CN106787231A - A kind of unmanned plane automatic charge device and its charging method - Google Patents
A kind of unmanned plane automatic charge device and its charging method Download PDFInfo
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Abstract
一种无人机自动充电装置及其充电方法,采用底板、定位装置、驱动装置、锁紧装置和充电装置的结构设计,利用科学优化的充电方法;大大改善了现有无人机充电技术的不足,所述定位装置用于无人机降落时的定位,保证无人机安全准确的降落在专用卡槽内;所述驱动装置为锁紧装置提供相关动力;所述锁紧装置用于完成对无人机的锁死固定工作,并将充电电极准确对准无人机受电电极;充电装置:用于对无人机进行充电作业;本发明防雨防水,可以安装在任何高度和地方,无需人工干预;抗风性能良好,技术成熟、安全可靠、定位简单、成本低廉;标准构型设计,重量较轻、加工装配方便,适合于大批量生产。
An automatic charging device for an unmanned aerial vehicle and a charging method thereof, adopting a structural design of a base plate, a positioning device, a driving device, a locking device and a charging device, and utilizing a scientifically optimized charging method; greatly improving the efficiency of the existing unmanned aerial vehicle charging technology Insufficient, the positioning device is used for the positioning of the UAV when it lands, so as to ensure that the UAV lands safely and accurately in the special card slot; the driving device provides relevant power for the locking device; the locking device is used to complete Lock and fix the drone, and accurately align the charging electrode with the receiving electrode of the drone; charging device: used for charging the drone; the invention is rainproof and waterproof, and can be installed at any height and place , without manual intervention; good wind resistance performance, mature technology, safe and reliable, simple positioning, low cost; standard configuration design, light weight, easy processing and assembly, suitable for mass production.
Description
技术领域technical field
本发明属于充电技术领域,尤其是一种无人机自动充电装置及其充电方法。The invention belongs to the technical field of charging, in particular to an automatic charging device for an unmanned aerial vehicle and a charging method thereof.
背景技术Background technique
无线充电可以让人们的生活更加便捷,可以消除电源插接可能导致的虚接、电弧、电网波动、电能无效消耗等问题,在手机充电、电动车充电以及无人机充电等应用领域,越来越得到关注;Wireless charging can make people's life more convenient, and can eliminate problems such as virtual connections, arcs, grid fluctuations, and invalid power consumption that may be caused by power plugging. It is increasingly used in mobile phone charging, electric vehicle charging, and drone charging. get more attention;
无人机是一种历史悠久的飞行器具,以前主要是运用在一些环境恶劣、危险性很高的工作领域,由于使用的范围很小,所以没有大量普及运用。近年来,各国都加大了对无人机的研发和投入,大大提升了无人机的技术和性能,扩大了无人机的使用范围,特别是在民用领域获得了长足的发展,在提高工作效率,加强人身安全保障等方面,有着不可替代的优势。无人机的发展也是推陈出新,方兴未艾,呈现出了一片欣欣向荣的景象。目前开发的无人机主要有:地图测绘景街拍摄无人机、地质勘测无人机、自然灾害监测无人机、低空气象探测无人机、空中交通管制无人机、边境控制无人机、通信中继无人机、农业害虫监测、农药喷洒无人机、海洋监测无人机、绿化环保无人机,野生动物追踪及监测无人机;快速邮递业务无人机、航空体育摄影无人机、高压电力巡检无人机等,几乎渗透到了我们日常生活和工作的方方面面;UAV is a kind of flying equipment with a long history. It was mainly used in some harsh environments and high-risk work fields in the past. Due to the small range of use, it has not been widely used. In recent years, countries have increased research and development and investment in UAVs, greatly improving the technology and performance of UAVs, and expanding the scope of use of UAVs, especially in the civilian field. It has irreplaceable advantages in terms of work efficiency and personal safety protection. The development of drones is also in the ascendant, presenting a thriving scene. The currently developed drones mainly include: map surveying and mapping street shooting drones, geological survey drones, natural disaster monitoring drones, low-altitude meteorological detection drones, air traffic control drones, and border control drones , communication relay drones, agricultural pest monitoring, pesticide spraying drones, marine monitoring drones, greening and environmental protection drones, wildlife tracking and monitoring drones; express mail business drones, aviation sports photography Human-machine, high-voltage power inspection drones, etc., have penetrated into almost every aspect of our daily life and work;
