首页> 外国专利> Aircraft with multiple lift surfaces - has jet engine in nose to augment air flow and retractable rotary wings giving VSTOL capability

Aircraft with multiple lift surfaces - has jet engine in nose to augment air flow and retractable rotary wings giving VSTOL capability

机译:具有多个升力面的飞机-机头装有喷气发动机,以增加气流,并提供可伸缩旋翼,提供VSTOL功能

摘要

The aircraft has flap-controlled air intake openings near the nose of its fuselage. Air discharge openings are provided along top and sides, and at the tail. Two jet engines inside the nose augment the flow over several internal lift surfaces with flaps for takeoff/landing. Together with the main propulsion units, mounted in pairs in echelon on mid-fuselage stub wings, these jets provide power for normal flight. For VSTOL, additional lift is provided by three rotary wings above the fuselage, retracting into the latter when not in use. Normal control surfaces are fitted at the tail.
机译:飞机的机头附近有襟翼控制的进气口。排气孔沿顶部,侧面和尾部提供。机头内部的两个喷气发动机通过带有用于起飞/降落的襟翼的多个内部提升表面来增加流量。这些喷气式飞机与主要推进装置成对安装在机身中部短翼上的梯队中,为正常飞行提供动力。对于VSTOL,机身上方的三个旋转翼提供了额外的提起力,在不使用时可缩回到机身中。正常的控制面安装在尾部。

著录项

  • 公开/公告号DE2634258A1

    专利类型

  • 公开/公告日1978-02-02

    原文格式PDF

  • 申请/专利权人 HAITZAUGUST;

    申请/专利号DE19762634258

  • 发明设计人 HAITZAUGUST;

    申请日1976-07-30

  • 分类号B64C27/22;

  • 国家 DE

  • 入库时间 2022-08-22 22:01:24

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