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CN118169641A - Development test platform for in-hole omnibearing scanning radar antenna acquisition and control system - Google Patents

Development test platform for in-hole omnibearing scanning radar antenna acquisition and control system Download PDF

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Publication number
CN118169641A
CN118169641A CN202410337597.2A CN202410337597A CN118169641A CN 118169641 A CN118169641 A CN 118169641A CN 202410337597 A CN202410337597 A CN 202410337597A CN 118169641 A CN118169641 A CN 118169641A
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motor
slip ring
fixed
hole
connecting flange
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Inventor
李涛涛
曾鹏
何宇
王鹏杰
冯塬塬
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Pingxiang University
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Pingxiang University
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO 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
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/02Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S13/00
    • G01S7/40Means for monitoring or calibrating
    • G01S7/4004Means for monitoring or calibrating of parts of a radar system

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Radar Systems Or Details Thereof (AREA)

Abstract

The invention relates to the technical field of radar in holes, in particular to a development and test platform of an omnidirectional scanning radar antenna acquisition and control system in holes. The development test platform consists of a base part, a first supporting part, a second supporting part, a power part and a rotary scanning part. The base portion serves as a platform base for securing the first support portion and the second support portion. The first supporting part and the second supporting part are symmetrically distributed on two sides of the base part and are used for supporting the rotary scanning part. The power section provides power for the rotational movement of the rotating scan section. The base part, the first supporting part and the second supporting part are relatively fixed, and the rotary scanning part rotates relative to the base part under the action of the power part. The development test platform completely corresponds to the working state of continuous rotation scanning of the radar core component relative to the antenna sleeve in actual engineering, is convenient to assemble and disassemble in the development test process, can avoid winding of wires, and completely meets the requirement of rotation scanning test.

Description

一种孔中全方位扫描雷达天线采控系统开发测试平台A development and testing platform for the acquisition and control system of an all-round scanning radar antenna in a hole

技术领域Technical Field

本发明涉及孔中雷达技术领域,尤其是涉及一种孔中全方位扫描雷达天线采控系统开发测试平台。The invention relates to the technical field of borehole radar, and in particular to a development and testing platform for an in-hole omnidirectional scanning radar antenna acquisition and control system.

背景技术Background technique

孔中雷达技术在探测深度和精度上均有上佳表现,因而被广泛应用于地下油气资源勘探以及煤矿开采超前探测等领域。Borehole radar technology has excellent performance in detection depth and accuracy, and is therefore widely used in fields such as underground oil and gas resource exploration and advanced detection of coal mining.

采控系统是孔中雷达技术的核心,用于实现孔中雷达定向探测时的方向精准可控,扫描探测时的方向精细可循。在孔中全方位扫描雷达天线采控系统开发过程中,旋转扫描功能测试通常采用两种方式。一种是将雷达核心部件如控制单元、位姿监测单元、雷达辐射面等直接置于台面进行测试,这种方式简单快捷,但由于雷达核心部件在实际工作时处于不断旋转扫描的状态,这种方式往往会出现导线缠绕的情况,进而影响测试效果。另一种方式是将雷达的核心部件装入天线套管内进行测试,这种测试方式虽然避免了导线缠绕,但拆装过程繁琐,难以满足开发过程中反复测试的需求。The acquisition and control system is the core of borehole radar technology. It is used to achieve precise control of the direction of borehole radar directional detection and precise tracking of the direction during scanning detection. In the development process of the borehole all-round scanning radar antenna acquisition and control system, there are usually two ways to test the rotation scanning function. One is to place the core components of the radar such as the control unit, posture monitoring unit, radar radiation surface, etc. directly on the table for testing. This method is simple and fast, but because the core components of the radar are in a state of continuous rotation and scanning during actual work, this method often causes wire entanglement, which affects the test effect. Another way is to install the core components of the radar into the antenna casing for testing. Although this test method avoids wire entanglement, the disassembly and assembly process is cumbersome and it is difficult to meet the needs of repeated testing during the development process.

因此,有必要设计一种开发测试平台,使孔中全方位扫描雷达天线采控系统的开发测试过程更加简单高效。Therefore, it is necessary to design a development and testing platform to make the development and testing process of the borehole omnidirectional scanning radar antenna acquisition and control system simpler and more efficient.

发明内容Summary of the invention

基于上述背景,本发明提供了一种孔中全方位扫描雷达天线采控系统开发测试平台,所述开发测试平台由底座部分、第一支承部分、第二支承部分、动力部分和旋转扫描部分组成;所述底座部分作为所述开发测试平台的基座,用于固定所述第一支承部分和第二支承部分;所述第一支承部分和第二支承部分对称分布在底座部分两侧,用于支撑所述旋转扫描部分;所述动力部分为旋转扫描部分的旋转运动提供动力;所述底座部分、第一支承部分和第二支承部分相对固定,所述旋转扫描部分可在动力部分作用下相对底座部分旋转,这完全对应了实际工程中雷达核心部件相对天线套管不断旋转扫描的工作状态。Based on the above background, the present invention provides a development and testing platform for an in-hole omnidirectional scanning radar antenna acquisition and control system, wherein the development and testing platform consists of a base part, a first supporting part, a second supporting part, a power part and a rotating scanning part; the base part serves as a base of the development and testing platform, and is used to fix the first supporting part and the second supporting part; the first supporting part and the second supporting part are symmetrically distributed on both sides of the base part, and are used to support the rotating scanning part; the power part provides power for the rotational movement of the rotating scanning part; the base part, the first supporting part and the second supporting part are relatively fixed, and the rotating scanning part can rotate relative to the base part under the action of the power part, which completely corresponds to the working state of the radar core component continuously rotating and scanning relative to the antenna sleeve in actual engineering.

