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Take-off and landing platform for vertical take-off and landing aircraft with vertical lift jet engines

机译:带有垂直升降喷气发动机的垂直起降飞机的起降平台

摘要

1,133,260. Aircraft take-off and landing places. ENTWICKLUNGSRING SUD G.m.b.H. 8 Dec., 1966 [23 Dec., 1965], No. 55103/66. Heading B7G. A landing stage for V.T.O.L. aircraft comprises a deck 32 having a series of apertures 41 each of which has a downward opening closure 40 with means 42 to 42SP1111/SP of limiting the opening of the closure 4. The apertures 41 are provided to deflect the downwardly exhausted V.T.O.L. engine efflux to prevent re-entry into the engine. The apertures 41 may be either narrow rectangular, the closures 40 being flaps hinged along their long sides, or circular holes, the closures 40 being vertically reciprocable valves, Fig. 6 (not shown). The landing stage may comprise a series of decks side by side at different levels, Fig. 1 (not shown).
机译:1,133,260。飞机起降场所。 1966年12月8日[1965年12月23日],编号55103/66。标题B7G。 V.T.O.L.的着陆阶段飞机包括具有一系列孔41的甲板32,每个孔具有向下开口的封闭件40,封闭件40具有限制封闭件4的开口的装置42至42 1111 。向下耗尽VTOL发动机外流,以防止再次进入发动机。孔41可以是狭窄的矩形,闭合件40是沿其长边铰接的折板,也可以是圆形孔,闭合件40是竖直可往复运动的阀,图6(未示出)。着陆台可包括一系列在不同高度并排的甲板,图1(未显示)。

著录项

  • 公开/公告号GB1133260A

    专利类型

  • 公开/公告日1968-11-13

    原文格式PDF

  • 申请/专利权人 ENTWICKLUNGSRING SUED GMBH;

    申请/专利号GB19660055103

  • 发明设计人 MADELUNG GERO;

    申请日1966-12-08

  • 分类号B64F1/00;E01C9/00;

  • 国家 GB

  • 入库时间 2022-08-23 11:54:56

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