WO2021168743A1 - Unmanned aerial vehicle - Google Patents

Unmanned aerial vehicle Download PDF

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Publication number
WO2021168743A1
WO2021168743A1 PCT/CN2020/077004 CN2020077004W WO2021168743A1 WO 2021168743 A1 WO2021168743 A1 WO 2021168743A1 CN 2020077004 W CN2020077004 W CN 2020077004W WO 2021168743 A1 WO2021168743 A1 WO 2021168743A1
Authority
WO
WIPO (PCT)
Prior art keywords
mounting plate
lower mounting
counterweight
fuselage
aerial vehicle
Prior art date
Application number
PCT/CN2020/077004
Other languages
French (fr)
Chinese (zh)
Inventor
杨哲
Original Assignee
南京唐壹信息科技有限公司
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 南京唐壹信息科技有限公司 filed Critical 南京唐壹信息科技有限公司
Priority to PCT/CN2020/077004 priority Critical patent/WO2021168743A1/en
Publication of WO2021168743A1 publication Critical patent/WO2021168743A1/en

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
    • B64U20/00—Constructional aspects of UAVs
    • B64U20/70—Constructional aspects of the UAV body
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C17/00—Aircraft stabilisation not otherwise provided for
    • B64C17/02—Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D9/00—Equipment for handling freight; Equipment for facilitating passenger embarkation or the like

Definitions

  • the invention relates to an unmanned aerial vehicle.
  • UAVs are more and more widely used and can transport materials, especially for places with more complicated road environments.
  • UAVs transport materials, some materials are irregular, which will cause the center of gravity of the UAV to shift. It is not convenient for drones to take off. How to provide an unmanned aerial vehicle that can balance the center of gravity has become an urgent problem for those skilled in the art.
  • the present invention provides an unmanned aerial vehicle in order to solve the above-mentioned problems in the prior art.
  • an unmanned aerial vehicle including a fuselage, a rotor assembly arranged on the fuselage, and an electric control assembly for remotely controlling the rotor assembly
  • the fuselage includes an upper mounting plate and a lower mounting
  • the upper mounting plate and the lower mounting plate are arranged parallel to each other, a storage cavity is formed between the upper mounting plate and the lower mounting plate, and a number of fixed columns are fixed between the upper mounting plate and the lower mounting plate
  • the fixed column is perpendicular to the upper and lower mounting plates
  • the counterweight is detachably plugged into one or more fixed columns
  • the rotor assembly and the electric control assembly are fixedly connected to the bottom surface of the lower mounting plate.
  • the counterweight includes a metal block and a rubber block, the rubber block is arranged inside the metal block, and an insertion slot is provided on the counterweight block, and the insertion slot penetrates the metal block and the rubber block.
  • the metal block and the rubber block are both circular structures, and the insertion groove is arranged along the radial direction of the counterweight.
  • the upper mounting plate and the lower mounting plate are both rectangular plate structures, four mounting arms are evenly distributed on the lower mounting plate, and a rotor assembly is provided on each mounting arm.
  • the invention can facilitate the transportation of materials, and can be used for medical rescue, express delivery, fire rescue and other purposes.
  • the balance of the drone is ensured by adding or reducing counterweights.
  • the counterweight has a simple structure and is easy to install.
  • the self-elasticity of the rubber ensures the fixation and the use effect is good.
  • Figure 1 is a three-dimensional structure diagram of the present invention.
  • Figure 2 is a structural diagram of the counterweight in the present invention.
  • an unmanned aerial vehicle of the present invention includes a fuselage 1, a rotor assembly 2 provided on the fuselage 1, and an electric control assembly for remotely controlling the rotor assembly.
  • the fuselage 1 includes an upper mounting plate 11, a lower mounting plate 12, a fixed column 13, and a counterweight 14.
  • the upper mounting plate 11 and the lower mounting plate 12 are arranged parallel to each other, and a storage cavity is formed between the upper mounting plate 11 and the lower mounting plate 12 ,
  • a number of fixed posts 13 are fixed between the upper mounting plate 11 and the lower mounting plate 12.
  • the fixed posts 13 are perpendicular to the upper and lower mounting plates, and the counterweight 14 is detachably plugged into one or more fixed posts 13 ,
  • the rotor assembly 2 and the electric control assembly are both fixedly connected to the bottom surface of the lower mounting plate 12.
  • the counterweight 14 in the present invention includes a metal block 141 and a rubber block 142.
  • the rubber block 142 is provided on the inner side of the metal block 141.
  • the counterweight 14 is provided with an insertion slot 143 which penetrates the metal block 141. And rubber block 142.
  • the metal block 141 and the rubber block 142 both have a circular structure, and the insertion groove 143 is arranged along the radial direction of the counterweight 14.
  • the rubber block 142 itself is elastically hugged on the fixed post 13, that is, the rubber block 142 and the fixed post 13 are in an interference fit.
  • the upper mounting plate 11 and the lower mounting plate 12 are both rectangular plate structures, four mounting arms are evenly distributed on the lower mounting plate 12, and a rotor assembly 2 is provided on each mounting arm.
  • the invention can facilitate the transportation of materials, and can be used for medical rescue, express delivery, fire rescue and other purposes.
  • the balance of the drone is ensured by adding or reducing counterweights.
  • the counterweight has a simple structure and is easy to install.
  • the self-elasticity of the rubber ensures the fixation and the use effect is good.