进一步地,所述底座部分由脚垫、底板、间隔柱和搭载板组成;所述底板为矩形板材,边缘设有若干通孔以安装脚垫和间隔柱;所述脚垫通过螺纹连接固定在底板的一面;所述间隔柱一端通过螺纹连接固定在底板的另一面;所述搭载板通过螺纹连接固定在间隔柱另一端,用于搭载数据线接口、电线连接器、平台开关和控制电路板;Furthermore, the base part is composed of a foot pad, a bottom plate, a spacer column and a mounting plate; the bottom plate is a rectangular plate with a plurality of through holes on the edge for mounting the foot pad and the spacer column; the foot pad is fixed to one side of the bottom plate by a threaded connection; one end of the spacer column is fixed to the other side of the bottom plate by a threaded connection; the mounting plate is fixed to the other end of the spacer column by a threaded connection, and is used to carry a data line interface, a wire connector, a platform switch and a control circuit board;

所述第一支承部分垂直固定在所述底座部分的一侧,由第一支撑板、直角角码、连接法兰和联轴器组成;所述第一支撑板通过直角角码垂直固定在底板上;所述连接法兰为盘形,其中部设置有圆柱凸起结构;所述连接法兰的盘形端面通过螺钉与第一支撑板侧面固连;所述连接法兰的圆柱凸起结构与联轴器的一端固连;The first supporting part is vertically fixed to one side of the base part, and is composed of a first supporting plate, a right-angle bracket, a connecting flange and a coupling; the first supporting plate is vertically fixed to the bottom plate by the right-angle bracket; the connecting flange is disc-shaped, and a cylindrical protrusion structure is arranged in the middle; the disc-shaped end surface of the connecting flange is fixedly connected to the side surface of the first supporting plate by screws; the cylindrical protrusion structure of the connecting flange is fixedly connected to one end of the coupling;

所述第二支承部分垂直固定在所述底座部分的另一侧,由第二支撑板、直角角码、滑环连接法兰和导电滑环组成;所述第二支撑板通过直角角码垂直固定在底板上;所述滑环连接法兰为回转体零件,整体呈放倒的“T”字形,其一端为细长轴,另一端为扁平的盘形结构;所述导电滑环包含滑环外圈和滑环内圈,所述滑环外圈可绕所述滑环内圈旋转;所述滑环连接法兰的细长轴端通过紧定螺钉与所述滑环内圈固连;所述滑环外圈端面通过螺钉与第二支撑板侧面固连;The second supporting part is vertically fixed to the other side of the base part, and is composed of a second supporting plate, a right-angle bracket, a slip ring connecting flange and a conductive slip ring; the second supporting plate is vertically fixed to the bottom plate by the right-angle bracket; the slip ring connecting flange is a rotating body part, and is in an inverted "T" shape as a whole, one end of which is a slender shaft and the other end is a flat disc structure; the conductive slip ring comprises a slip ring outer ring and a slip ring inner ring, and the slip ring outer ring can rotate around the slip ring inner ring; the slender shaft end of the slip ring connecting flange is fixedly connected to the slip ring inner ring by a set screw; the end face of the slip ring outer ring is fixedly connected to the side of the second supporting plate by a screw;

所述动力部分由电机、电机安装端盖和电机安装套组成;所述电机为圆柱形,电机输出轴在其一侧伸出,所述电机靠近电机输出轴的端面上设置有安装螺孔;所述电机安装端盖设置有与所述安装螺孔相配合的通孔;所述电机通过螺钉与所述电机安装端盖固连;所述电机安装套为圆柱形,其内部设置有可容纳所述电机的圆孔;电机安装套一端通过螺钉与所述电机安装端盖固连;所述电机输出轴容纳至所述联轴器的另一端,并通过紧定螺钉固定;The power part is composed of a motor, a motor mounting end cover and a motor mounting sleeve; the motor is cylindrical, the motor output shaft extends out from one side of the motor, and a mounting screw hole is provided on the end face of the motor close to the motor output shaft; the motor mounting end cover is provided with a through hole matching the mounting screw hole; the motor is fixedly connected to the motor mounting end cover by screws; the motor mounting sleeve is cylindrical, and a round hole for accommodating the motor is provided inside the sleeve; one end of the motor mounting sleeve is fixedly connected to the motor mounting end cover by screws; the motor output shaft is accommodated in the other end of the coupling and fixed by a set screw;

所述旋转扫描部分包括旋转骨架、电源模块、控制单元、位姿监测单元和雷达辐射面;所述旋转骨架为长条状结构,其一端通过螺钉与所述滑环连接法兰固定,另一端通过螺钉与所述电机安装套固定;所述电源模块、控制单元、位姿监测单元和雷达辐射面均固定在所述旋转骨架上。The rotating scanning part includes a rotating skeleton, a power module, a control unit, a posture monitoring unit and a radar radiation surface; the rotating skeleton is a long strip structure, one end of which is fixed to the slip ring connecting flange by screws, and the other end is fixed to the motor mounting sleeve by screws; the power module, the control unit, the posture monitoring unit and the radar radiation surface are all fixed on the rotating skeleton.

进一步地,所述直角角码与所述底板通过螺栓螺母固定,所述直角角码与所述第一支撑板通过螺栓螺母固定,所述直角角码与所述第二支撑板通过螺栓螺母固定。Furthermore, the right-angle bracket is fixed to the base plate by bolts and nuts, the right-angle bracket is fixed to the first support plate by bolts and nuts, and the right-angle bracket is fixed to the second support plate by bolts and nuts.

进一步地,所述滑环内圈与滑环连接法兰为同轴固定;所述滑环连接法兰与旋转骨架为同轴固定;所述旋转骨架与电机安装套为同轴固定;所述电机安装套与电机安装端盖为同轴固定;所述电机安装端盖与电机为同轴固定;所述电机输出轴与联轴器为同轴固定;所述联轴器与连接法兰的圆柱凸起结构为同轴固定。Furthermore, the slip ring inner ring and the slip ring connecting flange are coaxially fixed; the slip ring connecting flange and the rotating skeleton are coaxially fixed; the rotating skeleton and the motor mounting sleeve are coaxially fixed; the motor mounting sleeve and the motor mounting end cover are coaxially fixed; the motor mounting end cover and the motor are coaxially fixed; the motor output shaft and the coupling are coaxially fixed; the coupling and the cylindrical protrusion structure of the connecting flange are coaxially fixed.

