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Supersonic aircraft with reduced supersonic bang uses injection of light gas along leading edges of wings to minimize occurrence of supersonic bang

机译:超音速爆炸的超音速飞机沿机翼前缘注入轻质气体,以最大程度地减少超音速爆炸的发生

摘要

The aircraft has a light gas such as helium vented over the wing leading edge to alter the shock waves as the aircraft becomes supersonic and thus reduce sonic effects. The supersonic aircraft has a very light gas such as hydrogen or helium ejected on the leading edges of the fuselage or the wings. This has the effect of reducing the shock waves produced when the aircraft breaks through the sound barrier, or preventing their formation completely. Specifically the gas is ejected through apertures on the fuselage (22) which are upstream of the leading edges of the wing (21). The leading edges may have a convex structure, leading to a large fuel storage capacity for a given payload.
机译:飞机的机翼前缘上方放有氦气之类的轻质气体,以在飞机变为超音速时改变冲击波,从而降低声音效果。超音速飞机在机身或机翼的前缘喷射出非常轻的气体,例如氢气或氦气。这具有减少飞机冲破声屏障时产生的冲击波或完全防止其形成的效果。具体地,气体通过机翼(21)的前缘上游的机身(22)上的孔喷射。前缘可以具有凸形结构,从而对于给定的有效载荷导致大的燃料存储容量。

著录项

  • 公开/公告号FR2783499A1

    专利类型

  • 公开/公告日2000-03-24

    原文格式PDF

  • 申请/专利权人 FOURNIER GERARD;

    申请/专利号FR19980011792

  • 发明设计人 FOURNIER GERARD;

    申请日1998-09-22

  • 分类号B64C30/00;B64C23/00;B64C21/04;

  • 国家 FR

  • 入库时间 2022-08-22 01:39:41

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