Unmanned aerial vehicle body prepared from composite material, and preparation method thereof
A composite material and UAV technology, applied in the field of UAV body and its preparation, can solve the problems of long time consumption, heavy body weight, and reducing the structural strength of UAV, and achieve excellent tensile strength and tear resistance , Reduce maintenance costs and cycles, and the effect of strong applicability in appearance design
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[0035] The preparation method of the unmanned aerial vehicle body of the embodiment of the present invention, the preparation method comprises the following steps:
[0036] In the preheated forming upper mold, paste the layered connection material in the fuselage or wing group, and eliminate the edge;
[0037] In the preheated molding lower mold, stick the layered connection material in the fuselage or wing group, put the insert, install the air duct, and close the upper mold and the lower mold;
[0038] Thermoforming.
[0039] In order to make the above and other purposes, features, and advantages of the present invention more comprehensible, several examples are given below to illustrate the UAV body made of composite materials and its preparation method according to the present invention.
Embodiment 1
[0041] Such as figure 1 As shown, the UAV body made of composite materials in Example 1 of the present invention includes a fuselage 1 and a wing group, and the wing group includes a main wing 2 and an empennage 3 respectively arranged on both sides of the fuselage. The two sides of the wing 2 are connected with the first and second wings 4, 5; the materials of the fuselage and the wing group are in a layered structure; cloth, the first polyvinyl chloride cloth and the third carbon fiber cloth; the materials of the main wing 2 and the first and second side wings 4, 5 respectively include the first carbon fiber cloth, the first polyvinyl chloride cloth and the first carbon fiber cloth connected in layers successively. The second carbon fiber cloth; the material of the empennage 3 includes the first carbon fiber cloth, the first polyvinyl chloride cloth and the second carbon fiber cloth which are sequentially connected in layers.
[0042]In the materials for preparing the fusel...
Embodiment 2
[0054] Such as figure 1 As shown, the UAV body made of composite materials in Example 2 of the present invention includes a fuselage 1 and a wing group, and the wing group includes a main wing 2 and an empennage 3 respectively arranged on both sides of the fuselage. The two sides of the wing 2 are connected with the first and second wings 4, 5; the materials of the fuselage and the wing group are in a layered structure; cloth, the first polyvinyl chloride cloth and the third carbon fiber cloth; the materials of the main wing 2 and the first and second side wings 4, 5 respectively include the first carbon fiber cloth, the first polyvinyl chloride cloth and the first carbon fiber cloth connected in layers successively. The second carbon fiber cloth; the material of the empennage 3 includes the first carbon fiber cloth, the first polyvinyl chloride cloth and the second carbon fiber cloth which are sequentially connected in layers.
[0055] In the materials for preparing the fuse...
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