首页> 外国专利> Combination aircraft has rotor lift for telescoping of rotor power unit and makes it possible for rotor drive to be withdrawn completely from aerodynamic influence in plane flying by recessing into fuselage or to extend it from fuselage

Combination aircraft has rotor lift for telescoping of rotor power unit and makes it possible for rotor drive to be withdrawn completely from aerodynamic influence in plane flying by recessing into fuselage or to extend it from fuselage

机译:组合飞机具有旋翼升降机,用于伸缩旋翼动力单元,并可以通过缩进机身或将其从机身延伸而完全摆脱飞机飞行中的空气动力影响

摘要

The combination aircraft has a rotor lift (1) for telescoping of the rotor power unit and makes it possible for the rotor drive to be withdrawn completely from the aerodynamic influence in plane flying by recessing into the fuselage (6), or to extend it from the fuselage. A leading edge slat (2) is installed below the canard wings (7) under the fuselage and enables stabilizing of the flying craft even during the telescoping of the rotor drive during the transition of plane flying to rotary wing operation, and vice versa.
机译:组合式飞机具有一个旋翼升降机(1),用于伸缩旋翼动力单元,并使旋翼驱动器可以通过凹进机身(6)来完全摆脱飞机飞行中的空气动力影响,或者从中伸出机身。前缘板条(2)安装在机身下方的鸭翼(7)下方,即使在飞机飞行过渡到旋翼操作过程中旋翼驱动器伸缩时,也能使飞行器稳定,反之亦然。

著录项

  • 公开/公告号DE20303024U1

    专利类型

  • 公开/公告日2003-08-14

    原文格式PDF

  • 申请/专利权人 HINUEBER EDGAR V.;

    申请/专利号DE2003203024U

  • 发明设计人

    申请日2003-02-19

  • 分类号B64C29/00;

  • 国家 DE

  • 入库时间 2022-08-21 23:41:01

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