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, satellite, aeroplane and solid rocket booster are provided with similar locking device, comprise the housing (6-41), sleeve (9-42) and the screw clamps (11-15). The housing (6) is composite with thrust ring (7) and sleeve (9) with a number of sectors (10), which are provided with a module multiple thread. The screw clamps (11-15) are formed with a draw hook engageable with thrust ring (7) and provided with similar module multiple thread, so that to the sectors (10) screw in the screw with clamps (11-15) to joint the detachable sections. In addition to it, spacecraft, satellite, aeroplane are provided with a tripping mechanism which is disconnecting the joined sections. Explosive charges which may be fired by means of ejection gear mounted and disposed on a break line between sections and carry out detachment the sections from the remainder. The parachutes (4) in the pack are released one at a time or predetermined order and the crew capsule (2) or the compartment with people on board makes a safe, soft landing.
机译:航天器,卫星,飞机和固体火箭助推器均设有类似的锁定装置,包括壳体(6-41),套筒(9-42)和螺丝夹(11-15)。壳体(6)由推力环(7)和套筒(9)制成,该套筒具有多个扇形部(10),扇形部具有模块多螺纹。螺丝夹(11-15)形成有可与止推环(7)接合的拉钩,并具有类似的模块多螺纹,以便将螺丝(11-15)拧入扇形部分(10)以将其连接可拆卸部分。除此以外,航天器,卫星,飞机还设有脱扣机构,该脱扣机构使连接的部分断开。爆炸性装药可以通过安装并安置在分段之间的折线上的弹射装置来发射,并使分段与其余部分分离。一次或按预定顺序释放背包中的降落伞(4),乘员舱(2)或载有人员的舱室可以安全,软着陆。

著录项

  • 公开/公告号WO8806120A1

    专利类型

  • 公开/公告日1988-08-25

    原文格式PDF

  • 申请/专利权人 LEVIN ZINOVI;

    申请/专利号WO1987GB00906

  • 发明设计人 LEVIN ZINOVI;

    申请日1987-12-15

  • 分类号B64D25/12;B64G1/52;F42B15/00;

  • 国家 WO

  • 入库时间 2022-08-22 06:56:21

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