首页> 外国专利> Hydromechanical delay mechanism for e.g. aircraft missile - liquid filled bellows with calibrated orifice controlling rate of liquid discharge to determine timed interval

Hydromechanical delay mechanism for e.g. aircraft missile - liquid filled bellows with calibrated orifice controlling rate of liquid discharge to determine timed interval

机译:液压机械延迟机制,例如飞机导弹-装有校准孔口的充液波纹管,控制液体的排放率,确定定时间隔。

摘要

The hydromechanical delay mechanism includes a sealed hydraulic bellows subject to tension by a spring. The time delay determined by the mechanism is controlled by the holes in the plate, which defines the end of the bellows, so that the time taken for the liquid to flow out of the bellows may be controlled. A second bellows receives the liquid after passage through the calibrated holes of the end plate. The liquid used is an oil whose viscosity does not vary greatly with variations in temperature. A locking and release mechanism is arranged to allow the spring to act on the bellows once the time interval is to be started.
机译:液压机械延迟机构包括受弹簧拉紧的密封液压波纹管。由机构确定的时间延迟由限定波纹管末端的板上的孔控制,因此可以控制液体从波纹管中流出所花费的时间。第二个波纹管在通过端板的校准孔后接收液体。所使用的液体是粘度随温度变化而变化不大的油。一旦开始时间间隔,锁定和释放机构被布置成允许弹簧作用在波纹管上。

著录项

  • 公开/公告号FR2524083A1

    专利类型

  • 公开/公告日1983-09-30

    原文格式PDF

  • 申请/专利权人 SOCIETE NALE INDLE AEROSPATIALE;

    申请/专利号FR19820004987

  • 发明设计人 HENRI LOUBEYRE;

    申请日1982-03-24

  • 分类号F15B21/10;F16K31/48;G05G15/04;H01H7/02;

  • 国家 FR

  • 入库时间 2022-08-22 09:59:33

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