WO2023155086A1 - 一种用于气象观测的激光雷达 - Google Patents

一种用于气象观测的激光雷达 Download PDF

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Publication number
WO2023155086A1
WO2023155086A1 PCT/CN2022/076570 CN2022076570W WO2023155086A1 WO 2023155086 A1 WO2023155086 A1 WO 2023155086A1 CN 2022076570 W CN2022076570 W CN 2022076570W WO 2023155086 A1 WO2023155086 A1 WO 2023155086A1
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WO
WIPO (PCT)
Prior art keywords
fixedly installed
sleeve
plate
rod
meteorological observation
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Application number
PCT/CN2022/076570
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English (en)
French (fr)
Inventor
蒋媛
卢超
魏瑞
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陕西理工大学
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Application filed by 陕西理工大学 filed Critical 陕西理工大学
Priority to PCT/CN2022/076570 priority Critical patent/WO2023155086A1/zh
Priority to US18/149,120 priority patent/US11762098B2/en
Publication of WO2023155086A1 publication Critical patent/WO2023155086A1/zh

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Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S17/00—Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/88—Lidar systems specially adapted for specific applications
    • G01S17/95—Lidar systems specially adapted for specific applications for meteorological use
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/481—Constructional features, e.g. arrangements of optical elements
    • G01S7/4811—Constructional features, e.g. arrangements of optical elements common to transmitter and receiver
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48—Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/481—Constructional features, e.g. arrangements of optical elements
    • G01S7/4811—Constructional features, e.g. arrangements of optical elements common to transmitter and receiver
    • G01S7/4813—Housing arrangements
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01W—METEOROLOGY
    • G01W1/00—Meteorology
    • G01W1/02—Instruments for indicating weather conditions by measuring two or more variables, e.g. humidity, pressure, temperature, cloud cover or wind speed
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
    • Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
    • Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation

Definitions

  • the invention relates to the technical field of meteorology, and more specifically, the invention relates to a laser radar for meteorological observation.
  • the laser radar By emitting and receiving laser beams, the laser radar analyzes the return time of the laser beam after encountering the detection target, calculates the relative distance between the detection target and the location of the laser radar, and collects information such as three-dimensional coordinates and reflectivity of a large number of dense points on the surface of the detection target , reconstruct the 3D model of the detection target. .
  • the communication between the device on the radar rotor and other fixed devices mainly has the following channels:
  • slip rings to realize coaxial data transmission.
  • the stator of the slip ring is connected to the stator of the lidar, and the signal is transmitted to a rotating brush slip ring connector at the input end, and then the signal is output at the output end of the connector.
  • the rotor of the slip ring is connected to the rotor of the lidar; when rotating, the electrical signal is transmitted through the signal channel on the slip ring.
  • the main disadvantage of this method is that when the slip ring is used to realize coaxial data transmission, the slip ring inevitably has wear problems, is prone to friction and heat, and has a short service life.
  • the main disadvantage of this method is: when using electromagnetic induction coils to realize coaxial data transmission, the coils will generate electromagnetic radiation, which will affect other electromagnetically sensitive devices. Moreover, when multiple data lines are to be transmitted, it is necessary to consider the problem of electromagnetic shielding among the lines, which will make the signal transmission more complicated.
  • an embodiment of the present invention provides a laser radar for meteorological observation.
  • the air pressure at the bottom is increased to make it fall off, and the gap between the stable seat and the connecting sleeve is realized.
  • the disassembly of the connecting sleeve and the base is mainly to change the magnetic pole by switching the current direction of the external coil of the positioning electromagnet, resulting in the separation of the positioning electromagnet and the locking magnet, so that the base and the connecting sleeve are conveniently coordinated with the linkage assembly. The falling off, thereby facilitating the disassembly process of the whole device, to solve the problems raised in the above background technology.
  • a laser radar for meteorological observation including a base, the top of the base is fixedly installed with a stable seat, the top of the stable seat is installed with a connecting sleeve, the A shell is installed on the top of the connection sleeve, a power board is fixedly installed on the bottom surface of the inner cavity of the base, a snap-in slot plate is fixedly installed on the top of the power board, and a connection plug-in board is snap-fitted on the top of the snap-in slot board,
  • the outer fixing sleeve of the connection board is provided with a fixed sleeve, and the left and right sides of the fixed sleeve are fixed with horizontal plates, and the inside of the horizontal plate is respectively fixed with a locking magnet and a linkage assembly.
