首页> 外国专利> DEVICE FOR OVERCOMING THE PROBLEM OF CREW SAFETY DURING A SPACECRAFT LAUNCH AND INPROVE THE JOINTS CONNECTING THE SEGMENTS OF THE SOLID ROCKET BOOSTER

DEVICE FOR OVERCOMING THE PROBLEM OF CREW SAFETY DURING A SPACECRAFT LAUNCH AND INPROVE THE JOINTS CONNECTING THE SEGMENTS OF THE SOLID ROCKET BOOSTER

机译:克服航天飞机发射过程中机组安全问题并改善连接固体火箭助推器段的接头的装置

摘要

Spacecraft, satellites, aircraft and powder rocket launchers are provided with similar clamping devices comprising a housing (6-41), a sleeve (9-42) and the clamping screw (11-15). The housing (6) consists of a stop ring (7) and the sleeve (9) of a number of sectors (10) provided with a modular multiple thread. The clamping screw (11-15) are formed of a towing hook engageable with a stop ring (7) and are provided with a similar modular thread so that the sectors (10) are screwed into the clamping screw (11-15) so as to attach the detachable sections. In addition, spacecraft, satellites and planes are provided with an actuator mechanism which disconnects the joined sections. Explosive charges may be fired by means of a gear mounted ejection and disposed on an interrupt line between sections and can separate the sections from the rest. The parachutes (4), which are in the parachute bag, are released one at a time or in a predetermined order and the crew capsule (2) or the compartment in which persons are supported in on board allows a soft landing and sure.
机译:航天器,卫星,飞机和火药火箭发射器配备有类似的夹紧装置,包括壳体(6-41),套筒(9-42)和夹紧螺钉(11-15)。壳体(6)由止动环(7)和多个扇形部分(10)的套筒(9)组成,所述扇形部分(10)设有模块化多螺纹。夹紧螺钉(11-15)由可与挡圈(7)接合的拖钩形成,并设有类似的模块化螺纹,以便将扇形体(10)拧入夹紧螺钉(11-15)中,以便连接可拆卸部分。另外,航天器,卫星和飞机设有致动器机构,该致动器机构使连接的部分断开。爆炸性装药可以通过装在齿轮上的弹射来发射,并放置在部分之间的中断线上,并且可以将部分与其余部分分开。降落伞袋中的降落伞(4)一次或以预定顺序释放一次,乘员舱(2)或船上人员被支撑在其中的舱室可以软着陆并确保安全。

著录项

  • 公开/公告号EP0303628A1

    专利类型

  • 公开/公告日1989-02-22

    原文格式PDF

  • 申请/专利权人 LEVIN ZINOVI;

    申请/专利号EP19880900035

  • 发明设计人 LEVIN ZINOVI;

    申请日1987-12-15

  • 分类号B64D25/08;B64G1/52;B64G1/64;B64G1/00;B64G1/40;B64G1/60;

  • 国家 EP

  • 入库时间 2022-08-22 06:34:26

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