Carbon fiber component folding structure for a drone

Abstract

The utility model discloses a carbon fiber component folding structure of unmanned plane, including upper fixed plate, lower fixed plate and rotating plate, upper fixed plate, lower fixed plate and rotating plate are carbon fiber material, and upper fixed plate and lower fixed plate are provided with upper air-avoiding groove and lower air-avoiding groove respectively along the end of its carbon fiber length direction, upper air-avoiding groove and lower air-avoiding groove combine and constitute air-avoiding area, and the both sides of air-avoiding area are provided with rotating groove respectively, the end of rotating plate is connected with the rotating shaft, and the both ends of rotating shaft respectively extend into rotating groove and can rotatable connection. The utility model discloses upper fixed plate, lower fixed plate and rotating plate are vertical folding structure. Upper air-avoiding groove, lower air-avoiding groove and rotating groove can be through respectively first to upper fixed plate and lower fixed plate are processed, and after loading rotating plate and rotating shaft, then again the compound of upper fixed plate and lower fixed plate, need not to implant the rotating structure between the metal, and the processing difficulty is low, and the weight of finished product is effectively avoided and increases excessively, and the stability and reliability of unmanned plane flight are ensured.

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