  • the top of the fixed sleeve plate is fixedly installed with a positioning electromagnet directly below the locking magnet, and the top of the positioning electromagnet is in contact with the bottom of the locking magnet.
  • the linkage assembly includes a bottom bar, and the top of the bottom bar.
  • the movable suit has a sleeve rod, the bottom of the inner cavity of the sleeve rod is fixedly installed with an inner rod, and the bottom of the inner rod is movable with the top of the bottom rod;
  • the top surface of the stable seat is provided with a bottom that is compatible with the connecting sleeve, the bottom of the connecting sleeve is fixedly sleeved, the edge is frictionally connected with the inner wall, and the top of the connecting board extends to the connecting
  • a bottom frame is fixedly installed inside the cover plate, and the top of the bottom frame extends to the inside of the outer casing, and a rotor radar is fixedly installed inside, and a horizontal plate is fixedly installed on the outside of the rotor radar, and a dust removal box is fixedly installed inside the horizontal plate
  • the inside of the bottom frame is fixedly installed with an inner frame
  • the inside of the inner frame is fixedly installed with a main shaft
  • the large input end of the main shaft is electrically connected with the output end of the connection board
  • the top of the main shaft is fixedly installed with
  • the auxiliary shaft, the top of the auxiliary shaft extends to the outside of the rotor radar and is fixedly installed with a signal receiving and processing terminal, the
  • the lidar includes a laser emitting component, the output end of the lidar is connected to an information processing component, the output end of the information processing component is connected to a scanning system, and the output end of the scanning system is electrically connected to a display component .
  • a balance spring is movably sleeved on the outside of the inner rod, and the upper and lower ends of the balance spring are fixedly connected to the top surface of the bottom rod and the bottom surface of the inner cavity of the sleeve rod respectively, and the bottom rod is composed of two It consists of two detachable rods snapped together.
  • the inside of the stability seat is provided with a connection with each other, and the front of the stability seat is provided with a pressure relief hole in communication with the connection.
  • the dust removal box includes a box body, openings are opened on the upper and lower sides of the box body, and a filter screen is fixedly installed on the inner wall of the opening.
  • the inner wall of the housing is provided with two negative pressure holes, and the two negative pressure holes are respectively located on the upper and lower sides of the horizontal plate.
  • the laser emitting component includes an excitation source, the output end of the excitation source is telecommunication connected with a laser, and the laser is electrically connected with a beam controller.
  • the information processing component includes an information receiver, and an output end of the information receiver is electrically connected to an information converter and a photoelectric converter.
  • the input end of the positioning electromagnet is in telecommunication connection with the output end of the power board, and the initial magnetic pole at the top of the positioning electromagnet is different from the magnetic pole at the bottom of the locking magnet.
  • the present invention can reduce the volume of the laser radar by setting the rotor radar to cooperate with the main shaft and the auxiliary shaft, improve the device integration of the laser radar, further save the space on the main shaft, and improve the space utilization rate;
  • the present invention increases the air pressure at the bottom by injecting gas into the inside, so that it falls off from it, and realizes the disassembly between the stable seat and the connecting cover plate;
  • the disassembly process of the connecting cover plate and the base is mainly by switching the external positioning electromagnet
  • the direction of the coil current changes its magnetic pole, resulting in the separation of the positioning electromagnet and the locking magnet, so as to cooperate with the linkage assembly to facilitate the detachment of the base and the connecting sleeve, thereby facilitating the disassembly and assembly process of the entire device;
  • the present invention introduces gas to the two negative pressure holes in turn, and the dust is driven into the interior of the dust removal box through the air flow, thereby realizing the dust removal process, wherein the negative pressure hole and the opening on the surface of the stable seat are in a sealed state during operation, thereby ensuring The inside of the housing is not affected by dust.
  • Figure 1 is a schematic diagram of the overall structure of the present invention.
  • FIG. 2 is a schematic diagram of the external structure of FIG. 1 of the present invention.
  • Fig. 3 is a schematic diagram of the structure at A in Fig. 1 of the present invention.
