake valve through the shut-off valve. The wheel brake is in fluid communication with and downstream from the shut-off valve.
申请公布号 EP2930074(B1) 申请公布日期 2016.08.31
申请号 EP20150168441 申请日期 2011.10.10
申请人 HONDA PATENTS & TECHNOLOGIES NORTH AMERICA, LLC 发明人 OYAMA, HIROKI;BOLAND, MICHAEL JOSEPH
分类号 B60T8/34;B60T13/12;B64C25/22;B64C25/44;B64C25/46;F15B11/00;F15B13/01;F16K11/044 主分类号 B60T8/34
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