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UNMANNED STEALTHY AIRCRAFT-HELICOPTER

机译:意外的隐身直升机-直升机

摘要

FIELD: aviation.;SUBSTANCE: invention relates to the field of aircraft engineering and can be used in the design of unmanned aerial vehicles. Unmanned stealth aircraft-helicopter (USAH) is equipped on ends of left and right rotary profiled brackets (RPB) with single-blade rotors, used in vertical and short takeoff / landing or on transient and patrolling modes of flight. After turning in the horizontal plane RPB allow placing the corresponding rotors in side external niches from corresponding boards of inter-wing nacelles. USAH is equipped with two lifting-and-moving turbojet two-circuit engines (TTCE) with controlled thrust vector and power take-off to rotors drive to create lifting force and control moments when vertical takeoff and landing and hovering, and jet thrust at horizontal flight. USAH has mid-centered wing with X-shaped sweep in plan, root parts of which with outruns are mounted above underwing side air intakes of TTCE, having structure from channels with double S-shape at sight and from above, and sideways.;EFFECT: reduced infrared and visual visibility, higher speed and range of flight.;3 cl, 1 tbl, 4 dwg
机译:技术领域本发明涉及飞机工程领域,可用于无人飞行器的设计中。无人驾驶隐形飞机直升机(USAH)在左右旋转轮廓支架(RPB)的末端装有单叶片旋翼,用于垂直和短距起飞/着陆或瞬态和巡逻飞行模式。在水平面转弯后,RPB允许将相应的旋翼放在机翼机舱的相应板上的侧面外部壁ni中。 USAH配备了两个起升和移动涡轮喷气两回路发动机(TTCE),具有受控的推力矢量和对转子驱动的动力输出,可在垂直起飞,降落和悬停时产生升力和控制力矩,在水平方向产生喷气推力飞行。 USAH在平面图中具有X形扫掠的中心机翼,其根部伸出的部分安装在TTCE机翼下侧进气口上方,具有从视线和视线上方以及侧面和侧面呈双S形的通道构成的结构; :减少红外和视觉可见度,提高速度和飞行范围; 3 cl,1 tbl,4 dwg

著录项

  • 公开/公告号RU2686574C1

    专利类型

  • 公开/公告日2019-04-29

    原文格式PDF

  • 申请/专利权人 DUROV DMITRIJ SERGEEVICH;

    申请/专利号RU20180120399

  • 发明设计人 DUROV DMITRIJ SERGEEVICH (RU);

    申请日2018-06-01

  • 分类号B64C29;F02K1/12;B64C15/02;

  • 国家 RU

  • 入库时间 2022-08-21 11:46:16

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