  • FIG. 4 is a schematic diagram of the structure at B in FIG. 1 of the present invention.
  • Fig. 5 is a structural schematic diagram of the linkage assembly of the present invention.
  • Fig. 6 is a schematic structural diagram of the dust removal box of the present invention.
  • Fig. 7 is a system block diagram of the present invention.
  • the reference signs are: 1, base; 101, power supply board; 102, snap-in slot plate; 103, connecting plug-in board; 104, fixed cover plate; 105, horizontal plate; 2, stable seat; 3, connecting cover plate; 4 , shell; 5, positioning electromagnet; 51, locking magnet; 6, linkage assembly; 61, bottom rod; 62, sleeve rod; 63, inner rod; 64, balance spring; 7, horizontal plate; 71, dust removal box ;711, box body; 712, opening; 713, filter screen; 8, main shaft; 81, auxiliary shaft; 9, signal receiving and processing end; 10, rotor radar; 11, inner frame; 12, bottom frame; 13, wireless receiving Coil; 14. Negative pressure hole; 15. Signal transmitting frame; 16. Signal receiving end.
  • a kind of lidar for meteorological observation as shown in accompanying drawing 1-7 comprises base 1, and the top of described base 1 is fixedly installed with stable base 2, and the top of described stable base 2 is equipped with connecting sleeve plate 3,
  • the top of the connecting cover plate 3 is equipped with a shell 4, the bottom surface of the inner cavity of the base 1 is fixedly installed with a power supply board 101, and the top of the power supply board 101 is fixedly installed with a clamping slot plate 102, and the clamping slot plate 102
  • the top of the connecting board 103 is clamped with a connecting board 103, and the outer fixed sleeve of the connecting board 103 is provided with a fixed sleeve plate 104, and the left and right sides of the fixed sleeve board 104 are fixedly equipped with a horizontal plate 105, and the horizontal plate 105
  • the locking magnet 51 and the linkage assembly 6 are respectively fixedly set inside, and the positioning electromagnet 5 located directly below the locking magnet 51 is fixedly installed on the top of the
  • the top surface of the stable seat 2 is provided with a 201 that is compatible with the bottom of the connection sleeve 3, and the bottom of the connection sleeve 3 is fixedly fitted with a 301, and the edge of the 301 is frictionally connected with the inner wall of the 201, and the connection
  • the top of the plugboard 103 extends to the inside of the connecting sleeve 3 and is fixedly installed with a bottom frame 12, and the top of the bottom frame 12 extends to the inside of the casing 4 and is fixedly installed with a rotor radar 10.
  • the air is introduced, and the dust is driven into the inside of the dust removal box 71 by the air flow, thereby realizing the dust removal process, wherein the negative pressure hole 14 and the opening on the surface of the stable seat 2 are in a sealed state during operation, thereby ensuring that the inside of the housing 4 is not affected by dust.
  • the outside of the rotor radar 10 is fixedly fitted with a horizontal plate 7, the inside of the horizontal plate 7 is fixedly equipped with a dust removal box 71, the inside of the bottom frame 12 is fixedly installed with an inner frame 11, and the inside of the inner frame 11 is fixed.
  • a main shaft 8 is installed, and the large input end of the main shaft 8 is electrically connected to the output end of the connecting plate 103.
  • the top of the main shaft 8 is fixedly installed with a sub-shaft 81, and the top of the sub-shaft 81 extends to the rotor radar 10.
  • the outer wall of the main shaft 8 is fixedly installed with a signal receiving and processing terminal 9, the outer wall of the main shaft 8 is fixedly installed with a wireless receiving coil 13 inside the rotor radar 10, and the front of the housing 4 is fixedly installed with a signal transmitting frame 15 and a signal receiving terminal 16 ;
  • the lidar includes a laser emitting component, the output end of the lidar is connected to an information processing component, the output end of the information processing component is connected to a scanning system, and the output end of the scanning system is electrically connected to a display component .
  • the specific implementation method is: by setting the rotor radar 10 to cooperate with the main shaft 8 and the auxiliary shaft 81, the volume of the laser radar can be reduced, the device integration of the laser radar can be improved, the space on the main shaft can be further saved, and the space utilization rate can be improved.
