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Two-position latching electromagnetic valve of liquid-pressurised pipe systems e.g. for space flight vehicles drive systems

机译:液体压力管道系统的二位自锁电磁阀用于太空飞行器驱动系统

摘要

The valve has its inlet (2) and outlet (3) at opposite ends of its housing (1) which encloses a hollow cylindrical armature (6) with a central annular ferromagnetic projection (8) movable axially in the gap between two coils (4,5). The armature extends into a plunger (9) carrying a sealing head (10) and bellows (11) at the outlet end. The inlet end is terminated with a flange (17) and another bellows (16). At each end a main spring washer (21) is provided with a subsidiary spring washer (22) sliding along it in the same annular space (19).
机译:该阀在其壳体(1)的相对两端具有入口(2)和出口(3),该壳体包围空心圆柱形电枢(6),该圆柱形电枢具有在两个线圈(4)之间的间隙中可轴向移动的中央环形铁磁凸起(8) ,5)。衔铁伸入带有密封头(10)和波纹管(11)的柱塞(9)的出口端。入口端用法兰(17)和另一个波纹管(16)终止。在主弹簧垫圈(21)的每个端部上设有在同一环形空间(19)中沿其滑动的辅助弹簧垫圈(22)。

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