The invention belongs to the technical field of airplanes, and discloses a high-wind-resistance distributed propulsion aircraft. The aircraft comprises a fuselage, wings, an empennage and distributed propellers, the fuselage and the wings are fused in the middle of the fuselage, the fuselage is in a non-circular and non-flat U shape, the wings are divided into an inner wing, an outer wing and a small wing, the distributed propellers are symmetrically installed at the tail edge of the upper surface of the inner wing, and the empennage is arranged in a V-tail or pi-tail mode and installed above the tail of the fuselage. According to the high-wind-resistance distributed propulsion aircraft, through the fusion design of the aircraft body and the wings, the aircraft has small course static stability, through differential control of the distributed propellers, the aircraft has high course control capacity, and compared with an aircraft with a traditional layout, the aircraft has the advantages that the aircraft is more stable; the high-wind-resistance distributed propulsion aircraft disclosed by the invention has very high wind resistance.
本发明属于飞机技术领域,公开了一种高抗风的分布式推进飞行器。该飞行器包含机身、机翼、尾翼和分布式推进器,机身和机翼在机身中部融合设计,机身采用非圆非扁平的U型,机翼分为内翼、外翼和小翼,分布式推进器对称安装在内翼上表面尾缘处,尾翼采用V尾或π尾布局并安装在机身尾部上方。本发明的一种高抗风的分布式推进飞行器,通过机身和机翼的融合设计使飞机具有较小的航向静稳定性,通过分布式推进器差动控制使飞机具有较高的航向操控能力,相对传统布局飞行器,本发明的一种高抗风的分布式推进飞行器具备很强的抗风能力。
High-wind-resistance distributed propulsion aircraft
一种高抗风的分布式推进飞行器
2023-04-04
Patent
Elektronische Ressource
Chinesisch
Ionic wind propulsion aircraft and propulsion method thereof
Europäisches Patentamt | 2020
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