  • the outer movable sleeve of the inner rod 63 is equipped with a balance spring 64, and the upper and lower ends of the balance spring 64 are respectively fixedly connected to the top surface of the bottom rod 61 and the bottom surface of the inner cavity of the sleeve rod 62.
  • the bottom rod 61 is composed of two movable The dismounting rods are connected to each other.
  • the inside of the stable seat 2 is provided with a 202 communicating with the 201.
  • the front of the stable seat 2 is provided with a pressure relief hole connected with the 202.
  • the dust removal box 71 includes a box body 711 , the upper and lower sides of the box 711 are provided with openings 712, the inner wall of the opening 712 is fixedly equipped with a filter screen 713, the inner wall of the housing 4 is provided with two negative pressure holes 14, and the two negative pressure holes 14 are respectively located on the upper and lower sides of the horizontal plate 7.
  • the laser emitting component includes an excitation source, the output end of the excitation source is connected to a laser, and the laser is electrically connected to a beam controller.
  • the information processing component includes an information receiving device, the output end of the information receiver is electrically connected to an information converter and a photoelectric converter, the input end of the positioning electromagnet 5 is connected to the output end of the power supply board 101 by telecommunication, and the initial position on the top of the positioning electromagnet 5 The poles are different from the bottom poles of the locking magnet 51 .
  • the specific implementation method is: by injecting gas into 202, increasing the air pressure at the bottom of 301, so that 301 falls off from 201, realizing the disassembly between the stable seat 2 and the connection sleeve 3; about the disassembly of the connection sleeve 3 and the base 1
  • the process is mainly to change the magnetic pole by switching the current direction of the external coil of the positioning electromagnet 5, causing the positioning electromagnet 5 and the locking magnet 51 to separate, so as to cooperate with the linkage assembly 6 to facilitate the falling off of the base 1 and the connecting sleeve 3, thereby facilitating The disassembly process of the entire device.
  • the technical advantage of the present invention is that the overall structure is simple in arrangement, takes up little space, and is easy to disassemble as a whole. Therefore, the working principle of the present invention lies in the disassembly process at multiple places and the dust-proof control inside the casing 4;
  • the disassembly process of the stabilizer 2 and the connecting sleeve 3 it is mainly used to inject gas into the interior of 202 in advance to increase the air pressure at the bottom of 301, so that 301 falls off from 201, and the disassembly between the stabilizer 2 and the connecting sleeve 3 is realized ;
  • the magnetic pole is changed mainly by switching the current direction of the external coil of the positioning electromagnet 5, causing the positioning electromagnet 5 and the locking magnet 51 to separate, thereby facilitating the base with the linkage assembly 6 1 and the falling off of the connecting sleeve plate 3;
  • the gas is mainly introduced into the two negative pressure holes 14 in turns, and the dust is driven into the inside of the dust removal box 71 by the air flow, thereby realizing the dust removal process, wherein the negative pressure holes 14 and the opening on the surface of the stable seat 2 are in operation.
  • the process is in a sealed state.
