The invention relates to the technical field of aircrafts, and concretely relates to a translational wing aircraft adjusting structure. The structure comprises a translational wing and a driving device, the translational wing comprises two wings and a rotating bearing, and the driving device is connected with the rotating bearing, so that the translational wing can move up and down in a reciprocating mode; and mounting shafts are symmetrically arranged on the two sides of the rotating bearing, the two wings are oppositely arranged on the two sides of the rotating bearing, deflection shaft sleeves are arranged on the wing roots of the wings, the deflection shaft sleeves are connected with the mounting shafts in a matched mode, and deflection controllers are arranged between the deflection shaft sleeves and the mounting shafts. The structure is reasonable in structure, the translation wing reciprocates up and down, the spoiler wing surface and air act to generate rotational motion, and the flapping wing surface generates lift force by combining the rotational motion and descending motion; and when the translational wing is started, the attack angle is close to 0 DEG, so that the rotating resistance is minimum, the starting time of the translational wing is shortened, the centrifugal force overcomes the action of the deflection controller to increase the attack angle, the lift force generated by the flapping wing surface is increased, and the output efficiency of the translational wing is improved.
本发明涉及飞行器技术领域,具体指一种平动翼飞行器调节结构;包括平动翼和驱动装置,所述平动翼包括两个翼翅和转动轴承,所述驱动装置与转动轴承连接从而使平动翼可往复上下运动;所述转动轴承的两侧对称设有安装轴,两个翼翅相对地设置在转动轴承的两侧,翼翅的翅根上设有偏转轴套,偏转轴套与安装轴配合连接,且偏转轴套与安装轴之间设有偏转控制器;本发明结构合理,平动翼上下往复运动,扰流翼面与空气作用产生旋转运动,扇动翼面结合旋转运动和下行运动产生升力;平动翼启动时的攻角接近0°使其旋转阻力最小从而缩短平动翼启动时间,离心力克服偏转控制器的作用使攻角变大,使扇动翼面产生的升力增加,提高平动翼的输出效率。
Translational wing aircraft adjusting structure
一种平动翼飞行器调节结构
2021-03-09
Patent
Elektronische Ressource
Chinesisch
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