无人机有许多得天独厚的优势:不受地面交通拥堵的影响,速度快,可以直接完成点对点的服务工作,因此效率高,但缺点也是很明显的:就是受无人机结构及重量的限制一般航程较短,不能完成连续长时间大航程的飞行要求,民用无人机尤甚;如何解决无人机在途中补充能量来完成后续的飞行任务问题,目前采用的主要方法是设置无人机自动充电装置,作为无人机中继获取能量的方便驿站;UAVs have many unique advantages: they are not affected by ground traffic congestion, they are fast, and they can directly complete point-to-point service work, so they are efficient, but the disadvantages are also obvious: they are limited by the structure and weight of UAVs. The voyage is short, and it cannot meet the flight requirements of continuous long-term and large voyages, especially for civilian UAVs; how to solve the problem of UAVs replenishing energy on the way to complete subsequent flight tasks, the main method currently used is to set UAVs to automatically The charging device is used as a convenient station for UAVs to relay and obtain energy;
目前国际国内主要有一下几种充电方式:At present, there are mainly several charging methods at home and abroad:
1.微波共振耦合方式:1. Microwave resonance coupling method:
优点是:采用非接触式充电,防水性和防尘性高;The advantages are: non-contact charging, high water resistance and dust resistance;
缺点是:不能防风抗风,由于是非接触式,充电时有损耗,效率不高,装置工作不稳定,尚在实验阶段;Disadvantages are: not windproof and windproof, because it is non-contact, there is loss when charging, the efficiency is not high, the device is unstable, and it is still in the experimental stage;
2.金属平板式充电方式:2. Metal plate charging method:
优点是:采用有线充电方式,充电效率高;The advantage is: the wired charging method is adopted, and the charging efficiency is high;
缺点是:采用触点完成充电,无人机不能锁死,不能抗风防水,必须安装有遮雨棚;The disadvantages are: the charging is completed by contacts, the drone cannot be locked, it cannot be windproof and waterproof, and must be installed with a canopy;
3.空中对接式充电方式:3. Air docking charging method:
充电头在空中受空气湍流影响不能准确定位,与无人机无法精确对接,因此在短期时间内不能使用,尚在实验阶段;The charging head cannot be accurately positioned in the air due to the influence of air turbulence, and it cannot be accurately docked with the drone, so it cannot be used in a short period of time and is still in the experimental stage;
4.利用高压输电线充电方式:4. Using high-voltage power lines to charge:
优点是:利用高压输电线路发出的磁场为无人机充电,无需设置充电装置,亦属于非接触式充电方式,主要运用于高压电力巡检领域;缺点是充电时间较长,受天气影响较大,运用领域较窄,目前尚处于概念阶段;The advantage is: use the magnetic field emitted by the high-voltage transmission line to charge the drone, no need to install a charging device, and it is also a non-contact charging method, which is mainly used in the field of high-voltage power inspection; the disadvantage is that the charging time is long and is greatly affected by the weather. , the field of application is relatively narrow, and it is still in the conceptual stage;
发明内容Contents of the invention
为了解决上述技术问题,本发明提供了一种无人机自动充电装置及其充电方法,该装置基于以上无人机充电装置的技术和市场现状,以简便、实用、安全可靠、成本低廉为理念,进而设计开发而成;满足了结构安全可靠,抗风防水防尘,操作简单,维护方便,无人值守,充电方法技术成熟等各项要求;In order to solve the above technical problems, the present invention provides a UAV automatic charging device and its charging method, which is based on the technology and market status of the UAV charging device above, with the concept of simplicity, practicality, safety, reliability and low cost , and then designed and developed; it meets the requirements of safe and reliable structure, windproof, waterproof and dustproof, simple operation, convenient maintenance, unattended, and mature charging method technology;
一种无人机自动充电装置及其充电方法,其中:An automatic charging device for an unmanned aerial vehicle and a charging method thereof, wherein:
一种无人机自动充电装置,包括:底板,还包括:定位装置、驱动装置、锁紧装置和充电装置;An automatic charging device for an unmanned aerial vehicle, comprising: a base plate, and also comprising: a positioning device, a driving device, a locking device and a charging device;
所述定位装置、驱动装置、锁紧装置和充电装置均设置在底板上;The positioning device, the driving device, the locking device and the charging device are all arranged on the bottom plate;
定位装置:负责无人机降落时的定位,保证无人机安全准确的降落在专用卡槽内;Positioning device: responsible for the positioning of the drone when it lands, ensuring that the drone lands safely and accurately in the dedicated card slot;
作为一种举例说明,所述定位装置包括:外壳、超声波传感器、机载控制电路和充电平台控制电路;As an example, the positioning device includes: a housing, an ultrasonic sensor, an onboard control circuit and a charging platform control circuit;
作为一种应用举例说明,所述机载控制电路和充电平台控制电路均采用现有控制单元,且其均不设置在该发明的机械结构内;As an application example, both the airborne control circuit and the charging platform control circuit use existing control units, and none of them are arranged in the mechanical structure of the invention;
所述超声波传感器安装在所述底板上,所述外壳安装在所述底板的专用固定孔上;The ultrasonic sensor is installed on the base plate, and the housing is installed on a special fixing hole of the base plate;