  • connection should be understood in a broad sense, which can be mechanical connection Or electrical connection, it can also be the internal communication of two components, it can be directly connected, "up”, “down”, “left”, “right”, etc. are only used to indicate the relative positional relationship, when the absolute position of the object being described Change, the relative positional relationship may change;

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  • Physics & Mathematics (AREA)
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  • Radar, Positioning & Navigation (AREA)
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  • Environmental & Geological Engineering (AREA)
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Abstract

一种用于气象观测的激光雷达，包括底座（1），底座（1）的顶部固定安装有稳定座（2），稳定座（2）的顶部安装有连接套板（3），连接套板（3）顶部安装有外壳（4），底座（1）内腔的底面固定安装有电源板（101），电源板（101）的顶部固定安装有卡接槽板（102），卡接槽板（102）的顶部卡接有连接插板（103），连接插板（103）的外部固定套装有固定套板（104）。通过向内部注入气体，增加底部的气压，实现了稳定座（2）和连接套板（3）之间的拆卸；关于连接套板（3）和底座（1）的拆卸过程，主要是通过切换定位电磁铁（5）外部线圈电流方向改变其磁极，导致定位电磁铁（5）和锁紧磁铁（51）分离，从而配合连动组件（6）方便了底座（1）和连接套板（3）的脱落，从而方便了整个装置的拆装过程。

Description

一种用于气象观测的激光雷达 技术领域
本发明涉及气象技术领域，更具体地说，本发明涉及一种用于气象观测的激光雷达。
 背景技术
激光雷达通过发射和接收激光光束，分析激光光束遇到探测目标后的折返时间，计算出探测目标与激光雷达所在地的相对距离，并收集探测目标表面大量密集的点的三维坐标、反射率等信息，复建出探测目标的三维模型。。
在同轴转动条件下，雷达转子上的器件和其他固定器件之间的通信主要有以下途径：
1.利用滑环来实现同轴数据传输。如，机械旋转激光雷达中，滑环的定子连接着激光雷达的定子，在输入端把信号传到一个转动的电刷滑环连接器，然后再把信号在连接器输出端输出。滑环的转子连接着激光雷达的转子；在转动时，电信号通过滑环上的信号通道传递。该方式的主要不足在于：利用滑环来实现同轴数据传输时，滑环不可避免存在磨损问题，容易摩擦发热，使用寿命短。
2.利用电磁感应线圈来实现同轴数据传输，该方式的主要不足在于：利用电磁感应线圈来实现同轴数据传输时，线圈产生电磁辐射，对于电磁敏感的其他器件会有影响。而且，若要实现多条数据线路传输时，需要考虑各线路间的电磁屏蔽问题，这将会导致信号传输较为复杂。
 技术解决方案
为了克服现有技术的上述缺陷，本发明的实施例提供一种用于气象观测的激光雷达，通过向内部注入气体，增加底部的气压，使得从中脱落，实现了稳定座和连接套板之间的拆卸；关于连接套板和底座的拆卸过程，主要是通过切换定位电磁铁外部线圈电流方向改变其磁极，导致定位电磁铁和锁紧磁铁分离，从而配合连动组件方便了底座和连接套板的脱落，从而方便了整个装置的拆装过程，以解决上述背景技术中提出的问题。
