The invention relates to a tilting composite wing aircraft taking a multi-rotor framework as a main part, belongs to the technical field of aircrafts, and solves the technical problem that the existing tilting composite wing aircraft is relatively low in flight safety. The aircraft provided by the invention comprises an aircraft body, wherein the aircraft body comprises an aircraft head and an aircraft tail; hang gliders which are connected to the two sides of the fuselage; two front arms which are connected to the machine head; two rear arms which are connected to the tail; a first rotor system is fixedly mounted on the front arms, a second rotor system is fixedly mounted on the rear arms, a third rotor system is mounted on the hang glider, the two front arms and the two rear arms are parallel to a first plane, a rotor surface of the first rotor system and a rotor surface of the second rotor system are parallel to a second plane, and an included angle alpha is formed between the first plane and the second plane; wherein 0 < alpha < 60 degrees. The aircraft is higher in flight safety, higher in hovering stability and wider in application range.
本发明涉及一种以多旋翼构架为主的倾转复合翼飞行器,属于飞行器技术领域,解决现有倾转复合翼飞行器飞行安全性较低的技术问题。本发明提供的飞行器包括机身,机身包括机头和机尾;滑翔翼,机身的两侧均连接有滑翔翼;两根前臂,前臂连接在机头;两根后臂,后臂连接在机尾;前臂固装有第一旋翼系统,后臂固装有第二旋翼系统,滑翔翼安装有第三旋翼系统,两根前臂和两根后臂均与第一平面平行,第一旋翼系统的旋翼面和第二旋翼系统的旋翼面均与第二平面平行,第一平面和第二平面之间具有夹角α,0<α<60°。该飞行器的飞行安全性更高,悬停稳定性更高,并且使用范围更广。
Tilting composite wing aircraft taking multi-rotor wing framework as main part
一种以多旋翼构架为主的倾转复合翼飞行器
2021-06-01
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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