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stabilizer and / or steering committee for aerodynamic or ballistic flugkoerper i electric fields

机译:空气动力学或弹道电子稳定器和/或转向委员会

摘要

1,064,235. Aircraft. H. VON ENGEL. March 16, 1964 [April 4, 1963], No. 11105/64. Headings B7G and B7W. [Also in Division F3] A stabilizing or control member for a flying body subjected to the action of an electrostatic field has an electrically conducting surface or surfaces forming one or more parts of a helix. In Fig. 3, for example, a stabilizer 7 is attached to a flying body 3, and is stated to diminish any tendency for an electrostatic field to divert the body from its course. The stabilizer is rotatable about the fore-and-aft axis of the body 6. Two such stabilizers may be hinged to the trailing edge of an annular wing, which may also be a ram-jet casing. Discrete parts only of the helix may be electrically conducting, these parts being embedded in a non-conductive support. Such stabilizers or control members may also provide some propulsive and lifting forces in an electrostatic field. Two such stabilizers may be attached at diametrically opposite points of the body, or two bodies may be attached one to each end of a stabilizer. A plurality of stabilizers may extend downwardly from hinge joints on the body. A kite-shaped body may have helices extending from both its upper and lower surfaces. In Fig. 10, a number of stabilizers 28 are attached to a body 27, and each terminates in a lifting aerofoil, the tip of which is adjustable for trimming or control purposes. Each stabilizer is rotatable about its axis, and the set of stabilizers may be rotatable about the body 27 to provide lift like a helicopter rotor. The flying body may itself set up an electrostatic field, by means of radio-active sheet metal, thermal ionization devices, or by the friction of a discharge nozzle on streams of gas or essential oils.
机译:1,064,235。飞机。 H.冯恩格尔。 1964年3月16日[1963年4月4日],编号11105/64。标题B7G和B7W。 [也在F3分部中]用于飞行体的受到静电场作用的稳定或控制构件具有形成螺旋的一个或多个部分的一个或多个导电表面。例如,在图3中,稳定器7附接到飞行主体3,并且被声明为减小静电场使主体偏离其航向的任何趋势。稳定器可绕主体6的前后轴线旋转。两个这样的稳定​​器可铰接到环形机翼的后缘,该环形机翼也可以是冲压喷气机壳体。仅螺旋的离散部分可以是导电的,这些部分被嵌入在不导电的支架中。这种稳定器或控制构件还可在静电场中提供一些推进力和提升力。两个这样的稳定​​器可以连接在主体的相对的两个点上,或者两个主体可以一个连接到稳定器的每一端。多个稳定器可以从主体上的铰链接头向下延伸。风筝形的主体可以具有从其上表面和下表面延伸的螺旋。在图10中,多个稳定器28附接到主体27,并且每个稳定器终止于提升翼型,翼型的末端可调节以用于修整或控制目的。每个稳定器可绕其轴线旋转,并且该组稳定器可绕主体27旋转以提供升力,如直升机旋翼。飞行体本身可以借助放射性金属薄板,热电离装置或通过排放喷嘴在气体或精油流上的摩擦来建立静电场。

著录项

  • 公开/公告号DE000001428685A

    专利类型

  • 公开/公告日1969-02-27

    原文格式PDF

  • 申请/专利权人 ENGEL HANS WERNER VON;

    申请/专利号DE1428685A

  • 发明设计人 VON ENGEL HANS-WERNER;HALIK ERICH;

    申请日1963-10-11

  • 分类号

  • 国家 DE

  • 入库时间 2022-08-23 12:22:25

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