为实现上述目的，本发明提供如下技术方案：一种用于气象观测的激光雷达，包括底座，所述底座的顶部固定安装有稳定座，所述稳定座的顶部安装有连接套板，所述连接套板顶部安装有外壳，所述底座内腔的底面固定安装有电源板，所述电源板的顶部固定安装有卡接槽板，所述卡接槽板的顶部卡接有连接插板，所述连接插板的外部固定套装有固定套板，所述固定套板的左右两侧均固定安装有横板，所述横板的内部分别固定套装有锁紧磁铁和连动组件，所述固定套板的顶部固定安装有位于锁紧磁铁正下方的定位电磁铁，所述定位电磁铁的顶部与锁紧磁铁的底部相互接触，所述连动组件包括底杆，所述底杆的顶部活动套装有套杆，所述套杆内腔的底部固定安装有内杆，所述内杆的底部与底杆的顶部活动套装；
所述稳定座的顶面开设有与连接套板底部相适配的，所述连接套板的底部固定套装有，所述的边缘与的内壁摩擦连接，所述连接插板的顶部延伸至连接套板的内部固定安装有底框，所述底框的顶部延伸至外壳的内部固定安装有转子雷达，所述转子雷达的外部固定套装有横板，所述横板的内部固定安装有除尘箱，所述底框的内部固定安装有内框，所述内框的内部固定安装有主轴，所述主轴的大输入端与连接插板的输出端电性连接，所述主轴的顶部固定安装有副轴，所述副轴的顶部延伸至转子雷达的外部并固定安装有信号接收处理端，所述主轴的外壁固定安装有位于转子雷达内部的无线接收线圈，所述外壳的正面固定安装有信号发射框和信号接收端；
所述激光雷达包括激光发射组件，所述激光雷达的输出端电信连接有信息处理组件，所述信息处理组件的输出端电信连接有扫描***，所述扫描***的输出端电性连接有显示组件。
在一个优选地实施方式中，所述内杆外部活动套装有平衡弹簧，所述平衡弹簧的上下两端分别于底杆的顶面和套杆内腔的底面固定连接，所述底杆由两个可拆卸杆相互卡接组成。
在一个优选地实施方式中，所述稳定座的内部开设有与相互连通的，所述稳定座的正面开设有与相连通的泄压孔。
在一个优选地实施方式中，所述除尘箱包括箱体，所述箱体的上下两面均开设有开口，所述开口的内壁固定安装有滤网。
在一个优选地实施方式中，所述外壳的内壁开设有两个负压孔，两个所述负压孔分别位于横板的上下两侧。
在一个优选地实施方式中，是激光发射组件包括激励源，所述激励源的输出端电信连接有激光器，所述激光器电性连接有光束控制器。
在一个优选地实施方式中，所述信息处理组件包括信息接收器，所述信息接收器的输出端电性连接有信息转换器和光电转换器。
在一个优选地实施方式中，所述定位电磁铁的输入端与电源板的输出端电信连接，所述定位电磁铁顶部的初始磁极与锁紧磁铁的底部磁极相异。
 有益效果
本发明的技术效果和优点：
1、本发明通过设置转子雷达配合主轴和副轴，能够减小激光雷达的体积，提高激光雷达的器件集成度，能进一步节省主轴上的空间，提高空间利用率；
2、本发明通过向内部注入气体，增加底部的气压，使得从中脱落，实现了稳定座和连接套板之间的拆卸；关于连接套板和底座的拆卸过程，主要是通过切换定位电磁铁外部线圈电流方向改变其磁极，导致定位电磁铁和锁紧磁铁分离，从而配合连动组件方便了底座和连接套板的脱落，从而方便了整个装置的拆装过程；
本发明通过向两个负压孔轮次导入气体，通过气流带动灰尘进入除尘箱的内部，从而实现除尘过程，其中负压孔和稳定座表面的开口在运行过程中处于密封状态，从而保证了外壳内部不受灰尘影响。
 附图说明
图1为本发明的整体结构示意图。
图2为本发明的图1的外部结构示意图。
图3为本发明的图1的A处结构示意图。
图4为本发明的图1的B处结构示意图。
图5为本发明的连动组件结构示意图。
图6为本发明的除尘箱结构示意图。
图7为本发明的***框图。
附图标记为：1、底座；101、电源板；102、卡接槽板；103、连接插板；104、固定套板；105、横板；2、稳定座；3、连接套板；4、外壳；5、定位电磁铁；51、锁紧磁铁；6、连动组件；61、底杆；62、套杆；63、内杆；64、平衡弹簧；7、横板；71、除尘箱；711、箱体；712、开口；713、滤网；8、主轴；81、副轴；9、信号接收处理端；10、转子雷达；11、内框；12、底框；13、无线接收线圈；14、负压孔；15、信号发射框；16、信号接收端。
 本发明的实施方式
下面将结合本发明实施例中的附图，对本发明实施例中的技术方案进行清楚、完整地描述，显然，所描述的实施例仅仅是本发明一部分实施例，而不是全部的实施例。基于本发明中的实施例，本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例，都属于本发明保护的范围。