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  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Mechanical Engineering (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

Disclosed is an unmanned aerial vehicle, comprising a fuselage (1), a rotor wing assembly (2) arranged on the fuselage (1), and an electric control assembly for remotely controlling the rotor wing assembly (2). The fuselage (1) comprises an upper mounting plate (11) and a lower mounting plate (12), which are arranged in parallel to each other, a storage cavity is provided between the upper mounting plate (11) and the lower mounting plate (12), a plurality of fixing columns (13) are fixed between the upper mounting plate (11) and the lower mounting plate (12), the fixing columns (13) are perpendicular to the upper mounting plate and the lower mounting plate, balancing weights (14) are detachably inserted into one or more fixing columns (13), and the rotor wing assembly (2) and the electric control assembly are fixedly connected to the bottom surface of the lower mounting plate (12). The unmanned aerial vehicle facilitates transportation of materials and can be used for medical rescue, express delivery, fire rescue etc., the balance of the unmanned aerial vehicle is guaranteed by increasing or decreasing the balancing weights (14) when objects are transported, and the balancing weights (14) are simple in structure and convenient to mount, can guarantee fixing by means of the elasticity of rubber, and achieve a good usage effect.

Description

一种无人机A kind of unmanned aerial vehicle 技术领域：Technical field:
本发明涉及一种无人机。The invention relates to an unmanned aerial vehicle.
背景技术：Background technique:
无人机的应用越来越广泛，可以输送物资，尤其是针对一些路面环境较为复杂的地方，无人机在运输物资时，由于有些物资形成不规则，会导致无人机的重心偏移，不方便无人机的起飞。如何提供一种可以平衡重心的无人机成为了本领域技术人员亟需解决的问题。UAVs are more and more widely used and can transport materials, especially for places with more complicated road environments. When UAVs transport materials, some materials are irregular, which will cause the center of gravity of the UAV to shift. It is not convenient for drones to take off. How to provide an unmanned aerial vehicle that can balance the center of gravity has become an urgent problem for those skilled in the art.
发明内容：Summary of the invention:
本发明是为了解决上述现有技术存在的问题而提供一种无人机。The present invention provides an unmanned aerial vehicle in order to solve the above-mentioned problems in the prior art.
本发明所采用的技术方案有：一种无人机，包括机身、设于机身上的旋翼组件以及对旋翼组件进行远程控制的电控制组件，所述机身包括上安装板、下安装板、固定柱和配重块，所述上安装板与下安装板相互平行设置，上安装板与下安装板之间形成置物腔，在上安装板与下安装板之间固定若干根固定柱，固定柱垂直于上、下安装板，配重块可拆卸地插接于一根或多根固定柱上，所述旋翼组件和电控制组件均固定连接在下安装板的底面上。The technical solution adopted by the present invention is: an unmanned aerial vehicle including a fuselage, a rotor assembly arranged on the fuselage, and an electric control assembly for remotely controlling the rotor assembly, the fuselage includes an upper mounting plate and a lower mounting The upper mounting plate and the lower mounting plate are arranged parallel to each other, a storage cavity is formed between the upper mounting plate and the lower mounting plate, and a number of fixed columns are fixed between the upper mounting plate and the lower mounting plate , The fixed column is perpendicular to the upper and lower mounting plates, the counterweight is detachably plugged into one or more fixed columns, and the rotor assembly and the electric control assembly are fixedly connected to the bottom surface of the lower mounting plate.
进一步地，所述配重块包括金属块和橡胶块，所述橡胶块设于金属块的内侧，在配重块上设有插接槽，所述插接槽贯穿于金属块和橡胶块。Further, the counterweight includes a metal block and a rubber block, the rubber block is arranged inside the metal block, and an insertion slot is provided on the counterweight block, and the insertion slot penetrates the metal block and the rubber block.
进一步地，所述金属块和橡胶块均为圆形结构，插接槽沿着配重块的径向方向设置。Further, the metal block and the rubber block are both circular structures, and the insertion groove is arranged along the radial direction of the counterweight.
进一步地，所述上安装板与下安装板均为矩形板结构，在下安装板上均布有四个安装臂，每个安装臂上设置一个旋翼组件。Further, the upper mounting plate and the lower mounting plate are both rectangular plate structures, four mounting arms are evenly distributed on the lower mounting plate, and a rotor assembly is provided on each mounting arm.
