Unmanned aerial vehicle pan-tilt quick release structure

• Main Authors: FU WANLONG, DU JIAN, ZHOU TENGJUN
• Format: Patent
• Language: Chinese; English
• Published: 12.11.2019
• Subjects: AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The utility model belongs to the field of unmanned aerial vehicles. The utility model provides a quick release structure of an unmanned aerial vehicle pan-tilt. The device comprises an unmanned aerialvehicle fixing end and a holder plugboard end. The airplane fixing end is matched with the pan-tilt plugboard end; dovetail grooves are respectively formed in two sides of the upper hanging plate; the distance between the dovetail grooves is greater than the width of a lower insertion plate in the holder insertion plate end; the lower inserting plate can be inserted into the dovetail groove and then makes contact with the lower end of the dovetail groove. A movable sliding block is arranged on the outer side of the dovetail groove in one side of the lock tongue upper hanging plate, the outerside of the sliding block is wrapped by a sliding block cover, the sliding block cover is fixed to the upper hanging plate, a first threaded hole is formed in the sliding block cover, a screw rod is arranged in the first threa