SUPPORT FRAME FITTING STRUCTURE

• Main Authors: LI, Kunhuang, CHEN, Zenan, ZHOU, Lijia, HE, Ruijiang
• Format: Patent
• Language: Chinese; English; French
• Published: 24.12.2020
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; COSMONAUTICS; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; HELICOPTERS; PARACHUTES; PERFORMING OPERATIONS; TRANSPORTING

The present invention relates to the technical field of unmanned aerial vehicles, and particularly relates to a support frame fitting structure, comprising: a housing provided with a fastening block at a base thereof; a support frame, wherein a mounting portion engageable with the fastening block is provided at a top end of the support frame, and insertion connection holes are provided at corresponding positions of the mounting portion and the fastening block, respectively; and a quick release pin capable of being inserted into the insertion connection holes, wherein the fastening block is connected and fastened to the mounting portion via the quick release pin, the quick release pin is provided with a button, and the quick release pin is released from the insertion connection holes when the button is pressed, such that the mounting portion is released from the fastening block. The support frame fitting structure provided by the present application enables the following operations when the support frame needs