进一步地,所述滑环连接法兰中部设有通孔结构,用于容纳内圈引出线;所述第二支撑板中部设有通孔,用于容纳外圈引出线;所述电机安装套和旋转骨架端部设有通孔,用于容纳电机导线。Furthermore, a through hole structure is provided in the middle of the slip ring connecting flange for accommodating the inner ring lead wire; a through hole is provided in the middle of the second support plate for accommodating the outer ring lead wire; and through holes are provided at the motor mounting sleeve and the end of the rotating skeleton for accommodating the motor wires.

本发明的有益效果主要在于:The beneficial effects of the present invention are mainly:

①所述开发测试平台完全对应实际工程中雷达核心部件相对天线套管不断旋转扫描的工作状态,测试过程可避免导线缠绕,完全满足孔中全方位扫描雷达天线采控系统开发过程中的旋转扫描测试需求;① The development and testing platform fully corresponds to the working state of the radar core components in the actual project, which is continuously rotating and scanning relative to the antenna sleeve. The test process can avoid the winding of wires and fully meet the rotation scanning test requirements in the development process of the full-range scanning radar antenna acquisition and control system in the hole;

②所述开发测试平台可避免反复将雷达核心部件装入天线套管内的繁琐操作,核心部件拆卸方便,可提高大大开发测试效率;② The development and testing platform can avoid the tedious operation of repeatedly installing the radar core components into the antenna casing, and the core components are easy to disassemble, which can greatly improve the development and testing efficiency;

③所述开发测试平台结构简单,加工方便,易于搭建。③The development and testing platform has a simple structure, is easy to process and build.

附图说明BRIEF DESCRIPTION OF THE DRAWINGS

下面结合附图和实施例对本发明进一步说明:The present invention is further described below in conjunction with the accompanying drawings and embodiments:

图1为本发明实施例中开发测试平台的整体结构示意图;FIG1 is a schematic diagram of the overall structure of a development and testing platform according to an embodiment of the present invention;

图2为本发明实施例中开发测试平台的爆炸视图;FIG2 is an exploded view of a development and testing platform according to an embodiment of the present invention;

图3为本发明实施例提供的底座部分的爆炸视图;FIG3 is an exploded view of a base portion provided by an embodiment of the present invention;

图4为本发明实施例提供的第一支承部分的爆炸视图;FIG4 is an exploded view of a first supporting portion provided by an embodiment of the present invention;

图5为本发明实施例提供的第二支承部分的爆炸视图;FIG5 is an exploded view of a second supporting portion provided by an embodiment of the present invention;

图6为本发明实施例提供的动力部分的爆炸视图;FIG6 is an exploded view of a power part provided by an embodiment of the present invention;

图7为本发明实施例提供的旋转扫描部分的示意图;FIG7 is a schematic diagram of a rotation scanning part provided by an embodiment of the present invention;

图8为本发明实施例中开发测试平台的整体剖切视图。FIG8 is an overall cross-sectional view of the development and testing platform in an embodiment of the present invention.

图中:In the figure:

1-底座部分;2-第一支承部分;3-第二支承部分;4-动力部分;5-旋转扫描部分;11-脚垫;12-底板;13-间隔柱;14-搭载板;141-数据线接口;142-电线连接器;143-平台开关;144-控制电路板;21-第一支撑板;22-直角角码;23-连接法兰;231-圆柱凸起结构;31-第二支撑板;32-滑环连接法兰;321-通孔结构;33-导电滑环;331-滑环外圈;3311-外圈引出线;332-滑环内圈;3321-内圈引出线;41-电机;411-电机输出轴;412-电机导线;42-电机安装端盖;43-电机安装套;51-旋转骨架;52-电源模块;53-控制单元;54-位姿监测单元;55-雷达辐射面。1-base part; 2-first supporting part; 3-second supporting part; 4-power part; 5-rotating scanning part; 11-foot pad; 12-bottom plate; 13-spacer column; 14-mounting board; 141-data line interface; 142-wire connector; 143-platform switch; 144-control circuit board; 21-first supporting plate; 22-right angle bracket; 23-connecting flange; 231-cylindrical protrusion structure; 31-second supporting plate; 32-slip ring connecting flange; 321-through hole structure; 33-conductive slip ring; 331-slip ring outer ring; 3311-outer ring lead wire; 332-slip ring inner ring; 3321-inner ring lead wire; 41-motor; 411-motor output shaft; 412-motor wire; 42-motor mounting end cover; 43-motor mounting sleeve; 51-rotating skeleton; 52-power module; 53-control unit; 54-posture monitoring unit; 55-radar radiation surface.

具体实施方式Detailed ways

下面将结合附图对本发明的技术方案进行清楚、完整地描述;需要说明的是,术语“中心”、“上”、“下”、“左”、“右”、“竖直”、“水平”、“内”、“外”等指示的方位或位置关系为基于附图所示的方位或位置关系,仅是为了便于描述本发明和简化描述,而不是指示或暗示所指的装置或元件必须具有特定的方位、以特定的方位构造和操作,因此不能理解为对本发明的限制;此外,术语“第一”、“第二”、“第三”仅用于描述目的,而不能理解为指示或暗示相对重要性。The technical solution of the present invention will be clearly and completely described below in conjunction with the accompanying drawings; it should be noted that the directions or positional relationships indicated by terms such as "center", "up", "down", "left", "right", "vertical", "horizontal", "inside" and "outside" are based on the directions or positional relationships shown in the accompanying 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 direction, be constructed and operate in a specific direction, and therefore cannot be understood as limiting the present invention; in addition, the terms "first", "second" and "third" are used for descriptive purposes only and cannot be understood as indicating or implying relative importance.

如图1至图8所示,本发明实施例提供了一种孔中全方位扫描雷达天线采控系统开发测试平台,该开发测试平台完全对应实际工程中雷达核心部件相对天线套管不断旋转扫描的工作状态,雷达核心部件拆装方便,且可避免旋转时导线缠绕,完全满足孔中全方位扫描雷达天线采控系统开发过程中的旋转测试需求。As shown in Figures 1 to 8, an embodiment of the present invention provides a development and testing platform for an in-hole omnidirectional scanning radar antenna acquisition and control system. The development and testing platform completely corresponds to the working state of the radar core components in actual engineering projects that continuously rotate and scan relative to the antenna casing. The radar core components are easy to disassemble and assemble, and the wires can be prevented from being entangled during rotation, which fully meets the rotation test requirements during the development of the in-hole omnidirectional scanning radar antenna acquisition and control system.