本发明具有如下有益效果：The present invention has the following beneficial effects:
本发明可以便于运输物资，可以作为医用救援、快递、消防救援等用途，在运输物品时，通过增减配重块保证无人机的平衡，配重块结构简单，配重块方便安装，通过橡胶的自身弹性保证固定，使用效果好。The invention can facilitate the transportation of materials, and can be used for medical rescue, express delivery, fire rescue and other purposes. When transporting goods, the balance of the drone is ensured by adding or reducing counterweights. The counterweight has a simple structure and is easy to install. The self-elasticity of the rubber ensures the fixation and the use effect is good.
附图说明：Description of the drawings:
图1为本发明三维结构图。Figure 1 is a three-dimensional structure diagram of the present invention.
图2为本发明中配重块的结构图。Figure 2 is a structural diagram of the counterweight in the present invention.
具体实施方式：Detailed ways:
下面结合附图对本发明作进一步的说明。The present invention will be further described below in conjunction with the accompanying drawings.
如图1和图2，本发明一种无人机，包括机身1、设于机身1上的旋翼组件2以及对旋翼组件进行远程控制的电控制组件。As shown in Figures 1 and 2, an unmanned aerial vehicle of the present invention includes a fuselage 1, a rotor assembly 2 provided on the fuselage 1, and an electric control assembly for remotely controlling the rotor assembly.
机身1包括上安装板11、下安装板12、固定柱13和配重块14，上安装板11与下安装板12相互平行设置，上安装板11与下安装板12之间形成置物腔，在上安装板11与下安装板12之间固定若干根固定柱13，固定柱13垂直于上、下安装板，配重块14可拆卸地插接于一根或多根固定柱13上，旋翼组件2和电控制组件均固定连接在下安装板12的底面上。The fuselage 1 includes an upper mounting plate 11, a lower mounting plate 12, a fixed column 13, and a counterweight 14. The upper mounting plate 11 and the lower mounting plate 12 are arranged parallel to each other, and a storage cavity is formed between the upper mounting plate 11 and the lower mounting plate 12 , A number of fixed posts 13 are fixed between the upper mounting plate 11 and the lower mounting plate 12. The fixed posts 13 are perpendicular to the upper and lower mounting plates, and the counterweight 14 is detachably plugged into one or more fixed posts 13 , The rotor assembly 2 and the electric control assembly are both fixedly connected to the bottom surface of the lower mounting plate 12.
本发明中的配重块14包括金属块141和橡胶块142，橡胶块142设于金属块141的内侧，在配重块14上设有插接槽143，插接槽143贯穿于金属块141和橡胶块142。The counterweight 14 in the present invention includes a metal block 141 and a rubber block 142. The rubber block 142 is provided on the inner side of the metal block 141. The counterweight 14 is provided with an insertion slot 143 which penetrates the metal block 141. And rubber block 142.
金属块141和橡胶块142均为圆形结构，插接槽143沿着配重块14的径向方向设置。The metal block 141 and the rubber block 142 both have a circular structure, and the insertion groove 143 is arranged along the radial direction of the counterweight 14.
配重块14在使用时，通过橡胶块142自身弹性抱紧在固定柱13上，即橡胶块142与固定柱13之间过盈配合。When the counterweight 14 is in use, the rubber block 142 itself is elastically hugged on the fixed post 13, that is, the rubber block 142 and the fixed post 13 are in an interference fit.
本发明中的上安装板11与下安装板12均为矩形板结构，在下安装板12上均布有四个安装臂，每个安装臂上设置一个旋翼组件2。In the present invention, the upper mounting plate 11 and the lower mounting plate 12 are both rectangular plate structures, four mounting arms are evenly distributed on the lower mounting plate 12, and a rotor assembly 2 is provided on each mounting arm.
本发明可以便于运输物资，可以作为医用救援、快递、消防救援等用途，在运输物品时，通过增减配重块保证无人机的平衡，配重块结构简单，配重块方便安装，通过橡胶的自身弹性保证固定，使用效果好。The invention can facilitate the transportation of materials, and can be used for medical rescue, express delivery, fire rescue and other purposes. When transporting goods, the balance of the drone is ensured by adding or reducing counterweights. The counterweight has a simple structure and is easy to install. The self-elasticity of the rubber ensures the fixation and the use effect is good.
以上所述仅是本发明的优选实施方式，应当指出，对于本技术领域的普通技术人员来说，在不脱离本发明原理的前提下还可以作出若干改进，这些改进也应视为本发明的保护范围。The above are only the preferred embodiments of the present invention. It should be pointed out that for those of ordinary skill in the art, several improvements can be made without departing from the principle of the present invention, and these improvements should also be regarded as the present invention. protected range.

