The invention relates to the technical field of aircraft design, and discloses a fixed-wing aircraft with a four-power-cabin compound function cabin, which comprises a fuselage, wings and an empennage, the fuselage comprises a left fuselage, a right fuselage and two hanging power cabins, the wings are composed of a middle wing, a left outer wing and a right outer wing, and the middle wing is connected to the upper portions of the left fuselage and the right fuselage; the left outer wing is connected to the left end of the middle wing, and the right outer wing is connected to the right end of the middle wing; the left end and the right end of the horizontal empennage are correspondingly connected with the tails of the left fuselage and the right fuselage respectively; the tail parts of the two hanging power cabins are connected with the middle section wing; and a power device is arranged in each of the left fuselage, the right fuselage and the two hanging power cabins. The power conversion efficiency of the fixed-wing aircraft is effectively improved, the maneuverability of the aircraft is improved, and the ground sliding direction of the aircraft is more efficiently and easily controlled; and a double-machine-body layout is adopted, so that the structural strength and the space of the functional bin are increased, and the stress area is dispersed.
本发明涉及飞行器设计技术领域,公开了一种四动力舱复合功能舱的固定翼飞机,包括机身、机翼和尾翼;机身包括左机身、右机身以及两个吊挂动力舱,机翼由中段机翼、左侧外翼、右侧外翼组成,中段机翼连接于左机身与右机身的上部;左侧外翼连接在中段机翼的左端,右侧外翼连接在中段机翼的右端;尾翼为水平尾翼,其左右两端分别对应连接左机身与右机身的尾部;两个吊挂动力舱的尾部与中段机翼相连接;左机身、右机身以及两个吊挂动力舱内各自安装有一台动力装置。本发明有效提升了固定翼飞机的动力转换效率,提高了飞行器的机动性,使飞行器地面滑行方向控制更加高效容易;并且采用双机身布局,增加了结构强度和功能仓空间,分散了受力面积。
Fixed-wing aircraft with four-power-cabin compound function cabin
一种四动力舱复合功能舱的固定翼飞机
2024-04-02
Patent
Electronic Resource
Chinese