首页> 外国专利> APPARATUS FOR REDUCING SONIC BOOM SHOCKWAVE PROPAGATION IN THE DIRECTION TOWARDS THE EARTH CAUSED BY AN AIRCRAFT IN SUPERSONIC FLIGHT

APPARATUS FOR REDUCING SONIC BOOM SHOCKWAVE PROPAGATION IN THE DIRECTION TOWARDS THE EARTH CAUSED BY AN AIRCRAFT IN SUPERSONIC FLIGHT

机译:减少超声速飞行中飞机向地球方向的声波波传播的装置

摘要

1,205,865. Inhibiting sonic boom on aircraft. H. PREUSS. 24 June, 1968, No. 29994/68. Heading B7W. A device for reducing the supersonic boom caused by aircraft in the direction of the earth's surface, Fig. 9, comprises reflecting surfaces 1, 2 attached under the fuselage 3 and wings 4 respectively, by the supports 7 and 8. The surface 1 which may be hollow, may be filled completely or in part with damping material, carry an electric charge, or be pressurized, is convex with respect to the fuselage, as shown in Fig. 9, and is positioned such that it is in the area of the sonic boom wave caused by the fuselage in supersonic flight; the surfaces 2 are similarly positioned to reflect the boom wave of the wings. The surface 1 is adjustably mounted and its position may be altered by means of an electronic computer.
机译:1,205,865。抑制飞机上的音爆。 H.普锐斯。 1968年6月24日,编号29994/68。标题B7W。一种用于减少飞机沿地球表面方向引起的超音速动臂的装置,图9,包括反射面1、2,分别通过支撑件7和8连接在机身3和机翼4下方。如图9所示,它可以是空心的,可以完全或部分地用阻尼材料填充,可以带电荷或被加压,相对于机身是凸形的,并且位置应使其位于机身的区域内。超音速飞行中机身引起的音爆波;表面2类似地定位以反映机翼的动臂波。表面1是可调节地安装的,并且其位置可以借助于电子计算机来改变。

著录项

  • 公开/公告号GB1205865A

    专利类型

  • 公开/公告日1970-09-23

    原文格式PDF

  • 申请/专利权人 HEINZ PREUSS;

    申请/专利号GB19680029994

  • 发明设计人 HEINZ PREUSS;

    申请日1968-06-24

  • 分类号B64C23/04;

  • 国家 GB

  • 入库时间 2022-08-23 10:30:03

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