The invention provides a vertical-lifting short-distance take-off and landing fixed-wing unmanned aerial vehicle which comprises a vehicle body, a vertical-lifting short-distance take-off and landing fixed-wing unmanned aerial vehicle body and a vertical-lifting The photoelectric pod load position is located on the front end face of the fuselage and used for installing a photoelectric pod, and the photoelectric pod and the fuselage are tangent to each other and are in smooth transition; the bottoms of the wings are connected with the top of the fuselage, the length directions of the wings are perpendicular to the length direction of the fuselage, the wings are symmetrically arranged about the center line in the length direction of the fuselage, and the section of the horizontal plane where the wing part located on one side of the fuselage is located is trapezoidal; the thickness of the section, close to the front end of the fuselage, of the vertical plane where the wings are located is larger than that away from the front end of the fuselage; the tail booms are positioned on two sides of the fuselage; two ends of the empennage are connected and integrally formed with the tail of the tail boom, and a main body part of the empennage is parallel to the wings to form a horizontal tail. Induced resistance is low and reliability is high.
本发明提供了一种垂起短距起降固定翼无人机,包括:机身,所述机身整体呈流线型;光电吊舱载荷位,位于所述机身前端面,用于安装光电吊舱,所述光电吊舱与所述机身连接处相切并光滑过渡;机翼,其底部与所述机身的顶部连接,其长度方向与所述机身的长度方向垂直,所述机翼以所述机身长度方向中心线对称设置,位于机身一侧的机翼部分所在的水平面的截面呈梯形;机翼所在的竖直面的截面靠近机身前端部分的厚度大于远离机身前端部分的厚度;尾撑,位于机身两侧;尾翼,其两端与尾撑的尾部连接并一体成型,其主体部分与机翼平行设置形成平尾。诱导阻力低,可靠性高。
Vertical short-distance take-off and landing fixed-wing unmanned aerial vehicle
一种垂起短距起降固定翼无人机
2022-07-22
Patent
Electronic Resource
Chinese
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