Vertical take-off and landing unmanned aerial vehicle equipment capable of generating power in air
A technology of vertical take-off and landing of unmanned aerial vehicles, which is applied in the direction of bird strike prevention equipment, emergency equipment, unmanned aircraft, etc., can solve the problem of lack of a good parachute mechanism, and achieve the effect of avoiding the crash of the airframe and protecting the airframe
Pending Publication Date: 2020-09-11
广东国安通航智能航空技术发展有限公司
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Problems solved by technology
[0004] Aiming at the deficiencies of the prior art, the present invention provides a vertical take-off and landing UAV device that can generate electricity in the air, which solves the problem that the UAV device does not have a better parachute mechanism
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[0024] 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.
[0025] see Figure 1-3 , the present invention provides a technical solution: a vertical take-off and landing unmanned aerial vehicle device that can generate electricity in the air, including a body 1, and wings 4 are fixedly installed around the annular outer surface of the body 1, and fixed at the inner edge of the wing 4 A rotating motor 11 is installed, and the output end of the rotating motor 11 is fixedly connected with a propeller 5, a fixed disc 2 is ...
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The invention discloses vertical take-off and landing unmanned aerial vehicle equipment capable of generating power in the air. The invention relates to the technical field of vertical take-off and landing unmanned aerial vehicles. The equipment comprises a machine body, wings are fixedly mounted at the peripheral positions of the annular outer surface of the aircraft body; a rotating motor is fixedly mounted at the inner edge of each wing; the output end of the rotating motor is fixedly connected with a propeller; a fixed disc is fixedly mounted on the outer surface of the upper end of the machine body; a photovoltaic solar panel is fixedly installed in the fixed disc, a fixed cylinder is fixedly installed on the outer surface of the lower end of the machine body, a storage battery is fixedly installed at the position, close to the upper end, in the machine body, and an inverter is fixedly installed at the position, below the storage battery, in the machine body. According to the device, the machine body can slowly fall to the ground, the machine body is effectively protected and prevented from being crashed, and through the deformation effect of the first springs and the second springs, shock absorption can be effectively conducted on the machine body, and circuit elements in the machine body are protected.
Description
technical field [0001] The invention relates to the technical field of vertical take-off and landing unmanned aerial vehicles, in particular to a vertical take-off and landing unmanned aerial vehicle equipment capable of generating electricity in the air. Background technique [0002] Unmanned aircraft, referred to as "UAV", is an unmanned aircraft operated by radio remote control equipment and its own program control device; , monitoring infectious diseases, surveying and mapping, news reports, power inspections, disaster relief, film and television shooting, and romantic manufacturing applications have greatly expanded the use of drones themselves. Developed countries are also actively expanding industry applications and developing drones Technology, there are more and more types of drones, and the existing vertical take-off and landing drones can also effectively use solar energy to generate electricity in the air, and store them in the energy storage power supply for use...
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IPC IPC(8): B64C25/62B64D17/80B64D45/00
CPCB64C25/62B64D17/80B64D45/00B64D2045/0095B64U10/10B64U30/20B64U50/19Y02T50/50
Inventor 郑敏辉
Owner 广东国安通航智能航空技术发展有限公司