如图1和图2所示,本发明实施例提供的开发测试平台由底座部分1、第一支承部分2、第二支承部分3、动力部分4和旋转扫描部分5组成。其中,底座部分1是该平台的基座,用于固定第一支承部分2和第二支承部分3;第一支承部分2和第二支承部分3对称布置在底座部分1的两侧,用于支撑旋转扫描部分5;旋转扫描部分5用于搭载雷达核心部件如电源模块52、控制单元53、位姿监测单元54和雷达辐射面55等;动力部分4为旋转扫描部分5的旋转运动提供动力。As shown in Figures 1 and 2, the development and testing platform provided by the embodiment of the present invention is composed of a base part 1, a first support part 2, a second support part 3, a power part 4 and a rotating scanning part 5. Among them, the base part 1 is the base of the platform, which is used to fix the first support part 2 and the second support part 3; the first support part 2 and the second support part 3 are symmetrically arranged on both sides of the base part 1, and are used to support the rotating scanning part 5; the rotating scanning part 5 is used to carry radar core components such as a power module 52, a control unit 53, a posture monitoring unit 54 and a radar radiation surface 55; the power part 4 provides power for the rotating motion of the rotating scanning part 5.

在本发明实施例中,底座部分1、第一支承部分2、第二支承部分3相对固定,旋转扫描部分5可在动力部分4的带动下相对底座部分1不断旋转,完全对应了实际工程中雷达核心部件相对天线套管不断旋转扫描的工作状态。In the embodiment of the present invention, the base portion 1, the first supporting portion 2, and the second supporting portion 3 are relatively fixed, and the rotating scanning portion 5 can be continuously rotated relative to the base portion 1 driven by the power portion 4, which completely corresponds to the working state of the radar core component continuously rotating and scanning relative to the antenna sleeve in actual engineering.

如图3所示,底座部分由脚垫11、底板12、间隔柱13和搭载板14组成;本实施例中,所述底板12为矩形板材,其四周边缘对称设置了若干通孔用于安装脚垫11、间隔柱13、第一支承部分2以及第二支承部分3。为保证旋转测试的稳定性,平台重心不能过高,因此可采用激光切割钢板得到所述底板12。所述脚垫11用于防滑和提高平台放置稳定性,本实施例中,脚垫12为橡胶材质,呈圆台形,其中部设置内嵌有金属螺纹孔。所述间隔柱13一方面用于保持底板12与搭载板14的间距,另一方面将脚垫11固定至底板12。间隔柱13为阶梯轴状,其大直径一段为间隔段,内部设有螺纹孔,其小直径一段为螺纹段,该段透过底板12的通孔与脚垫11内部的螺纹孔形成螺纹连接,将脚垫11固定在底板12一面。所述搭载板14用于搭载数据线接口141、电线连接器142、平台开关143和控制电路板144等元件。搭载板14为非金属板材,外形与底板12基本一致,其两侧对称设置了内凹结构,用于容纳第一支撑部分2与第二支撑部分3。搭载板14边缘设置有若干通孔,螺钉可穿过该通孔旋入间隔柱13内部的螺纹孔,将搭载板14固定在间隔柱13的上端面。搭载板14在间隔柱13的作用下与底板12形成固定间隔,该间隔用于容纳导线。As shown in FIG3 , the base part is composed of a foot pad 11, a bottom plate 12, a spacer 13 and a mounting plate 14; in this embodiment, the bottom plate 12 is a rectangular plate, and a plurality of through holes are symmetrically arranged on the edges thereof for installing the foot pad 11, the spacer 13, the first supporting part 2 and the second supporting part 3. In order to ensure the stability of the rotation test, the center of gravity of the platform cannot be too high, so the bottom plate 12 can be obtained by laser cutting a steel plate. The foot pad 11 is used for anti-slip and improving the stability of the platform placement. In this embodiment, the foot pad 12 is made of rubber and is in a truncated cone shape, and a metal threaded hole is embedded in the middle. The spacer 13 is used to maintain the distance between the bottom plate 12 and the mounting plate 14 on the one hand, and to fix the foot pad 11 to the bottom plate 12 on the other hand. The spacer 13 is in the shape of a stepped shaft, and a large diameter section thereof is a spacer section, and a threaded hole is arranged inside, and a small diameter section thereof is a threaded section, which is threadedly connected with the threaded hole inside the foot pad 11 through the through hole of the bottom plate 12, so as to fix the foot pad 11 on one side of the bottom plate 12. The mounting plate 14 is used to carry components such as a data line interface 141, a wire connector 142, a platform switch 143, and a control circuit board 144. The mounting plate 14 is a non-metallic plate, and its appearance is basically the same as that of the bottom plate 12. The two sides of the mounting plate 14 are symmetrically provided with concave structures for accommodating the first support part 2 and the second support part 3. The edge of the mounting plate 14 is provided with a plurality of through holes, through which screws can be screwed into the threaded holes inside the spacer column 13 to fix the mounting plate 14 to the upper end surface of the spacer column 13. Under the action of the spacer column 13, the mounting plate 14 forms a fixed interval with the bottom plate 12, and the interval is used to accommodate the wires.