Claims (4)

  1. 一种无人机，包括机身(1)、设于机身(1)上的旋翼组件(2)以及对旋翼组件进行远程控制的电控制组件，其特征在于：所述机身(1)包括上安装板(11)、下安装板(12)、固定柱(13)和配重块(14)，所述上安装板(11)与下安装板(12)相互平行设置，上安装板(11)与下安装板(12)之间形成置物腔，在上安装板(11)与下安装板(12)之间固定若干根固定柱(13)，固定柱(13)垂直于上、下安装板，配重块(14)可拆卸地插接于一根或多根固定柱(13)上，所述旋翼组件(2)和电控制组件均固定连接在下安装板(12)的底面上。An unmanned aerial vehicle, comprising a fuselage (1), a rotor assembly (2) arranged on the fuselage (1), and an electric control assembly for remotely controlling the rotor assembly, characterized in that: the fuselage (1) It includes an upper mounting plate (11), a lower mounting plate (12), a fixed column (13) and a counterweight (14). The upper mounting plate (11) and the lower mounting plate (12) are arranged parallel to each other, and the upper mounting plate A storage cavity is formed between (11) and the lower mounting plate (12), and a number of fixed posts (13) are fixed between the upper mounting plate (11) and the lower mounting plate (12). The fixed posts (13) are perpendicular to the upper and lower mounting plates (12). The lower mounting plate, the counterweight (14) is detachably plugged into one or more fixed posts (13), and the rotor assembly (2) and the electric control assembly are fixedly connected to the bottom surface of the lower mounting plate (12) superior.
  2. 如权利要求1所述的无人机，其特征在于：所述配重块(14)包括金属块(141)和橡胶块(142)，所述橡胶块(142)设于金属块(141)的内侧，在配重块(14)上设有插接槽(143)，所述插接槽(143)贯穿于金属块(141)和橡胶块(142)。The drone according to claim 1, wherein the counterweight (14) includes a metal block (141) and a rubber block (142), and the rubber block (142) is provided on the metal block (141). An insertion groove (143) is provided on the inner side of the counterweight (14), and the insertion groove (143) penetrates the metal block (141) and the rubber block (142).
  3. 如权利要求1所述的无人机，其特征在于：所述金属块(141)和橡胶块(142)均为圆形结构，插接槽(143)沿着配重块(14)的径向方向设置。The UAV according to claim 1, characterized in that: the metal block (141) and the rubber block (142) are both circular structures, and the insertion slot (143) is along the diameter of the counterweight (14). Set in the direction.
  4. 如权利要求1所述的无人机，其特征在于：所述上安装板(11)与下安装板(12)均为矩形板结构，在下安装板(12)上均布有四个安装臂，每个安装臂上设置一个旋翼组件(2)。The UAV according to claim 1, characterized in that: the upper mounting plate (11) and the lower mounting plate (12) are both rectangular plate structures, and four mounting arms are evenly distributed on the lower mounting plate (12) , Each mounting arm is provided with a rotor assembly (2).
PCT/CN2020/077004 2020-02-27 2020-02-27 Unmanned aerial vehicle WO2021168743A1 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115531767A (en) * 2022-09-30 2022-12-30 新兴际华集团有限公司 Fire extinguishing system based on self-balancing augmented and stabilized unmanned aerial vehicle