定位装置的运行原理:当无人机飞临充电装置的上空时,所述无人机本体自带的定位装置与充电平台上的所述定位装置,通过通讯信号的建立进行自动联络,保证无人机以正确的姿态,将着陆撬对准外壳上的专设凹槽降落,当四个接触开关闭合同时发出信号时,表明无人机已经正常降落,由锁紧装置迅速将无人机锁定,进行充电;The operating principle of the positioning device: when the drone flies over the charging device, the positioning device on the drone body and the positioning device on the charging platform will automatically communicate through the establishment of a communication signal to ensure that there is no With the correct posture, the man-machine aligns the landing skid with the special groove on the shell and lands. When the four contact switches are closed and a signal is sent at the same time, it indicates that the drone has landed normally, and the drone is quickly locked by the locking device. Lock and charge;
作为一种举例说明,所述专设凹槽的尺寸可根据不同种类的无人机着陆撬,进行相应的尺寸变换设计;As an example, the size of the special groove can be designed according to different types of UAV landing skids;
驱动装置:为锁紧装置提供相关动力;Driving device: provide relevant power for the locking device;
作为一种举例说明,所述驱动装置包括:传动齿轮、传动轴、齿轮键、联轴器、轴承座、中间轴承座、电机、接触开关、电机座;As an example, the driving device includes: a transmission gear, a transmission shaft, a gear key, a shaft coupling, a bearing seat, an intermediate bearing seat, a motor, a contact switch, and a motor seat;
所述电机座安装在所述底板的预设位置上,然后将所述电机安装在电机座的固定孔内,并依次安装中间轴承座和轴承座,将所述联轴器安装在电机轴上,将两个传动齿轮、安装在传动轴上的专用位置,并将齿轮键与传动轴固定;然后将所述传动轴的一端穿过齿条与联轴器安装,另一端安装在中间轴承座和轴承座上,调整齿轮位置与齿条啮合,将传动轴安装调到传动工作要求的状态;The motor seat is installed on the preset position of the bottom plate, then the motor is installed in the fixing hole of the motor seat, and the intermediate bearing seat and the bearing seat are installed in sequence, and the coupling is installed on the motor shaft , install the two transmission gears on the special position on the transmission shaft, and fix the gear key and the transmission shaft; then install one end of the transmission shaft through the rack and the coupling, and install the other end on the middle bearing seat And on the bearing seat, adjust the position of the gear to mesh with the rack, and adjust the installation of the transmission shaft to the state required by the transmission work;
作为一种举例说明,所述接触开关安装在底板上的预设位置,并与所述外壳的专设凹槽处相对应;As an example, the contact switch is installed at a preset position on the bottom plate and corresponds to a special groove of the housing;
驱动装置的运行原理:当无人机降落后,着陆撬落入外壳上设置的专用凹槽内,当四个接触开关同时闭合时,表明无人机着陆撬已经完全到位,所述充电平台控制电路接通所述电机电路,此时电机通电后根据控制要求自动执行顺时针或逆时针方向旋转,通过联轴器带动传动轴同步旋转,将力矩传递给传动齿轮并带动所述锁紧装置的齿条移动完成锁紧工作;The operating principle of the driving device: when the UAV lands, the landing skid falls into the special groove set on the shell, and when the four contact switches are closed at the same time, it indicates that the UAV landing skid has been fully in place, and the charging platform controls The circuit is connected to the motor circuit. At this time, the motor automatically rotates clockwise or counterclockwise according to the control requirements after being powered on. The drive shaft is driven to rotate synchronously through the coupling, and the torque is transmitted to the drive gear and drives the locking device. The rack moves to complete the locking work;
锁紧装置:完成对无人机的锁死固定工作,并将充电电极准确对准无人机受电电极;Locking device: complete the locking and fixing of the drone, and accurately align the charging electrode with the receiving electrode of the drone;
作为一种举例说明,所述锁紧装置包括:齿条安装座、齿条、垫板、U型抱卡、板簧、销轴、第二接触开关;As an example, the locking device includes: a rack mounting seat, a rack, a backing plate, a U-shaped clamp, a leaf spring, a pin shaft, and a second contact switch;
所述齿条安装座是齿条的安装机架,将两组齿条分别插装在齿条安装座的方孔内;所述垫板安装在齿条的一端,为所述板簧提供压缩阻力点,板簧套装在齿条的插销上,再将所述U型抱卡插孔插入齿条的插销上,然后将所述销轴穿入U型抱卡和齿条的长孔内,并穿入开口销将销轴固定,所述第二接触开关安装在所述底板的预设位置,用于检验锁紧装置是否完成锁紧工作的状态;The rack mounting base is the mounting frame of the rack, and two sets of racks are respectively inserted into the square holes of the rack mounting base; the backing plate is installed at one end of the rack to provide compression for the leaf spring. At the resistance point, the leaf spring is set on the pin of the rack, and then the U-shaped card jack is inserted into the pin of the rack, and then the pin shaft is inserted into the long hole of the U-shaped card and the rack. And pass through the cotter pin to fix the pin shaft, the second contact switch is installed at the preset position of the bottom plate, and is used to check whether the locking device has completed the locking work state;