如图4所示,第一支承部分2由第一支撑板21、直角角码22、连接法兰23和联轴器24组成。所述第一支撑板21用于固定连接法兰23和联轴器24,为旋转扫描部分5的一端提供支撑。在本实施例中,第一支撑板21为金属板材,通过激光切割钢板得到。第一支撑板21底部设置有用于固定的通孔,中部设置有用于走线的通孔,上部设置有用于固定连接法兰23的通孔。所述直角角码22具有两个相互垂直的固定平面,平面内设有通孔。通过直角角码22的通孔、第一支撑板21的底部通孔和底板12的通孔形成的螺纹连接可将第一支撑板21垂直固定在底板12上。所述连接法兰23用于连接第一支撑板21和联轴器24。所述连接法兰23的主体为盘形结构,端面设置有与第一支撑板21上部通孔相对应的螺纹孔。连接法兰23中部设有圆柱凸起结构231,该结构的轴线与主体盘形结构的轴线共线。将螺钉穿过第一支撑板21上部通孔旋入连接法兰23端面螺纹孔可将连接法兰23固定在第一支撑板21侧面。所述联轴器24用于补偿由安装、制造产生的同轴度误差。联轴器24左右两端均设置有可容纳柱状轴的圆孔及螺钉紧固结构,在本实施例中,联轴器24右侧圆孔与连接法兰23的圆柱凸起结构231相配合,并通过螺钉紧固结构相互固定。As shown in FIG4 , the first supporting part 2 is composed of a first supporting plate 21, a right angle bracket 22, a connecting flange 23 and a coupling 24. The first supporting plate 21 is used to fix the connecting flange 23 and the coupling 24, and provide support for one end of the rotating scanning part 5. In this embodiment, the first supporting plate 21 is a metal plate obtained by laser cutting a steel plate. The first supporting plate 21 is provided with a through hole for fixing at the bottom, a through hole for wiring at the middle, and a through hole for fixing the connecting flange 23 at the top. The right angle bracket 22 has two mutually perpendicular fixing planes, and a through hole is provided in the plane. The first supporting plate 21 can be vertically fixed to the bottom plate 12 by a threaded connection formed by the through hole of the right angle bracket 22, the bottom through hole of the first supporting plate 21 and the through hole of the bottom plate 12. The connecting flange 23 is used to connect the first supporting plate 21 and the coupling 24. The main body of the connecting flange 23 is a disc-shaped structure, and the end face is provided with a threaded hole corresponding to the upper through hole of the first supporting plate 21. A cylindrical protrusion structure 231 is provided in the middle of the connecting flange 23, and the axis of the structure is colinear with the axis of the main disc-shaped structure. The connecting flange 23 can be fixed to the side of the first supporting plate 21 by passing a screw through the upper through hole of the first supporting plate 21 and screwing it into the threaded hole on the end face of the connecting flange 23. The coupling 24 is used to compensate for the coaxiality error caused by installation and manufacturing. The left and right ends of the coupling 24 are provided with a circular hole and a screw fastening structure that can accommodate a cylindrical shaft. In this embodiment, the circular hole on the right side of the coupling 24 cooperates with the cylindrical protrusion structure 231 of the connecting flange 23, and they are fixed to each other by a screw fastening structure.

如图5所示,第二支承部分3由第二支撑板31、直角角码22、滑环连接法兰32和导电滑环33组成。所述第二支撑板31用于固定滑环连接法兰32和导电滑环33,为旋转扫描部分5的另一端提供支撑。第二支撑板31同样为金属板材,通过激光切割钢板得到。第二支撑板31底部设置有用于固定的通孔,中部设置有用于走线的导线孔,上部设置有用于固定滑环连接法兰32的通孔。为保证平台整体的美观性与加工的便利性,本实施例中,第二支撑板31与第一支撑板21具有相同的外形与厚度,二者底部、中部的通孔大小相等,位置相同。通过直角角码22通孔、第二支撑板31底部通孔和底板21通孔形成的螺纹连接可将第二支撑板31垂直固定在底板12上。导电滑环33是连通旋转体、输送能源与信号的电气部件。导电滑环33包含滑环外圈331与滑环内圈332,滑环外圈331略短于滑环内圈332。滑环外圈331右端面设有若干用于安装的螺孔,该端面与滑环内圈332的右端面齐平。滑环内圈332设有通孔结构,其长于滑环外圈331的端部还设有紧定螺钉。在本实施例中,导电滑环33将不断旋转的雷达核心部件采集到的电信号传输至相对静止的数据线接口141处,完全避免了导线缠绕的情况。滑环连接法兰32为回转体零件,整体呈放倒的“T”字形,即其一端为细长轴结构,另一端为盘形结构。所述滑环连接法兰32中部设有一通孔,用于容纳导线;其盘形结构端面均布若干通孔,用于固定。滑环连接法兰32细长轴一端容纳至滑环内圈332的通孔中,并通过紧定螺钉相互固定接。As shown in FIG5 , the second supporting part 3 is composed of a second supporting plate 31, a right angle bracket 22, a slip ring connection flange 32 and a conductive slip ring 33. The second supporting plate 31 is used to fix the slip ring connection flange 32 and the conductive slip ring 33, and provide support for the other end of the rotating scanning part 5. The second supporting plate 31 is also a metal plate obtained by laser cutting a steel plate. The second supporting plate 31 is provided with a through hole for fixing at the bottom, a wire hole for wiring in the middle, and a through hole for fixing the slip ring connection flange 32 at the top. In order to ensure the overall aesthetics and processing convenience of the platform, in this embodiment, the second supporting plate 31 has the same shape and thickness as the first supporting plate 21, and the through holes at the bottom and the middle of the two are equal in size and position. The second supporting plate 31 can be vertically fixed on the bottom plate 12 by a threaded connection formed by the through hole of the right angle bracket 22, the through hole at the bottom of the second supporting plate 31 and the through hole of the bottom plate 21. The conductive slip ring 33 is an electrical component that connects the rotating body and transmits energy and signals. The conductive slip ring 33 includes a slip ring outer ring 331 and a slip ring inner ring 332, and the slip ring outer ring 331 is slightly shorter than the slip ring inner ring 332. The right end face of the slip ring outer ring 331 is provided with a plurality of screw holes for installation, and the end face is flush with the right end face of the slip ring inner ring 332. The slip ring inner ring 332 is provided with a through hole structure, and its end longer than the slip ring outer ring 331 is also provided with a set screw. In this embodiment, the conductive slip ring 33 transmits the electrical signal collected by the continuously rotating radar core component to the relatively static data line interface 141, completely avoiding the situation of wire winding. The slip ring connection flange 32 is a rotating body part, and the whole is in an inverted "T" shape, that is, one end thereof is a slender shaft structure, and the other end is a disc-shaped structure. A through hole is provided in the middle of the slip ring connection flange 32 for accommodating the wire; and a plurality of through holes are evenly distributed on the end face of the disc-shaped structure for fixing. One end of the slender shaft of the slip ring connecting flange 32 is received in the through hole of the slip ring inner ring 332 and fixed to each other by means of set screws.

