The invention belongs to the technical field of tilting rotorcrafts, and particularly relates to a tilting rotorcraft which comprises a fuselage and wings, the middles of the left end and the right end of each wing are each provided with a cavity hole and rotationally connected with an engine unit through the cavity holes, and main bodies of the engine units are horizontally blocked in the cavity holes or perpendicularly hung in the cavity holes through rotation; the neck parts of the engine units are clamped in U-shaped clamping grooves in the front end parts of the wings through rotation and extend to the outer parts of the front ends of the wings, the U-shaped clamping grooves extend to the middle parts of the front ends of the cavity holes, and the front end part and the rear end part of the fuselage are respectively provided and connected with a motor unit. According to the tilting rotorcraft, the safety problem that airfoils are impacted by airflow is solved, meanwhile, the problem that power is not matched during horizontal advancing and vertical lifting is solved, the problem that the bearing force of the roots of the airfoils is difficult to effectively control is also solved, the requirement for the strength of the airfoils is greatly lowered, and the flying safety of the tilting rotorcraft is guaranteed.

    本发明属于倾转旋翼机的技术领域,具体涉及一种倾转旋翼机,包括机身和机翼,所述机翼的左右两端中部各开设有一个腔洞并通过腔洞各旋转连接有一个发动机组,所述发动机组的主体通过旋转水平封堵于腔洞内或垂直悬挂于腔洞内,所述发动机组的颈部通过旋转卡设于机翼前端部的U型卡槽内并延伸至机翼的前端外部,所述U型卡槽延伸于腔洞的前端中部,所述机身的前后两端部各设置连接有一个电动机组。本发明在解决气流冲击机翼安全问题的,同时还解决了水平前行和垂直升降时功率不匹配的问题,同步也解决了机翼根部的承受力难以得到有效地控制的问题,大大降低了对机翼强度的要求,保证了倾转旋翼机飞行的安全性。


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    Title :

    Tilting rotorcraft


    Additional title:

    一种倾转旋翼机


    Contributors:

    Publication date :

    2024-11-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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