锁紧装置运行原理:所述齿条在传动齿轮的带动下左右移动,通过板簧的弹力,推动U型抱卡朝无人机着陆撬方向移动。当U型抱卡到达锁死位置时,第二接触开关闭合,输出信号控制驱动装置停止工作,完成锁死动作;The operating principle of the locking device: the rack moves left and right under the drive of the transmission gear, and through the elastic force of the leaf spring, the U-shaped clamp is pushed towards the UAV landing skid. When the U-shaped locking card reaches the locked position, the second contact switch is closed, and the output signal controls the driving device to stop working, and the locking action is completed;
充电装置:用于对无人机进行充电作业;Charging device: used to charge the UAV;
作为一种举例说明,所述充电装置包括:电极座、充电电极、弹簧、接线座、接线端子以及充电控制电路;As an example, the charging device includes: an electrode holder, a charging electrode, a spring, a wiring holder, a connecting terminal and a charging control circuit;
所述弹簧套装在电极轴上,所述电极轴装入电极座上的预设方孔内并将轴伸出,在伸出的部分安装接线座,所述接线端子安装在接线座上,保证电极在预设方孔内能够自由活动,最后将组装好的电极座安装在U型抱卡上;The spring is set on the electrode shaft, the electrode shaft is put into the preset square hole on the electrode seat and the shaft is extended, and a terminal block is installed on the protruding part, and the terminal block is installed on the terminal block to ensure The electrode can move freely in the preset square hole, and finally install the assembled electrode holder on the U-shaped holding card;
充电装置的运行原理:所述充电装置安装在所述锁紧装置的U型抱卡上,并随着U型抱卡左右移动,在U型抱卡尚未锁紧无人机着陆撬时,所述电极先于U型抱卡接触安装在无人机着陆撬上的受电电极.并在弹簧的作用下,紧密与着陆撬上的受电电极接触;当U型抱卡锁紧无人机着陆撬时,通过锁紧装置的第二接触开关发出的信号,充电控制电路向充电电极加电,开始正式充电;当无人机充电完毕后,充电控制电路向充电平台控制电路发出解锁动作指令,U型抱卡自动返回初始位置,同时带动充电装置同步返回;完成充电动作;The operating principle of the charging device: the charging device is installed on the U-shaped holding card of the locking device, and moves left and right with the U-shaped holding card. When the U-shaped holding card has not locked the UAV landing skid, the The above-mentioned electrode is in contact with the receiving electrode installed on the landing skid of the UAV before the U-shaped clamping card. And under the action of the spring, it is in close contact with the receiving electrode on the landing skid; when the U-shaped clamping card locks the drone When landing the skid, through the signal sent by the second contact switch of the locking device, the charging control circuit powers up the charging electrode to start formal charging; when the UAV is fully charged, the charging control circuit sends an unlocking action command to the charging platform control circuit , the U-shaped holding card automatically returns to the initial position, and at the same time drives the charging device to return synchronously; the charging action is completed;
一种无人机自动充电方法,包括如下技术步骤:An automatic charging method for an unmanned aerial vehicle, comprising the following technical steps:
步骤一、无人机着落定位:Step 1. UAV landing and positioning:
①当无人机需要补充电能的时候,无人机在GPS信号的引导下,飞向最近的本发明之一种无人机自动充电装置;① When the UAV needs to supplement electric energy, the UAV will fly to the nearest automatic charging device for UAVs of the present invention under the guidance of the GPS signal;
②当无人机进入到超声波感知的范围内时,GPS导航信号自动切换到超声波定位的功能上来;在超声波定位信号的引导下,无人机自动调整降落方向和位置,并保持一定的位置精度,使着陆撬对准外壳上设置的专用凹槽缓缓降落,并在自身重力的牵引下落入凹槽内,使着陆撬准确的插入专用凹槽内,四个接触开关同时向平台控制电路发出无人机已经安全着陆并且进入预定卡槽位置,做好充电准备的信号;②When the UAV enters the range of ultrasonic perception, the GPS navigation signal automatically switches to the ultrasonic positioning function; under the guidance of the ultrasonic positioning signal, the UAV automatically adjusts the landing direction and position, and maintains a certain position accuracy , so that the landing skid is aligned with the special groove set on the shell and slowly lands, and falls into the groove under the traction of its own gravity, so that the landing skid can be accurately inserted into the special groove, and the four contact switches simultaneously send a signal to the platform control circuit. The UAV has landed safely and entered the predetermined card slot position, ready to charge the signal;
