首页> 外国专利> Helicopter with enclosed rotors - has rear engine driving twin contra rotating rotors in wing section and using rear control flaps

Helicopter with enclosed rotors - has rear engine driving twin contra rotating rotors in wing section and using rear control flaps

机译:带有封闭式旋翼的直升机-在机翼部分具有后部发动机驱动双对旋式旋翼,并使用后部控制襟翼

摘要

The helicopter comprises an openwork boom, fitted with wheels. A wing section (18,19) is provided in a central position on this boom and contains twin contra-rotating rotors (1), cancelling torque reaction. The engine (6) is mounted at the rear. The pilot sits within a forward cabin (7), his head (10) at approximately rotor level. The rotor aperture in the wing is controlled (12) by pivoted shutters (13). At the rear of the wing is a control flap (20) acting as the tailplane and, at the rear of the boom, is another flap (21) acting as a rudder.
机译:该直升机包括一个装有轮子的镂空吊臂。机翼部分(18,19)设置在此动臂的中心位置,并包含两个反向旋转的转子(1),从而消除了扭矩反作用。发动机(6)安装在后部。飞行员坐在前机舱(7)内,其头部(10)大约处于旋翼高度。机翼中的转子孔径由枢转的百叶窗(13)控制(12)。在机翼的后部是用作尾翼的控制襟翼(20),在吊杆的后部是用作舵的另一个襟翼(21)。

著录项

  • 公开/公告号FR2462340A1

    专利类型

  • 公开/公告日1981-02-13

    原文格式PDF

  • 申请/专利权人 DEJEAN SUZANNE;

    申请/专利号FR19790019757

  • 发明设计人

    申请日1979-07-30

  • 分类号B64C27/22;

  • 国家 FR

  • 入库时间 2022-08-22 15:04:01

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