如附图1-7所示的一种用于气象观测的激光雷达，包括底座1，所述底座1的顶部固定安装有稳定座2，所述稳定座2的顶部安装有连接套板3，所述连接套板3顶部安装有外壳4，所述底座1内腔的底面固定安装有电源板101，所述电源板101的顶部固定安装有卡接槽板102，所述卡接槽板102的顶部卡接有连接插板103，所述连接插板103的外部固定套装有固定套板104，所述固定套板104的左右两侧均固定安装有横板105，所述横板105的内部分别固定套装有锁紧磁铁51和连动组件6，所述固定套板104的顶部固定安装有位于锁紧磁铁51正下方的定位电磁铁5，所述定位电磁铁5的顶部与锁紧磁铁51的底部相互接触，所述连动组件6包括底杆61，所述底杆61的顶部活动套装有套杆62，所述套杆62内腔的底部固定安装有内杆63，所述内杆63的底部与底杆61的顶部活动套装；
所述稳定座2的顶面开设有与连接套板3底部相适配的201，所述连接套板3的底部固定套装有301，所述301的边缘与201的内壁摩擦连接，所述连接插板103的顶部延伸至连接套板3的内部固定安装有底框12，所述底框12的顶部延伸至外壳4的内部固定安装有转子雷达10，通过向两个负压孔14轮次导入气体，通过气流带动灰尘进入除尘箱71的内部，从而实现除尘过程，其中负压孔14和稳定座2表面的开口在运行过程中处于密封状态，从而保证了外壳4内部不受灰尘影响，所述转子雷达10的外部固定套装有横板7，所述横板7的内部固定安装有除尘箱71，所述底框12的内部固定安装有内框11，所述内框11的内部固定安装有主轴8，所述主轴8的大输入端与连接插板103的输出端电性连接，所述主轴8的顶部固定安装有副轴81，所述副轴81的顶部延伸至转子雷达10的外部并固定安装有信号接收处理端9，所述主轴8的外壁固定安装有位于转子雷达10内部的无线接收线圈13，所述外壳4的正面固定安装有信号发射框15和信号接收端16；
所述激光雷达包括激光发射组件，所述激光雷达的输出端电信连接有信息处理组件，所述信息处理组件的输出端电信连接有扫描***，所述扫描***的输出端电性连接有显示组件。
具体实施方式为：通过设置转子雷达10配合主轴8和副轴81，能够减小激光雷达的体积，提高激光雷达的器件集成度，能进一步节省主轴上的空间，提高空间利用率。
所述内杆63外部活动套装有平衡弹簧64，所述平衡弹簧64的上下两端分别于底杆61的顶面和套杆62内腔的底面固定连接，所述底杆61由两个可拆卸杆相互卡接组成，所述稳定座2的内部开设有与201相互连通的202，所述稳定座2的正面开设有与202相连通的泄压孔，所述除尘箱71包括箱体711，所述箱体711的上下两面均开设有开口712，所述开口712的内壁固定安装有滤网713，所述外壳4的内壁开设有两个负压孔14，两个所述负压孔14分别位于横板7的上下两侧，是激光发射组件包括激励源，所述激励源的输出端电信连接有激光器，所述激光器电性连接有光束控制器，所述信息处理组件包括信息接收器，所述信息接收器的输出端电性连接有信息转换器和光电转换器，所述定位电磁铁5的输入端与电源板101的输出端电信连接，所述定位电磁铁5顶部的初始磁极与锁紧磁铁51的底部磁极相异。
具体实施方式为：通过向202内部注入气体，增加301底部的气压，使得301从201中脱落，实现了稳定座2和连接套板3之间的拆卸；关于连接套板3和底座1的拆卸过程，主要是通过切换定位电磁铁5外部线圈电流方向改变其磁极，导致定位电磁铁5和锁紧磁铁51分离，从而配合连动组件6方便了底座1和连接套板3的脱落，从而方便了整个装置的拆装过程。
本发明工作原理：
本发明的技术优势在于整体结构排列简单，占用空间小，且整体方便拆卸，因此本发明的工作原理在于多处的拆卸过程和外壳4内部的防尘操控；
关于稳定座2和连接套板3的拆卸过程，主要利用的事先向202内部注入气体，增加301底部的气压，使得301从201中脱落，实现了稳定座2和连接套板3之间的拆卸；关于连接套板3和底座1的拆卸过程，主要是通过切换定位电磁铁5外部线圈电流方向改变其磁极，导致定位电磁铁5和锁紧磁铁51分离，从而配合连动组件6方便了底座1和连接套板3的脱落；
关于外壳4内部除尘，主要是向两个负压孔14轮次导入气体，通过气流带动灰尘进入除尘箱71的内部，从而实现除尘过程，其中负压孔14和稳定座2表面的开口在运行过程中处于密封状态。
最后应说明的几点是：首先，在本申请的描述中，需要说明的是，除非另有规定和限定，术语“安装”、“相连”、“连接”应做广义理解，可以是机械连接或电连接，也可以是两个元件内部的连通，可以是直接相连，“上”、“下”、“左”、“右”等仅用于表示相对位置关系，当被描述对象的绝对位置改变，则相对位置关系可能发生改变；
