Unmanned aerial vehicle with structure for adjusting folding and unfolding of wings
A technology for adjusting the structure and folding wings, applied in the field of unmanned aerial vehicles, can solve the problems of not being able to fold the wings, increase the workload, etc., and achieve the effect of reducing the shaking of the gimbal
Inactive Publication Date: 2020-09-22
东莞市奇趣机器人科技有限公司
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Problems solved by technology
[0003] There are certain disadvantages in the use of existing drones. Most drones are produced with fixed wings, and when the wings need to be repaired, the overall shell needs to be replaced or repaired to increase the cost. In order to reduce the workload, when flying, if there is a narrow space in front to pass, the wings cannot be folded. Therefore, we provide a UAV with a wing folding and stretching adjustment structure
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[0027] The following will clearly and completely describe the technical solutions in the embodiments of the present invention with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only some of the embodiments of the present invention, not all of them.
[0028] In the description of the present invention, unless otherwise stated, the meaning of "plurality" is two or more; the terms "upper", "lower", "left", "right", "inner", "outer" , "front end", "rear end", "head", "tail", etc. indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than Indicates or implies that the device or element referred to must have a particular orientation, be constructed and operate in a particular orientation, and therefore should not be construed a...
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The invention discloses an unmanned aerial vehicle with a structure for adjusting folding and unfolding of wings. Specifically, the unmanned aerial vehicle comprises a main engine room, rotor arm assemblies, a power assembly and a cloud platform assembly, wherein a hatch cover is arranged above the main engine room; the rotor arm assemblies are installed on the two sides of the main engine room correspondingly; a mounting box is arranged at the bottom of the main engine room; a propeller is mounted above the power assembly; a front-side position indicating lamp is mounted at the front part ofthe outer side of the mounting box; and a cloud platform is arranged below the cloud platform assembly. According to the unmanned aerial vehicle with the structure for adjusting folding and unfoldingof wings in the invention, different positions of the body of the unmanned aerial vehicle are respectively provided with a top position indicating lamp, the front-side position indicating lamp and a rear-side position indicating lamp, and the light colors of the three position indicating lamps are different, so an operator can find the position of the unmanned aerial vehicle in a dark environmentto judge the flight form of the unmanned aerial vehicle; and through stretching of a telescopic rod, a wedging block in the power assembly can be driven to be embedded into or disengaged from a wedging groove so as to complete limiting of the power assembly.
Description
technical field [0001] The invention relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle with a wing folding and extending adjustment structure. Background technique [0002] Unmanned aircraft, referred to as "unmanned aerial vehicle", or "UAV" in English, is an unmanned aircraft that is controlled by radio remote control equipment and its own program control device, or is completely or intermittently operated autonomously by an on-board computer. [0003] There are certain disadvantages in the use of existing drones. Most drones are produced with fixed wings, and when the wings need to be repaired, the overall shell needs to be replaced or repaired to increase the cost. In order to reduce the workload, when flying, if there is a narrow space in front to pass, the wings cannot be folded. Therefore, we provide a drone with a wing folding and stretching adjustment structure. Contents of the invention [0004] Aiming at the...
Claims
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IPC IPC(8): B64C27/08B64C1/30B64C27/14B64C27/52B64D27/26B64D47/06B64D47/08B64D27/40
CPCB64C27/08B64C1/30B64C27/14B64C27/52B64D47/06B64D47/08B64U10/10B64U50/19B64U2101/30B64D27/40
Inventor 陈海华胡常华
Owner 东莞市奇趣机器人科技有限公司