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104743106A (en) * 2015-04-08 2015-07-01 唐枫一 Multi-rotor unmanned aerial vehicle
CN205311892U (en) * 2015-12-30 2016-06-15 苏州妙旋无人机应用有限公司 Controllable formula unmanned aerial vehicle of focus
CN106218877A (en) * 2016-08-03 2016-12-14 安阳全丰航空植保科技股份有限公司 The dynamic many rotors plant protection unmanned plane during flying pose adjustment changeable device of oil
CN107600399A (en) * 2017-08-08 2018-01-19 芜湖通全科技有限公司 A kind of multi-rotor unmanned aerial vehicle accurately delivered for express delivery terminal
CN108128457A (en) * 2017-12-24 2018-06-08 中山市得高行知识产权中心（有限合伙） A kind of unmanned plane vertically soaring level(l)ing mechanism
CN109850138A (en) * 2017-11-30 2019-06-07 中光电智能机器人股份有限公司 Unmanned plane and its propeller
CN209514414U (en) * 2019-04-28 2019-10-18 昆山市建设工程质量检测中心 A kind of device assisting detection slab thickness using unmanned plane during flying
JP2019189227A (en) * 2017-11-06 2019-10-31 株式会社エアロネクスト Flying body and method for controlling flying body
WO2020017488A1 (en) * 2018-07-17 2020-01-23 株式会社プロドローン Unmanned aerial vehicle

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104743106A (en) * 2015-04-08 2015-07-01 唐枫一 Multi-rotor unmanned aerial vehicle
CN205311892U (en) * 2015-12-30 2016-06-15 苏州妙旋无人机应用有限公司 Controllable formula unmanned aerial vehicle of focus
CN106218877A (en) * 2016-08-03 2016-12-14 安阳全丰航空植保科技股份有限公司 The dynamic many rotors plant protection unmanned plane during flying pose adjustment changeable device of oil
CN107600399A (en) * 2017-08-08 2018-01-19 芜湖通全科技有限公司 A kind of multi-rotor unmanned aerial vehicle accurately delivered for express delivery terminal
JP2019189227A (en) * 2017-11-06 2019-10-31 株式会社エアロネクスト Flying body and method for controlling flying body
CN109850138A (en) * 2017-11-30 2019-06-07 中光电智能机器人股份有限公司 Unmanned plane and its propeller
CN108128457A (en) * 2017-12-24 2018-06-08 中山市得高行知识产权中心（有限合伙） A kind of unmanned plane vertically soaring level(l)ing mechanism
WO2020017488A1 (en) * 2018-07-17 2020-01-23 株式会社プロドローン Unmanned aerial vehicle
CN209514414U (en) * 2019-04-28 2019-10-18 昆山市建设工程质量检测中心 A kind of device assisting detection slab thickness using unmanned plane during flying

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115531767A (en) * 2022-09-30 2022-12-30 新兴际华集团有限公司 Fire extinguishing system based on self-balancing augmented and stabilized unmanned aerial vehicle

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