The invention belongs to the technical field of aircraft overall aerodynamic layout design, and particularly relates to an unmanned aerial vehicle aerodynamic layout structure suitable for intensive mounting of combat aircrafts, which comprises a fuselage, wings, a horizontal tail, a vertical tail, a first power device and a second power device, the two sets of wings are arranged on the two sides of the fuselage, the horizontal empennages are arranged on the two sides of the fuselage, the vertical empennages are arranged at the tail of the fuselage, the first power device is arranged at the top of the fuselage, and the second power device is arranged at the tail of the fuselage. The first power device is connected with the wings and the horizontal empennage and can provide force arms for the wings and the horizontal empennage; the second power device is connected with the vertical empennage and can provide a force arm for the vertical empennage; the wings, the horizontal empennage and the vertical empennage are all foldable wings and form two modes, and the two modes comprise a flight mode and a mounting mode. The unmanned aerial vehicle group can be mounted on the combat aircraft through a small space, a small number of hangers and small resistance.
本申请属于飞机总体气动布局设计技术领域,特别涉及一种适用于作战飞机密集挂载的无人机气动布局结构,包括机身、机翼、水平尾翼、垂直尾翼、第一动力装置和第二动力装置;机翼共有两组并设于机身的两侧,水平尾翼设于机身的两侧,垂直尾翼设于机身的尾部,第一动力装置设于机身的顶部,第二动力装置设于机身的尾部;第一动力装置与机翼和水平尾翼相连,能够向机翼和水平尾翼提供力臂;第二动力装置与垂直尾翼相连,能够向垂直尾翼提供力臂;机翼、水平尾翼和垂直尾翼均为折叠型机翼,形成两种模式,两种模式包括飞行模式和挂载模式。无人机群可以通过较小的空间、较少的挂架和较小的阻力实现在作战飞机上的挂载。
Unmanned aerial vehicle aerodynamic layout structure suitable for intensive mounting of combat aircrafts
一种适用于作战飞机密集挂载的无人机气动布局结构
2025-02-18
Patent
Electronic Resource
Chinese
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