如图6所示,动力部分4由电机41、电机安装端盖42和电机安装套43组成。本实施例中,电机41为旋转扫描部分5的动力源。电机41为圆柱形,电机输出轴411在其一侧伸出,电机导线412在其另一侧引出,电机41靠近电机输出轴411的端面上设置有用于固定的螺孔。所述电机安装套43用于固定电机41。电机安装套43为柱状零件,中部设有可容纳电机41以及电机导线412的阶梯通孔,两端面均设置有用于固定的螺孔。所述电机安装端盖42同样用于固定电机41,其中部设有内凹圆孔用于容纳电机41端部及电机输出轴411,其端面设置有用于固定电机41和电机安装套43的通孔。螺钉穿过电机安装端盖42端面通孔,旋入电机41端面螺孔,可将电机41固定在电机安装端盖42上。螺钉穿过电机安装端盖42端面通孔,旋入电机安装套43右侧端面螺孔,可将电机安装端盖42连同电机41一起固定在电机安装套43的右端面。所述电机输出轴411容纳至联轴器24左端圆孔中,并通过螺钉紧固结构固定。As shown in FIG6 , the power part 4 is composed of a motor 41, a motor mounting end cover 42 and a motor mounting sleeve 43. In this embodiment, the motor 41 is the power source of the rotating scanning part 5. The motor 41 is cylindrical, the motor output shaft 411 extends out from one side thereof, the motor lead 412 is led out from the other side thereof, and a screw hole for fixing is arranged on the end face of the motor 41 near the motor output shaft 411. The motor mounting sleeve 43 is used to fix the motor 41. The motor mounting sleeve 43 is a columnar part, and a stepped through hole for accommodating the motor 41 and the motor lead 412 is arranged in the middle part, and screw holes for fixing are arranged on both end faces. The motor mounting end cover 42 is also used to fix the motor 41, and a concave circular hole is arranged in the middle part for accommodating the end of the motor 41 and the motor output shaft 411, and a through hole for fixing the motor 41 and the motor mounting sleeve 43 is arranged on the end face thereof. The screw passes through the through hole on the end face of the motor mounting end cover 42 and is screwed into the screw hole on the end face of the motor 41, so that the motor 41 can be fixed on the motor mounting end cover 42. The screw passes through the through hole of the motor mounting end cover 42 and is screwed into the screw hole on the right end of the motor mounting sleeve 43, so that the motor mounting end cover 42 and the motor 41 can be fixed to the right end of the motor mounting sleeve 43. The motor output shaft 411 is accommodated in the circular hole at the left end of the coupling 24 and fixed by a screw fastening structure.

如图7所示,所述旋转扫描部分5的主体是旋转骨架51,用于搭载电源模块52、控制单元53、位姿监测单元54和雷达辐射面55等雷达核心部件。所述旋转骨架51整体为“H”形的长条状结构,其两端是便于安装固定的圆柱结构,中部是便于搭载雷达核心部件的板状结构。旋转骨架51两端的圆柱结构内部设有通孔,用于容纳导线。所述旋转骨架51的中部板状结构中设有若干安装通孔,雷达核心部件通过所述安装通孔即可固定在旋转骨架51上。旋转骨架51右端圆柱结构设置有若干通孔,螺钉透过上述通孔,旋入电机安装套43左侧螺孔,可将旋转扫描部分5与第一支承部分2相互固定;旋转骨架51左端圆柱结构设置有若干螺孔,螺钉透过滑环连接法兰32盘形结构上的通孔,旋入上述螺孔中,可将旋转扫描部分5与第二支承部分3相互固定。As shown in FIG7 , the main body of the rotating scanning part 5 is a rotating skeleton 51, which is used to carry radar core components such as a power module 52, a control unit 53, a posture monitoring unit 54 and a radar radiation surface 55. The rotating skeleton 51 is an "H"-shaped long strip structure as a whole, with cylindrical structures at both ends that are easy to install and fix, and a plate-like structure in the middle that is easy to carry radar core components. Through holes are provided inside the cylindrical structures at both ends of the rotating skeleton 51 to accommodate wires. A number of mounting through holes are provided in the plate-like structure in the middle of the rotating skeleton 51, and the radar core components can be fixed on the rotating skeleton 51 through the mounting through holes. The cylindrical structure at the right end of the rotating skeleton 51 is provided with a number of through holes, and the screws pass through the through holes and are screwed into the left screw holes of the motor mounting sleeve 43, so that the rotating scanning part 5 and the first supporting part 2 can be fixed to each other; the cylindrical structure at the left end of the rotating skeleton 51 is provided with a number of screw holes, and the screws pass through the through holes on the disc-shaped structure of the slip ring connecting flange 32 and are screwed into the above screw holes, so that the rotating scanning part 5 and the second supporting part 3 can be fixed to each other.

如图8所示,本实施例中,电机导线412穿过旋转骨架51右端通孔,接入雷达核心部件;内圈引出线3321从滑环内圈(332)左端面引出,依次穿过滑环连接法兰32中部导线孔和旋转骨架51左端通孔接入雷达核心部件;外圈引出线3311从滑环外圈(331)右端面引出,依次穿过第二支撑板31上部的导线孔和第二支撑板31中部的导线孔接入搭载板14上的数据线接口141。As shown in FIG8 , in this embodiment, the motor lead 412 passes through the through hole at the right end of the rotating skeleton 51 and is connected to the radar core component; the inner ring lead wire 3321 is led out from the left end surface of the inner ring (332) of the slip ring, and passes through the wire hole in the middle of the slip ring connecting flange 32 and the through hole at the left end of the rotating skeleton 51 in sequence to connect to the radar core component; the outer ring lead wire 3311 is led out from the right end surface of the outer ring (331) of the slip ring, and passes through the wire hole on the upper part of the second support plate 31 and the wire hole in the middle of the second support plate 31 in sequence to connect to the data line interface 141 on the mounting plate 14.

