Deformable rolling aircraft

Abstract

The invention discloses a deformable rolling aircraft. The deformable rolling aircraft comprises a base body, a first wing part and a second wing part, two parallel rotors are arranged in the first wing part and the second wing part respectively; the locking mechanism is used for locking the first wing part, the second wing part and the base body; in the unfolded state, the locking mechanism unlocks the first wing part and the second wing part, the rotor wing is driven by the driving device to rotate, and the first wing part and the second wing part are unfolded towards the two sides away from the base body; after the deformable rolling aircraft lands, the rotor wings decelerate, so that the first wing parts and the second wing parts are folded towards the direction of the base body, and a spherical folded state is formed; in the folding state, the locking mechanism is triggered, the locking mechanism locks the first wing part and the second wing part with the base body, the rotating shaft of the rotor is changed from the vertical direction to the horizontal direction, and the rotor pushes the deformable rolling aircraft in the folding state to roll on the ground when rotating. The folding stable state can be kept, and the playing method diversity and interestingness of the aircraft are improved.

Description

Technical field [0001] The present invention relates to the technical field of aircraft, and more particularly to a deformable rolling aircraft. Background technique [0002] The existing four-axis aircraft can be achieved between the spherical translation and the unfolded state, usually after the spherical state is used for the landing, the expanded flight state is used in air. However, the technique of most of the prior art variable spherical four-axis aircraft is mainly concentrated in automatic correction functions behind the aircraft, and lacks research on more form of functional conversion after landing, making it possible to become spherical The four-axis aircraft function is single, lack of fun. Further, when the translation is lacking, the locking device is lacking, so that the aircraft is easily trembled, or because the impact to the ground causes the wing to be hit, affecting the mixing effect. [0003] Therefore, it is necessary to design a stable state capable of mai...

AI Technical Summary

Problems solved by technology

However, in the prior art, the technology of most of the four-axis aircraft that can be changed into a spherical shape mainly focuses on the automatic correction function after the aircraft lands, and there is a lack of research on more forms of functional conversion after landing, so that the four-axis aircraft that can be changed into a spherical shape The quadcopter has a single function and lacks fun

Moreover, in the folded state, there is no locking device, which makes the aircraft prone to tremors when it lands, or the wings are knocked open due to impact with the ground, which affects the folding effect

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