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    • 1. 发明授权
    • Aircrew escape system
    • AIRCREW ESCAPE系统
    • US3756546A
    • 1973-09-04
    • US3756546D
    • 1971-11-23
    • US NAVY
    • CARSON RLYONS J
    • B64D25/12
    • B64D25/12Y10S244/902Y10S244/903
    • An aircrew escape system comprising a capsule adapted to contain a crewmember, having attached thereto a deployable parawing controllable by the crewmember, and a deployable tractor rocket connected to the top of the capsule by a length of tow rope. Contained within the capsule is a control unit by which the crewmember, once in position, initiates the burn of the tractor rocket, initiating separation of the capsule from the aircraft and through which the crewmember can control the jettisoning of the tractor rocket and the ignition of an air-breathing powerplant mounted on the capsule. The parawing, in its deployed state, is aligned at an angle of attack relative the longitudinal axis of the capsule by preselected lengths of supporting shrouds having control shrouds attached to the trailing edge thereof terminating at a control stick in the capsule. Accordingly, when the capsule is accelerated by the tractor rocket to a velocity where the lift force of the parawing substantially balances the weight of the capsule the tractor rocket is released, the powerplant is started and the capsule is in position for controlled horizontal flight.
    • 一种空勤逃生系统,其包括适于容纳机组成员的胶囊,其附接有可由机组成员控制的可展开的解剖,以及可伸展的拖拉机火箭,其通过一定长度的牵引绳连接到胶囊的顶部。 包含在胶囊内的是控制单元,通过该控制单元,机组成员一旦处于适当位置,启动拖拉机火箭的燃烧,启动胶囊与飞机的分离,并且机组成员可以通过该单元控制拖拉机火箭的放弃和点火 安装在胶囊上的呼吸呼吸动力装置。 处于其展开状态的解剖通过预选长度的支撑罩以相对于胶囊的纵向轴线的迎角对准,其具有附接到其后缘的控制罩,其终止于胶囊中的控制棒。 因此,当胶囊被拖拉机火箭加速到速度时,其中解压的提升力基本上平衡了释放拖拉机火箭的胶囊的重量,起动动力装置并且胶囊处于适当位置以进行受控的水平飞行。