旋转扫描测试时,底座部分1、第一支承部分2、电机输出轴411、第二支撑板31、滑环外圈331及其外圈引出线3311相互固定,相对静止;电机安装端盖42、电机安装套43、电机41主体结构、电机导线412、旋转扫描部分5、滑环连接法兰32、滑环内圈332和内圈引出线3321相互固定,不断旋转。During the rotation scanning test, the base part 1, the first supporting part 2, the motor output shaft 411, the second supporting plate 31, the slip ring outer ring 331 and the outer ring lead wire 3311 are fixed to each other and relatively stationary; the motor mounting end cover 42, the motor mounting sleeve 43, the motor 41 main structure, the motor wire 412, the rotation scanning part 5, the slip ring connecting flange 32, the slip ring inner ring 332 and the inner ring lead wire 3321 are fixed to each other and rotate continuously.

上列详细说明是针对本发明可行实施例的具体说明,该实施例并非用以限制本发明的专利范围,凡未脱离本发明所为的等效实施或变更,均应包含于本案的专利范围中。The above detailed description is a specific description of a feasible embodiment of the present invention. The embodiment is not intended to limit the patent scope of the present invention. Any equivalent implementation or modification that does not deviate from the present invention should be included in the patent scope of this case.

Claims (5)

1.一种孔中全方位扫描雷达天线采控系统开发测试平台,其特征在于,所述开发测试平台由底座部分(1)、第一支承部分(2)、第二支承部分(3)、动力部分(4)和旋转扫描部分(5)组成;所述底座部分(1)作为所述开发测试平台的基座,用于固定所述第一支承部分(2)和第二支承部分(3);所述第一支承部分(2)和第二支承部分(3)对称分布在底座部分(1)两侧,用于支撑所述旋转扫描部分(5);所述动力部分(4)为旋转扫描部分(5)的旋转运动提供动力;所述底座部分(1)、第一支承部分(2)和第二支承部分(3)相对固定,所述旋转扫描部分(5)可在动力部分(4)的作用下相对底座部分(1)旋转,这完全对应了实际工程中雷达核心部件相对天线套管不断旋转扫描的工作状态。1. A development and testing platform for an in-hole omnidirectional scanning radar antenna acquisition and control system, characterized in that the development and testing platform comprises a base portion (1), a first supporting portion (2), a second supporting portion (3), a power portion (4) and a rotating scanning portion (5); the base portion (1) serves as a base of the development and testing platform and is used to fix the first supporting portion (2) and the second supporting portion (3); the first supporting portion (2) and the second supporting portion (3) are symmetrically distributed on both sides of the base portion (1) and are used to support the rotating scanning portion (5); the power portion (4) provides power for the rotating scanning portion (5) to rotate; the base portion (1), the first supporting portion (2) and the second supporting portion (3) are relatively fixed, and the rotating scanning portion (5) can rotate relative to the base portion (1) under the action of the power portion (4), which fully corresponds to the working state of the radar core component in actual engineering that continuously rotates and scans relative to the antenna sleeve. 2.根据权利要求1所述的一种孔中全方位扫描雷达天线采控系统开发测试平台,其特征在于,所述底座部分(1)由脚垫(11)、底板(12)、间隔柱(13)和搭载板(14)组成;所述底板(12)为矩形板材,边缘设有若干通孔以安装脚垫(11)和间隔柱(13);所述脚垫(11)通过螺纹连接固定在底板(12)的一面;所述间隔柱(13)一端通过螺纹连接固定在底板(12)的另一面;所述搭载板(14)通过螺纹连接固定在间隔柱(13)另一端,用于搭载数据线接口(141)、电线连接器(142)、平台开关(143)和控制电路板(144);2. A development and testing platform for an all-round scanning radar antenna acquisition and control system in a hole according to claim 1, characterized in that the base part (1) is composed of a foot pad (11), a bottom plate (12), a spacer column (13) and a mounting plate (14); the bottom plate (12) is a rectangular plate, and a plurality of through holes are provided on the edge for mounting the foot pad (11) and the spacer column (13); the foot pad (11) is fixed to one side of the bottom plate (12) by a threaded connection; one end of the spacer column (13) is fixed to the other side of the bottom plate (12) by a threaded connection; the mounting plate (14) is fixed to the other end of the spacer column (13) by a threaded connection, and is used to carry a data line interface (141), a wire connector (142), a platform switch (143) and a control circuit board (144); 所述第一支承部分(2)垂直固定在所述底座部分(1)的一侧,由第一支撑板(21)、直角角码(22)、连接法兰(23)和联轴器(24)组成;所述第一支撑板(21)通过直角角码(22)垂直固定在底板(12)上;所述连接法兰(23)为盘形,其中部设置有圆柱凸起结构(231);所述连接法兰(23)端面通过螺钉与第一支撑板(21)的侧面固连,连接法兰(23)中部的所述圆柱凸起结构(231)与联轴器(24)的一端固连;The first supporting portion (2) is vertically fixed to one side of the base portion (1), and is composed of a first supporting plate (21), a right-angle bracket (22), a connecting flange (23), and a coupling (24); the first supporting plate (21) is vertically fixed to the base plate (12) via the right-angle bracket (22); the connecting flange (23) is disc-shaped, and a cylindrical protruding structure (231) is provided in the middle thereof; the end surface of the connecting flange (23) is fixedly connected to the side surface of the first supporting plate (21) via screws, and the cylindrical protruding structure (231) in the middle of the connecting flange (23) is fixedly connected to one end of the coupling (24); 所述第二支承部分(3)垂直固定在所述底座部分(1)的另一侧,由第二支撑板(31)、直角角码(22)、滑环连接法兰(32)和导电滑环(33)组成;所述第二支撑板(31)通过直角角码(22)垂直固定在底板(12)上;所述滑环连接法兰(32)为回转体零件,整体呈放倒的“T”字形,其一端为细长轴,另一端为扁平的盘形结构;所述导电滑环(33)包含滑环外圈(331)和滑环内圈(332),所述滑环外圈(331)可绕所述滑环内圈(332)旋转;所述滑环连接法兰(32)的细长轴端通过紧定螺钉与所述滑环内圈(332)固连;所述滑环外圈(331)端面通过螺钉与第二支撑板(31)侧面固连;The