作为一种举例说明,所述凹槽的形状设计为倒梯形;As an example, the shape of the groove is designed as an inverted trapezoid;
作为一种举例说明,所述凹槽的底部还设置有排水孔,用于雨天雨水的及时排除,避免水位灌满凹槽后引起的短路现象;As an example, the bottom of the groove is also provided with a drainage hole, which is used for timely drainage of rainwater in rainy days, and avoids the short circuit phenomenon caused by the water level filling the groove;
作为一种举例说明,所述接触开关还可以采用位置开关或位置传感器中的一种或者组合模式;As an example, the contact switch can also adopt one or a combined mode of a position switch or a position sensor;
步骤二、驱动装置控制锁紧装置锁死;Step 2, the driving device controls the locking device to lock;
平台控制电路发出开关信号,电机得电旋转,驱动传动轴和齿轮转动,带动齿条左右运动,通过板簧的弹力,使U形卡槽将无人机着陆撬锁死在凹槽内,同时充电电极插入无人机着陆撬上的充电电极内,所述电极在弹簧提供的弹力下保持与充电电极紧密有效接触;The platform control circuit sends out a switch signal, the motor is energized to rotate, drives the transmission shaft and gear to rotate, drives the rack to move left and right, and through the elastic force of the leaf spring, the U-shaped card slot locks the UAV into the groove for landing, and at the same time The charging electrode is inserted into the charging electrode on the landing skid of the drone, and the electrode is kept in close and effective contact with the charging electrode under the elastic force provided by the spring;
步骤三、无人机充电;Step 3, UAV charging;
无人机被锁死后,第二接触开关发出准备就绪的信号,控制电机停止旋转,此时接通充电控制电路,为所述电极加电,开始为无人机电池充电;After the UAV is locked, the second contact switch sends a ready signal to control the motor to stop rotating. At this time, the charging control circuit is connected to power up the electrodes to start charging the UAV battery;
步骤四、无人机解锁飞离;Step 4, the drone unlocks and flies away;
当所述充电控制电路检测到无人机受电电池的电压达到额定值后,发出指令,自动切断充电电源,电极断电,然后驱动电机反向旋转,带动齿条移动,使U形卡槽缩回,同时充电电极随同U形卡槽同步缩回,对无人机的着陆撬实施解锁动作,无人机可随时重新起飞,完成后续的航程任务。When the charging control circuit detects that the voltage of the receiving battery of the drone reaches the rated value, an instruction is issued to automatically cut off the charging power supply, the electrodes are powered off, and then the motor is driven to rotate in reverse to drive the rack to move, so that the U-shaped card slot Retract, and at the same time, the charging electrode is retracted synchronously with the U-shaped card slot, and the landing skid of the drone is unlocked. The drone can take off again at any time to complete the subsequent voyage tasks.
有益效果:Beneficial effect:
1.本发明完全防雨防水,适合雨天等恶劣天气条件下进行正常充电工作;1. The invention is completely rainproof and waterproof, and is suitable for normal charging work under bad weather conditions such as rainy days;
2.可以安装在任何高度和地方,不需要人工进行干预;2. Can be installed at any height and place without manual intervention;
3.因为有锁死机构,抗风性能良好,只要无人机能够正常降落即可,不用考虑无人机被风吹动移走的问题;3. Because of the locking mechanism, the wind resistance performance is good, as long as the drone can land normally, there is no need to consider the problem of the drone being moved by the wind;
4.可以和国家电网、光伏发电站联合一起使用,组成集发电、充电一体的集成体系;4. It can be used together with the national grid and photovoltaic power stations to form an integrated system integrating power generation and charging;
5.技术成熟、安全可靠、定位简单、成本低廉;5. Mature technology, safe and reliable, simple positioning and low cost;
6.标准构型设计,重量较轻、加工装配方便,适合于大批量生产;6. Standard configuration design, light weight, convenient processing and assembly, suitable for mass production;
附图说明Description of drawings
图1为本发明一种无人机自动充电装置之充工作示意图Figure 1 is a schematic diagram of the charging operation of an automatic charging device for an unmanned aerial vehicle of the present invention
图2为本发明一种无人机自动充电装置之结构正向示意图Fig. 2 is a front schematic view of the structure of an automatic charging device for an unmanned aerial vehicle of the present invention
图3为本发明一种无人机自动充电装置之结构侧视示意图Figure 3 is a schematic side view of the structure of an automatic charging device for an unmanned aerial vehicle according to the present invention
图4为本发明一种无人机自动充电装置之整体结构俯视示意图Fig. 4 is a schematic top view of the overall structure of an automatic charging device for an unmanned aerial vehicle of the present invention
图5为本发明一种无人机自动充电装置之侧视示意图标号Ⅰ范围的三倍比例放大图Fig. 5 is a three-times scale enlarged view of a schematic side view of an automatic charging device for an unmanned aerial vehicle according to the present invention.
