Multipurpose unmanned aerial vehicle

A kind of unmanned aircraft and multi-purpose technology, which is applied in the direction of aircraft parts, aircraft control, and the influence of air flow passing through the surface of the aircraft. It can solve the problem of service life affecting the heating of electronic components, the inability to achieve multi-functional expansion, and high purchase and use costs. problems, to achieve the effect of superior practicability, simple structure and beautiful appearance

Pending Publication Date: 2016-10-12
珠海银通无人机科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Existing UAVs have a single function and cannot perform a variety of operations. When multi-functional use is required, a variety of UAVs need to be purchased. The cost of purchase and use is high, and multi-functional expansion cannot be achieved; and the existing The service life of the UAV is affected by the heating of electronic components. Heat dissipation is the primary problem to be solved. Generally, the airflow is driven by a fan, which consumes more power, and increases the weight of the fuselage, resulting in poor operational stability.

Method used

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  • Multipurpose unmanned aerial vehicle
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  • Multipurpose unmanned aerial vehicle

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Embodiment Construction

[0023] Embodiments of the present invention are described in detail below, examples of which are shown in the drawings, wherein the same or similar reference numerals represent the same or similar elements or elements having the same or similar functions throughout.

[0024] In the description of the present invention, it should be noted that for orientation words, such as the term "center", "horizontal", "longitudinal", "length", "width", "thickness", "upper", "lower" , "Front", "Back", "Left", "Right", "Vertical", "Horizontal", "Top", "Bottom", "Inner", "Outer", "Clockwise", "Counterclockwise " and other indication orientations and positional relationships are based on the orientations or positional relationships shown in the drawings, and are only for the convenience of describing the present invention and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, or in a specific orientation. The...

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Abstract

A multipurpose unmanned aerial vehicle comprises a drive main unit and a functional auxiliary unit detachably fitted to the drive main unit; the drive main unit comprises a case, a plurality of releasable foldable arms and a top cover covering the case, one end of every arm is connected with the case, and a rotor is disposed above the other end of each arm; the bottom of the case is provided with a radiating block, and the bottom or sidewall of the case is provided with a mounting structure for connecting the functional auxiliary unit. The multipurpose unmanned aerial vehicle is simple in structure, good in safety, low in manufacture cost and suitable for quick mounting and connection; the vehicle is firm and reliable to connect and good in radiating performance, effectively prolonging its service time and life; the vehicle has good bearing performance, simple in design, simple to mount and attractive in appearance, may be converted to be multifunctional to adapt various operation needs, and has multiple purposes; therefore, the vehicle is a product good in technicality, practicality and economy.

Description

【Technical field】 [0001] The invention relates to a multipurpose unmanned aircraft. 【Background technique】 [0002] Existing UAVs have a single function and cannot perform a variety of operations. When multi-functional use is required, a variety of UAVs need to be purchased. The cost of purchase and use is high, and multi-functional expansion cannot be achieved; and the existing The service life of the drone is affected by the heating of the electronic components, and heat dissipation is the primary problem to be solved. Generally, the airflow is driven by a fan, which consumes more power, and increases the weight of the fuselage, resulting in poor operational stability. [0003] In order to overcome the above-mentioned problems, we have developed a multi-purpose unmanned aircraft. 【Content of invention】 [0004] The technical problem to be solved by the purpose of this invention is to provide a kind of unmanned aircraft with multiple uses, which has simple structure, goo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/06B64C1/30B64D1/18B64D47/08B64D47/02
CPCB64C1/063B64C1/30B64D1/18B64D47/02B64D47/08
Inventor 黄彰标
Owner 珠海银通无人机科技有限公司
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