Vertical take-off and landing fixed wing unmanned aerial vehicle capable of being quickly disassembled, folded and boxed
The invention relates to a vertical take-off and landing fixed wing unmanned aerial vehicle capable of being quickly disassembled, folded and boxed. The vertical take-off and landing fixed wing unmanned aerial vehicle comprises a fuselage, wherein the fuselage is connected with a left wing through a...
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Main Authors | , , , |
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Format | Patent |
Language | Chinese English |
Published |
19.11.2019
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Subjects | |
Online Access | Get full text |
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Summary: | The invention relates to a vertical take-off and landing fixed wing unmanned aerial vehicle capable of being quickly disassembled, folded and boxed. The vertical take-off and landing fixed wing unmanned aerial vehicle comprises a fuselage, wherein the fuselage is connected with a left wing through a left wing connecting buckle, the fuselage is connected with a right wing through a right wing connecting buckle, the rear end of the left wing is connected with a left tail pipe, the rear end of the right wing is connected with a right tail pipe, and a trapezoid tail wing is arranged between the left tail pipe and the right tail pipe. According to the vertical take-off and landing unmanned aerial vehicle, disassembly and assembly of wings and rapid folding and recovery of tailpipes are realized, the vertical take-off and landing unmanned aerial vehicle can be unfolded from a transportation state to a take-off preparation state within a short time, and the vertical take-off and landing unmanned aerial vehicle can b |
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Bibliography: | Application Number: CN201910847045 |