具体实施方式detailed description
下面,参考附图1至图5所示,一种无人机自动充电装置及其充电方法,其中:Next, with reference to accompanying drawings 1 to 5, an automatic charging device for an unmanned aerial vehicle and a charging method thereof, wherein:
一种无人机自动充电装置及其充电方法,其中:An automatic charging device for an unmanned aerial vehicle and a charging method thereof, wherein:
一种无人机自动充电装置,包括:底板022,还包括:定位装置、驱动装置、锁紧装置和充电装置;An automatic charging device for an unmanned aerial vehicle, including: a bottom plate 022, and also includes: a positioning device, a driving device, a locking device and a charging device;
定位装置:负责无人机降落时的定位,保证无人机安全准确的降落在专用卡槽内;Positioning device: responsible for the positioning of the drone when it lands, ensuring that the drone lands safely and accurately in the dedicated card slot;
作为一种举例说明,所述定位装置包括:外壳001、超声波传感器021、机载控制电路和充电平台控制电路;As an example, the positioning device includes: a housing 001, an ultrasonic sensor 021, an on-board control circuit and a charging platform control circuit;
作为一种应用举例说明,所述机载控制电路和充电平台控制电路均采用现有控制单元,且其均不设置在该发明的机械结构内;As an application example, both the airborne control circuit and the charging platform control circuit use existing control units, and none of them are arranged in the mechanical structure of the invention;
所述超声波传感器021安装在所述底板022上,所述外壳001安装在所述底板的专用固定孔上;The ultrasonic sensor 021 is installed on the base plate 022, and the housing 001 is installed on a special fixing hole of the base plate;
定位装置的运行原理:当无人飞临充电装置的上空时,所述无人机本体自带的定位装置与充电平台上的所述定位装置,通过通讯信号的建立进行自动联络,保证无人机以正确的姿态,将着陆撬对准外壳001上的专设凹槽降落,当四个接触开关020闭合同时发出信号时,表明无人机已经正常降落,由锁紧装置迅速将无人机锁定,进行充电;The operating principle of the positioning device: when no one is flying over the charging device, the positioning device on the drone body and the positioning device on the charging platform will automatically communicate through the establishment of a communication signal to ensure that no one is charged. With the correct posture, align the landing skid with the special groove on the shell 001 and land. When the four contact switches 020 are closed and send out a signal at the same time, it indicates that the drone has landed normally, and the locking device quickly locks the drone into place. Lock and charge;
作为一种举例说明,所述专设凹槽的尺寸可根据不同种类的无人机着陆撬,进行相应的尺寸变换设计;As an example, the size of the special groove can be designed according to different types of UAV landing skids;
驱动装置:为锁紧装置提供相关动力;Driving device: provide relevant power for the locking device;
作为一种举例说明,所述驱动装置包括:传动齿轮004、传动轴005、齿轮键006联轴器016、轴承座017、中间轴承座018、电机019、接触开关020、电机座023;As an example, the driving device includes: a transmission gear 004, a transmission shaft 005, a gear key 006, a coupling 016, a bearing seat 017, an intermediate bearing seat 018, a motor 019, a contact switch 020, and a motor seat 023;
所述电机座023安装在所述底板022的预设位置上,然后将所述电机019安装在电机座023的固定孔内,并依次安装中间轴承座018和轴承座017,将所述联轴器安装在电机轴上,将两个传动齿轮004、安装在传动轴005上的专用位置,并将齿轮键006与传动轴固定;然后将所述传动轴的一端穿过齿条与联轴器安装,另一端安装在中间轴承座018和轴承座017上,调整齿轮位置与齿条啮合,将传动轴安装调整到传动工作要求的状态;The motor base 023 is installed on the preset position of the base plate 022, and then the motor 019 is installed in the fixing hole of the motor base 023, and the intermediate bearing housing 018 and the bearing housing 017 are installed in sequence, and the shaft coupling Install the device on the motor shaft, install the two transmission gears 004 on the special position on the transmission shaft 005, and fix the gear key 006 and the transmission shaft; then pass one end of the transmission shaft through the rack and the coupling Installation, the other end is installed on the middle bearing seat 018 and bearing seat 017, adjust the gear position to mesh with the rack, and adjust the installation of the transmission shaft to the state required by the transmission work;
作为一种举例说明,所述接触开关020安装在底板022上的预设位置,并与所述外壳001的专设凹槽处相对应;As an example, the contact switch 020 is installed at a predetermined position on the bottom plate 022, and corresponds to a special groove of the housing 001;
驱动装置的运行原理:当无人机降落后,着陆撬落入外壳001上设置的专用凹槽内,当四个接触开关020同时闭合时,表明无人机着陆撬已经完全到位,所述充电平台控制电路接通所述电机电路,此时电机通电后根据控制要求自动执行顺时针或逆时针方向旋转,通过联轴器带动传动轴同步旋转,将力矩传递给传动齿轮并带动所述锁紧装置的齿条完成锁紧工作;The operating principle of the driving device: when the UAV lands, the landing skid falls into the special groove set on the casing 001, and when the four contact switches 020 are closed simultaneously, it indicates that the UAV landing skid has been fully in place, and the charging The platform control circuit is connected to the motor circuit. At this time, the motor automatically rotates clockwise or counterclockwise according to the control requirements after being powered on. The drive shaft is driven to rotate synchronously through the coupling, and the torque is transmitted to the drive gear and drives the lock. The rack of the device completes the locking work;
