Convenient-to-install unmanned aerial vehicle wind resisting structure
A technology of drones and fans, which is applied to aircraft parts, transportation and packaging, and aircraft indicating devices, etc. It can solve the problems of poor wind resistance of drones, reduce vibration, reduce noise, and increase wind resistance The effect of intensity
Inactive Publication Date: 2019-02-26
HENAN HUANQIU AVIATION EQUIP TECH CO LTD
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Problems solved by technology
[0004] The purpose of the present invention is to provide an easy-to-install wind-resistant structure for unmanned aerial vehicles to solve the problem of poor wind-resistant performance of existing unmanned aerial vehicles proposed in the above-mentioned background technology
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[0019] 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. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without making creative efforts belong to the protection scope of the present invention.
[0020] see Figure 1-6 , the present invention provides a technical solution: an easy-to-install UAV wind-resistant structure, including a first chute 1, a fixed rod 3 and a fan 7, the inside of the first chute 1 is provided with a vibration-damping support base 8, And the first chute 1 is connected with the support rod 12 through the rotating shaft 11, the vibration-damping support base 8 is a porous structure, and the vibration-damping support base 8 is conn...
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The invention discloses a convenient-to-install unmanned aerial vehicle wind resisting structure. The structure comprises a first sliding groove, a fixing rod and a fan, the inner side of the first sliding groove is provided with a shock-absorbing supporting base, the first sliding groove is connected with a supporting rod through a rotary shaft, the upper end of the supporting rod is connected with a connecting rod, the outer side of the connecting is welded to a nut, the fixing rod penetrates through a rotary disc to be connected with an adjusting rod, the fixing rod and the adjusting rod are provided with a locking hole and a locking block respectively, second sliding grooves are formed in the lower surfaces of the fixing rod and the adjusting rod, the interiors of the fixing rod and the adjusting rod are connected with a sleeve rod and a third gear rod respectively, and the front end of the adjusting rod is connected with a protecting housing. The structure has the advantages thatby adopting the design of a first sliding groove, the rotary disc, the adjusting rod, the fan, the shock-absorbing supporting base, the connecting rod, the rotary shaft, the second sliding grooves anda transmission structure, thrusting force opposite to the direction of strong wind can be provided, and the wind resisting strength of the unmanned aerial vehicle is conveniently improved.
Description
technical field [0001] The invention relates to the technical field related to drones, in particular to a wind-resistant structure for drones that is easy to install. Background technique [0002] Unmanned aircraft, referred to as unmanned aerial vehicle, is an unmanned aircraft controlled by radio remote control equipment and its own program control device. [0003] However, due to its small size and light weight, the existing unmanned aerial vehicle will inevitably be affected by strong winds when flying in the air. In order to ensure that the unmanned aerial vehicle can fly stably in the air, it is necessary to study and design an unmanned aerial vehicle Man-machine wind-resistant structure, in order to enhance the wind-resistant performance of the UAV. Contents of the invention [0004] The purpose of the present invention is to provide an easy-to-install wind-resistant structure for unmanned aerial vehicles, so as to solve the problem of poor wind-resistant performan...
Claims
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Login to View More IPC IPC(8): B64D45/00
CPCB64D45/00
Inventor 王飞
Owner HENAN HUANQIU AVIATION EQUIP TECH CO LTD