Aircraft with slow descending mechanisms

An aircraft and slow descent technology, applied in the field of aircraft, can solve problems such as unstable airflow, crash, UAV failure, etc., and achieve the effect of reducing collisions

Active Publication Date: 2020-04-21
邱南昌
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] As previously mentioned, the existing fail-safe UAV 9 utilizes the two inflatable airbags 93 as a buffer, but the two inflatable airbags 93 are installed on the base 91 and are exposed to the outside. 93 may be broken due to collision or scratching of foreign objects, so that the gas cannot be filled in the inflatable airbag and achi

Method used

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  • Aircraft with slow descending mechanisms
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Embodiment Construction

[0062] In order to make the above-mentioned and other purposes, features and advantages of the present invention more obvious and understandable, the following is based on preferred embodiments of the present invention, and is described in detail as follows in conjunction with the accompanying drawings:

[0063] Please refer to figure 2 As shown, it is a preferred embodiment of the aircraft with a slow-down mechanism of the present invention, including a base 1, a judgment module 2 and a plurality of slow-down components 3, the base 1 has an accommodating space S, The judging module 2 is located in the accommodating space S, and the slow-down component 3 is combined with the base 1 .

[0064] The base 1 is used for erecting equipment or instruments and can be in various shapes. In this embodiment, the base has a first plate 1a and a second plate 1b, and there is a space between the first plate 1a and the second plate 1b to form the accommodating space S, the space can be, fo...

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Abstract

An aircraft with slow descending mechanisms is used for solving the problem that an existing aircraft falls due to faults. The aircraft comprises: a base with an accommodating space, wherein an air storage tank is positioned in the accommodating space, the base is provided a plurality of arms, each arm is convexly arranged at the periphery of the base, one end of each arm convexly arranged at theperiphery of the base is respectively provided with a fixing frame, and a rotor wing part is combined with the fixing frame; a judgment module positioned in the accommodating space, wherein the judgment module is provided with an independent power source, the independent power source is electrically connected to a sensing unit and a processor, and the sensing unit is coupled to the processor; a plurality of slow descending mechanisms, wherein each slow descending assembly is combined with the corresponding fixing frame, each slow descending assembly is provided with a container, each containeris provided with a containing chamber for containing an air bag, and each container communicates with the air storage tank and the corresponding air bag through an inflation pipe.

Description

technical field [0001] The invention relates to an aircraft, especially an aircraft with a slow-down mechanism. Background technique [0002] In recent years, with the development of science and technology and the reduction of development costs, unmanned aerial vehicles have been widely used in entertainment, photography, long-term video recording, investigation, search and rescue, or agriculture. Features such as carrying items can work in places that humans cannot easily reach to complete many difficult tasks, which can save a lot of operating time and cost. In addition, depending on the purpose of use, unmanned aerial vehicles have different sizes, number of axes and control methods, but no matter what kind of unmanned aerial vehicle, it will be affected by weather and external factors, resulting in aircraft failure and control signal interruption. Then the aircraft will fall due to being out of control. [0003] Please refer to figure 1 As shown, it is a kind of exist...

Claims

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Application Information

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IPC IPC(8): B64C25/56B64D17/80B64D17/78
CPCB64C25/56B64D17/78B64D17/80
Inventor 邱南昌
Owner 邱南昌
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