锁紧装置:完成对无人机的锁死固定工作,并将充电电极准确对准无人机受电电极;Locking device: complete the locking and fixing of the drone, and accurately align the charging electrode with the receiving electrode of the drone;
作为一种举例说明,所述锁紧装置包括:齿条安装座002、齿条003、垫板007、U型抱卡008、板簧009、销轴011、第二接触开关024;As an example, the locking device includes: a rack mount 002, a rack 003, a backing plate 007, a U-shaped clamp 008, a leaf spring 009, a pin shaft 011, and a second contact switch 024;
所述齿条安装座002是齿条003的安装机架,将两组齿条分别插装在齿条安装座的放孔内;所述垫板007安装在齿条的一端,为所述板簧009提供压缩阻力点,板簧套装在齿条的插销上,再将所述U型抱卡008插孔插入齿条的插销上,然后将所述销轴011穿入U型抱卡和齿条的长孔内,并穿入开口销将销轴固定,所述第二接触开关024安装在所述底板022的预设位置,用于检验锁紧装置是否完成锁紧工作的状态;The rack mounting base 002 is the mounting frame of the rack rack 003, and two groups of racks are respectively inserted into the holes of the rack mounting base; The spring 009 provides a compression resistance point, the leaf spring is set on the pin of the rack, and then the U-shaped holding card 008 jack is inserted into the pin of the rack, and then the pin shaft 011 is inserted into the U-shaped holding card and the tooth The long hole of the bar, and penetrate the cotter pin to fix the pin shaft, the second contact switch 024 is installed at the preset position of the bottom plate 022, and is used to check whether the locking device has completed the locking work state;
锁紧装置运行原理:所述齿条003在传动齿轮004的带动下左右移动,通过板簧的弹力,推动U型抱卡008朝无人机着陆撬方向移动。当U型抱卡008到达锁死位置时,第二接触开关024闭合,输出信号控制驱动装置停止工作,完成锁死动作;The operating principle of the locking device: the rack 003 moves left and right under the drive of the transmission gear 004, and through the elastic force of the leaf spring, pushes the U-shaped holding card 008 to move towards the UAV landing skid. When the U-shaped holding card 008 reaches the locking position, the second contact switch 024 is closed, and the output signal controls the driving device to stop working, and the locking action is completed;
充电装置:用于对无人机进行充电作业;Charging device: used to charge the UAV;
作为一种举例说明,所述充电装置包括:电极座010、充电电极012、弹簧013、接线座014、接线端子015以及充电控制电路;As an example, the charging device includes: an electrode holder 010, a charging electrode 012, a spring 013, a wire holder 014, a connection terminal 015 and a charging control circuit;
所述弹簧013套装在电极012轴上,所述电极轴装入电极座010上的预设方孔内并将轴伸出,在伸出的部分安装接线座014,所述接线端子015安装在接线座014上,保证电极012在预设方孔内能够自由活动,最后将组装好的电极座010安装在U型抱卡008上;The spring 013 is set on the shaft of the electrode 012, the electrode shaft is put into the preset square hole on the electrode holder 010 and the shaft is extended, and the terminal block 014 is installed on the protruding part, and the terminal block 015 is installed on the On the terminal block 014, ensure that the electrode 012 can move freely in the preset square hole, and finally install the assembled electrode seat 010 on the U-shaped holding card 008;
充电装置的运行原理:所述充电装置安装在所述锁紧装置的U型抱卡008上,并随着U型抱卡左右移动,在U型抱卡尚未锁紧无人机着陆撬时,所述电极012先于U型抱卡接触安装在无人机着陆撬上的受电电极.并在弹簧的作用下,紧密与着陆撬上的受电电极接触;当U型抱卡锁紧无人机着陆撬时,通过锁紧装置的第二接触开关024发出的信号,充电控制电路向充电电极加电,开始正式充电;当无人机充电完毕后,充电控制电路向充电平台控制电路发出解锁动作指令,U型抱卡自动返回初始位置,同时带动充电装置同步返回;完成充电动作;The operating principle of the charging device: the charging device is installed on the U-shaped holding card 008 of the locking device, and moves left and right with the U-shaped holding card. When the U-shaped holding card has not locked the UAV landing skid, The electrode 012 is in contact with the receiving electrode installed on the landing skid of the UAV before the U-shaped clamping card. Under the action of the spring, it is in close contact with the receiving electrode on the landing skid; when the U-shaped clamping card is locked, there is no When the man-machine lands on the pry, through the signal sent by the second contact switch 024 of the locking device, the charging control circuit powers up the charging electrode and begins formal charging; when the drone is fully charged, the charging control circuit sends a signal to the charging platform control circuit. Unlock the action command, the U-shaped card will automatically return to the initial position, and at the same time drive the charging device to return synchronously; complete the charging action;
作为一种举例说明,所述充电控制电路采用现有技术产品,本发明主要设计构思是采用现有控制单元实现特殊机械结构的工作效果;As an example, the charging control circuit adopts the product of the prior art, and the main design concept of the present invention is to use the existing control unit to realize the working effect of the special mechanical structure;
一种无人机自动充电方法,包括如下技术步骤:An automatic charging method for an unmanned aerial vehicle, comprising the following technical steps:
步骤一、无人机着落定位:Step 1. UAV landing and positioning:
