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    • 2. 发明授权
    • Missile for setting down a load
    • 导弹设置负载
    • US5016534A
    • 1991-05-21
    • US391452
    • 1989-08-09
    • Hubert NohrenGerhard SiebrandWerner Moritzen
    • Hubert NohrenGerhard SiebrandWerner Moritzen
    • F42B10/56
    • F42B10/56
    • In a missile for setting down a load ejected from the missile after its launch, with at least one parachute that is attached to the load being packed in a container mounted in the missile, and with the cords of the load-carrying parachute being attached to an intermediate member coupled to the load, the intention is to reduce the size of the operational parts to be transported with the missile and improve the operation thereof during the setting down process. For this purpose it is envisaged that the container should be in the form of a two-part casing having an upper part which can be sprung open, and a plate-shaped lower part having a portion fixedly connected to the load and a support disk as the intermediate member attached to cords of the parachute. The support disk is capable of being folded out from the lower part portion while remaining connected thereto by a connecting element.
    • 在导弹发射后放下从导弹弹出的载物的导弹,至少有一个降落伞连接在装载在安装在导弹中的容器中的载荷上,承载降落伞的绳索连接到 联接到负载的中间构件,其意图是减小要与导弹一起运输的操作部件的尺寸,并且在设置停止过程期间改善其操作。 为此目的,设想容器应为具有可以弹簧打开的上部的两部分壳体的形式,并且具有固定地连接到负载的部分的板形下部和支撑盘作为 中间构件附着在降落伞的绳索上。 支撑盘能够从下部部分折叠,同时由连接元件保持连接。
    • 3. 发明授权
    • Braking mechanism for rotating flying objects
    • 旋转飞行物体的制动机构
    • US4958566A
    • 1990-09-25
    • US282029
    • 1988-12-09
    • Gerhard SiebrandBruno Sturzenbecher
    • Gerhard SiebrandBruno Sturzenbecher
    • B64D17/00F42B10/50
    • F42B10/50B64D17/00
    • A braking mechanism for a rotating flying object. The braking mechanism includes a planar fabric sheet having a central attachment base portion that can be secured to the flying object. The fabric sheet is adapted to be stored in a folded-up readiness state in the flying object, and, when released and unfolded, is adapted to form a braking surface that encircles the flying object. The braking mechanism further includes a plurality of reinforcing strips that each extend radially between the central attachment base portion and an outer rim of the braking mechanism and are distributed about the periphery of the latter. Each reinforcing strip extends from the central attachment base portion to the rim and back again to at least partially form two layers and to form loop-like pockets at the rim, with centrifugal weights being disposed in these pockets.
    • 用于旋转飞行物体的制动机构。 制动机构包括具有能够固定到飞行物体的中心附接基部的平面织物片。 织物片适于在飞行物体中以折叠状态存储,并且当释放和展开时,适于形成围绕飞行物体的制动表面。 制动机构还包括多个加强条,每条加强条各自径向延伸在中心附接基部与制动机构的外缘之间,并分布在其周围的周边。 每个加强条从中心附件基部延伸到边缘并再次返回至少部分地形成两层,并且在边缘处形成环状袋,离心重物设置在这些袋中。