Luminous unmanned aerial vehicle wing
A technology for drones and wings, which is applied to wings, aircraft parts, chords/stringers, etc. It can solve the problems of heavy weight of wings and achieve high structural strength, weight reduction, and good connection stability.
Inactive Publication Date: 2018-05-15
南通霆川电子科技有限公司
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Problems solved by technology
[0003] However, due to the high strength of the current luminous drone wings, there are often a large number of ribs inside the wings, resulting in a large overall weight of the wings, which is difficult to meet the needs of the market.
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[0040] 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, not all, embodiments of the present invention. All other embodiments obtained by persons of ordinary skill in the art based on the embodiments of the present invention belong to the protection scope of the present invention.
[0041] Such as Figure 1-4 As shown, a luminous UAV wing includes an upper shell 1 and a lower shell 2, the back of the upper shell 1 and the lower shell 2 are all provided with carbon fiber cloth (not shown), and the upper shell Both the plate 1 and the lower shell plate 2 are bonded to the carbon fiber cloth on them respectively, and the outer surfaces of the upper shell plate 1 and the lower shell plate 2 are provided with a layer of fluorescent layer that is convenient for observing the c...
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The invention discloses a luminous unmanned aerial vehicle wing. The luminous unmanned aerial vehicle wing comprises an upper shell plate and a lower shell plate; carbon fiber cloth is arranged on theback sides of the upper shell plate and the lower shell plate; the upper shell plate and the lower shell plate adhere to the corresponding carbon fiber cloth; a cavity is formed between the upper shell plate and the lower shell plate; a wing rib and a connecting rod are arranged in the cavity; the wing rib and the connecting rod are hollow; the connecting rod penetrates through the wing rib; theconnecting rod is perpendicular to the wing rib; the connecting rod adheres to the wing rib; the wing rib adheres to the carbon fiber cloth; a connecting strip is arranged on the connecting rod; the connecting strip is hollow and arch-shaped; the connecting strip comprises a first connecting strip group, a second connecting strip group and a third connecting strip group; the two ends of the firstconnecting strip group, the second connecting strip group and the third connecting strip group are connected with the connecting rod; the vaults of the first connecting strip group and the second connecting strip group cling to the back side of the upper shell plate and the back side of the lower shell plate; the luminous unmanned aerial vehicle wing is lightweight.
Description
technical field [0001] The present invention relates to the technical field of unmanned aerial vehicles, in particular to a luminous unmanned aerial vehicle wing. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft controlled by radio remote control equipment and its own program control device. There is no cockpit on board, but equipment such as autopilot and program control device are installed. The personnel on the ground, on the ship, or at the remote control station of the parent aircraft track, locate, remotely control, telemeter and digitally transmit it through radar and other equipment. Under the radio control, it can take off like an ordinary aircraft or be launched into the air with a booster rocket, and it can also be taken into the air by the parent aircraft for flight. When recovering, it can automatically land in the same way as the common aircraft landing process, and can also be recovered by remote control with a p...
Claims
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IPC IPC(8): B64C3/00B64C3/18B64D47/02
CPCB64C3/00B64C3/18B64D47/02
Inventor 薛晨
Owner 南通霆川电子科技有限公司