①当无人机需要补充电能的时候,无人机在GPS信号的引导下,飞向最近的本发明之一种无人机自动充电装置;① When the UAV needs to supplement electric energy, the UAV will fly to the nearest automatic charging device for UAVs of the present invention under the guidance of the GPS signal;
②当无人机进入到超声波感知的范围内时,GPS导航信号自动切换到超声波定位的功能上来;在超声波定位信号的引导下,无人机自动调整降落方向和位置,并保持一定的位置精度,使着陆撬对准外壳上设置的专用凹槽缓缓降落,并在自身重力的牵引下落入凹槽内,使着陆撬准确的插入专用凹槽内,四个接触开关同时向平台控制电路发出无人机已经安全着陆并且进入预定卡槽位置,做好充电的准备工作;②When the UAV enters the range of ultrasonic perception, the GPS navigation signal automatically switches to the ultrasonic positioning function; under the guidance of the ultrasonic positioning signal, the UAV automatically adjusts the landing direction and position, and maintains a certain position accuracy , so that the landing skid is aligned with the special groove set on the shell and slowly lands, and falls into the groove under the traction of its own gravity, so that the landing skid can be accurately inserted into the special groove, and the four contact switches simultaneously send a signal to the platform control circuit. The UAV has landed safely and entered the predetermined card slot position, and is ready for charging;
作为一种举例说明,所述凹槽的形状设计为倒梯形;As an example, the shape of the groove is designed as an inverted trapezoid;
作为一种举例说明,所述接触开关还可以采用位置开关或位置传感器中的一种或者组合模式;As an example, the contact switch can also adopt one or a combined mode of a position switch or a position sensor;
步骤二、驱动装置控制锁紧装置锁死;Step 2, the driving device controls the locking device to lock;
平台控制电路发出开关信号,电机得电旋转,驱动传动轴和齿轮转动,带动齿条左右运动,通过板簧的弹力,使U形卡槽将无人机着陆撬锁死在凹槽内,同时充电电极插入无人机着陆撬上的受电电极内,所述电极在弹簧提供的弹力下保持与受电电极紧密有效接触;The platform control circuit sends out a switch signal, the motor is energized to rotate, drives the transmission shaft and gear to rotate, drives the rack to move left and right, and through the elastic force of the leaf spring, the U-shaped card slot locks the UAV into the groove for landing, and at the same time The charging electrode is inserted into the receiving electrode on the landing skid of the drone, and the electrode is kept in close and effective contact with the receiving electrode under the elastic force provided by the spring;
步骤三、无人机充电;Step 3, UAV charging;
无人机被锁死后,第二接触开关发出准备就绪的信号,控制电机停止旋转,此时接通充电控制电路,为所述电极加电,开始为无人机电池充电;After the UAV is locked, the second contact switch sends a ready signal to control the motor to stop rotating. At this time, the charging control circuit is connected to power up the electrodes to start charging the UAV battery;
步骤四、无人机解锁飞离;Step 4, the drone unlocks and flies away;
当所述充电控制电路检测到无人机受电电池的电压达到额定值后,发出指令,自动切断充电电源,电极断电,然后驱动电机反向旋转,带动齿条左右移动,使U形卡槽缩回,同时充电电极随同U形卡槽同步缩回,对无人机的着陆撬实施解锁动作,无人机可随时重新起飞,完成后续的航程任务。When the charging control circuit detects that the voltage of the receiving battery of the drone reaches the rated value, an instruction is issued to automatically cut off the charging power supply, the electrodes are powered off, and then the motor is driven to rotate in reverse, driving the rack to move left and right, so that the U-shaped card The slot is retracted, and the charging electrode is retracted synchronously with the U-shaped card slot to unlock the landing skid of the drone. The drone can take off again at any time to complete subsequent voyage tasks.
本发明完全防雨防水,必要时可在雨天进行正常充电工作;可以安装在任何高度和地方,不需要人工进行干预;抗风性能良好,因为有锁死机构,只要无人机能够正常降落即可,不用考虑无人机被风吹动移走的问题;可以和国家电网、光伏发电站联合一起使用,组成集发电、充电一体的集成体系;技术成熟、安全可靠、定位简单、成本低廉;标准构型设计,重量较轻、加工装配方便,适合于大批量生产;The invention is completely rainproof and waterproof, and can carry out normal charging work in rainy days if necessary; it can be installed at any height and place without manual intervention; the wind resistance performance is good, because there is a locking mechanism, as long as the drone can land normally Yes, there is no need to consider the problem of the UAV being moved by the wind; it can be used together with the State Grid and photovoltaic power stations to form an integrated system integrating power generation and charging; the technology is mature, safe and reliable, simple in positioning, and low in cost; Standard configuration design, light weight, convenient processing and assembly, suitable for mass production;
以上公开的仅为本申请的一个具体实施例,但本申请并非局限于此,任何本领域的技术人员能思之的变化,都应落在本申请的保护范围内。What is disclosed above is only a specific embodiment of the present application, but the present application is not limited thereto, and any changes conceivable by those skilled in the art shall fall within the protection scope of the present application.
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| CN117576598A (en) * | 2024-01-19 | 2024-02-20 | 中国民用航空飞行学院 | A UAV line inspection system based on cloud database |
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