其次：本发明公开实施例附图中，只涉及到与本公开实施例涉及到的结构，其他结构可参考通常设计，在不冲突情况下，本发明同一实施例及不同实施例可以相互组合；
最后：以上所述仅为本发明的优选实施例而已，并不用于限制本发明，凡在本发明的精神和原则之内，所作的任何修改、等同替换、改进等，均应包含在本发明的保护范围之内。

Claims (8)

  1. 一种用于气象观测的激光雷达，包括底座（1），其特征在于：所述底座（1）的顶部固定安装有稳定座（2），所述稳定座（2）的顶部安装有连接套板（3），所述连接套板（3）顶部安装有外壳（4），所述底座（1）内腔的底面固定安装有电源板（101），所述电源板（101）的顶部固定安装有卡接槽板（102），所述卡接槽板（102）的顶部卡接有连接插板（103），所述连接插板（103）的外部固定套装有固定套板（104），所述固定套板（104）的左右两侧均固定安装有横板（105），所述横板（105）的内部分别固定套装有锁紧磁铁（51）和连动组件（6），所述固定套板（104）的顶部固定安装有位于锁紧磁铁（51）正下方的定位电磁铁（5），所述定位电磁铁（5）的顶部与锁紧磁铁（51）的底部相互接触，所述连动组件（6）包括底杆（61），所述底杆（61）的顶部活动套装有套杆（62），所述套杆（62）内腔的底部固定安装有内杆（63），所述内杆（63）的底部与底杆（61）的顶部活动套装；
    所述稳定座（2）的顶面开设有与连接套板（3）底部相适配的（201），所述连接套板（3）的底部固定套装有（301），所述（301）的边缘与（201）的内壁摩擦连接，所述连接插板（103）的顶部延伸至连接套板（3）的内部固定安装有底框（12），所述底框（12）的顶部延伸至外壳（4）的内部固定安装有转子雷达（10），所述转子雷达（10）的外部固定套装有横板（7），所述横板（7）的内部固定安装有除尘箱（71），所述底框（12）的内部固定安装有内框（11），所述内框（11）的内部固定安装有主轴（8），所述主轴（8）的大输入端与连接插板（103）的输出端电性连接，所述主轴（8）的顶部固定安装有副轴（81），所述副轴（81）的顶部延伸至转子雷达（10）的外部并固定安装有信号接收处理端（9），所述主轴（8）的外壁固定安装有位于转子雷达（10）内部的无线接收线圈（13），所述外壳（4）的正面固定安装有信号发射框（15）和信号接收端（16）；
    所述激光雷达包括激光发射组件，所述激光雷达的输出端电信连接有信息处理组件，所述信息处理组件的输出端电信连接有扫描***，所述扫描***的输出端电性连接有显示组件。
  2. 根据权利要求1所述的一种用于气象观测的激光雷达，其特征在于：所述内杆（63）外部活动套装有平衡弹簧（64），所述平衡弹簧（64）的上下两端分别于底杆（61）的顶面和套杆（62）内腔的底面固定连接，所述底杆（61）由两个可拆卸杆相互卡接组成。
  3. 根据权利要求1所述的一种用于气象观测的激光雷达，其特征在于：所述稳定座（2）的内部开设有与（201）相互连通的（202），所述稳定座（2）的正面开设有与（202）相连通的泄压孔。
  4. 根据权利要求1所述的一种用于气象观测的激光雷达，其特征在于：所述除尘箱（71）包括箱体（711），所述箱体（711）的上下两面均开设有开口（712），所述开口（712）的内壁固定安装有滤网（713）。
  5. 根据权利要求1所述的一种用于气象观测的激光雷达，其特征在于：所述外壳（4）的内壁开设有两个负压孔（14），两个所述负压孔（14）分别位于横板（7）的上下两侧。
  6. 根据权利要求1所述的一种用于气象观测的激光雷达，其特征在于：是激光发射组件包括激励源，所述激励源的输出端电信连接有激光器，所述激光器电性连接有光束控制器。
  7. 根据权利要求1所述的一种用于气象观测的激光雷达，其特征在于：所述信息处理组件包括信息接收器，所述信息接收器的输出端电性连接有信息转换器和光电转换器。
  8. 根据权利要求1所述的一种用于气象观测的激光雷达，其特征在于：所述定位电磁铁（5）的输入端与电源板（101）的输出端电信连接，所述定位电磁铁（5）顶部的初始磁极与锁紧磁铁（51）的底部磁极相异。
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