second supporting portion (3) is vertically fixed to the other side of the base portion (1), and is composed of a second supporting plate (31), a right-angle bracket (22), a slip ring connecting flange (32) and a conductive slip ring (33); the second supporting plate (31) is vertically fixed to the base plate (12) by the right-angle bracket (22); the slip ring connecting flange (32) is a rotating body part, and is in an inverted "T" shape as a whole, with one end being a slender shaft and the other end being a flat disc-shaped structure; the conductive slip ring (33) comprises a slip ring outer ring (331) and a slip ring inner ring (332), and the slip ring outer ring (331) can rotate around the slip ring inner ring (332); the slender shaft end of the slip ring connecting flange (32) is fixedly connected to the slip ring inner ring (332) by a set screw; the end face of the slip ring outer ring (331) is fixedly connected to the side of the second supporting plate (31) by a screw; 所述动力部分(4)由电机(41)、电机安装端盖(42)和电机安装套(43)组成;所述电机(41)为圆柱形,电机输出轴(411)在其一侧伸出,所述电机(41)靠近电机输出轴(411)的端面上设置有安装螺孔;所述电机安装端盖(42)设置有与所述安装螺孔相配合的通孔;所述电机(41)通过螺钉与所述电机安装端盖(42)固连;所述电机安装套(43)为圆柱形,其内部设有可容纳所述电机(41)的圆孔;电机安装套(43)一端通过螺钉与所述电机安装端盖(42)固连;所述电机输出轴(411)容纳至所述联轴器(24)的另一端,并通过紧定螺钉固定;The power part (4) is composed of a motor (41), a motor mounting end cover (42) and a motor mounting sleeve (43); the motor (41) is cylindrical, the motor output shaft (411) extends out from one side of the motor, and a mounting screw hole is provided on the end surface of the motor (41) close to the motor output shaft (411); the motor mounting end cover (42) is provided with a through hole matching the mounting screw hole; the motor (41) is fixedly connected to the motor mounting end cover (42) by screws; the motor mounting sleeve (43) is cylindrical, and a circular hole capable of accommodating the motor (41) is provided inside the cylindrical sleeve; one end of the motor mounting sleeve (43) is fixedly connected to the motor mounting end cover (42) by screws; the motor output shaft (411) is accommodated in the other end of the coupling (24) and fixed by a set screw; 所述旋转扫描部分(5)包括旋转骨架(51)、电源模块(52)、控制单元(53)、位姿监测单元(54)和雷达辐射面(55);所述旋转骨架(51)为长条状结构,其一端通过螺钉与所述滑环连接法兰(32)固定,另一端通过螺钉与所述电机安装套(43)固定;所述电源模块(52)、控制单元(53)、位姿监测单元(54)和雷达辐射面(55)固定在所述旋转骨架(51)上。The rotating scanning part (5) comprises a rotating skeleton (51), a power module (52), a control unit (53), a posture monitoring unit (54) and a radar radiating surface (55); the rotating skeleton (51) is a long strip structure, one end of which is fixed to the slip ring connecting flange (32) by screws, and the other end of which is fixed to the motor mounting sleeve (43) by screws; the power module (52), the control unit (53), the posture monitoring unit (54) and the radar radiating surface (55) are fixed to the rotating skeleton (51). 3.根据权利要求2所述的一种孔中全方位扫描雷达天线采控系统开发测试平台,其特征在于,所述直角角码(22)与所述底板(12)通过螺栓螺母固定,所述直角角码(22)与所述第一支撑板(21)通过螺栓螺母固定,所述直角角码(22)与所述第二支撑板(31)通过螺栓螺母固定。3. The development and testing platform of the in-hole omnidirectional scanning radar antenna acquisition and control system according to claim 2, characterized in that the right-angle bracket (22) and the base plate (12) are fixed by bolts and nuts, the right-angle bracket (22) and the first support plate (21) are fixed by bolts and nuts, and the right-angle bracket (22) and the second support plate (31) are fixed by bolts and nuts. 4.根据权利要求2所述的一种孔中全方位扫描雷达天线采控系统开发测试平台,其特征在于,所述滑环内圈(332)与滑环连接法兰(32)为同轴固定;所述滑环连接法兰(32)与旋转骨架(51)为同轴固定;所述旋转骨架(51)与电机安装套(43)为同轴固定;所述电机安装套(43)与电机安装端盖(42)为同轴固定;所述电机安装端盖(42)与电机(41)为同轴固定;所述电机输出轴(411)与联轴器(24)为同轴固定;所述联轴器(24)与连接法兰(23)的圆柱凸起结构(231)为同轴固定。4. According to claim 2, a development and testing platform for an in-hole omnidirectional scanning radar antenna acquisition and control system, characterized in that the slip ring inner ring (332) and the slip ring connecting flange (32) are coaxially fixed; the slip ring connecting flange (32) and the rotating skeleton (51) are coaxially fixed; the rotating skeleton (51) and the motor mounting sleeve (43) are coaxially fixed; the motor mounting sleeve (43) and the motor mounting end cover (42) are coaxially fixed; the motor mounting end cover (42) and the motor (41) are coaxially fixed; the motor output shaft (411) and the coupling (24) are coaxially fixed; the coupling (24) and the cylindrical protrusion structure (231) of the connecting flange (23) are coaxially fixed. 5.根据权利要求2所述的一种孔中全方位扫描雷达天线采控系统开发测试平台,其特征在于,所述滑环连接法兰(32)中部设有通孔结构(321),用于容纳内圈引出线(3321);所述第二支撑板(31)中部设有通孔,用于容纳外圈引出线(3311);所述电机安装套(43)和旋转骨架(51)端部设有通孔,用于容纳电机导线(412)。5. According to claim 2, a development and testing platform for an in-hole omnidirectional scanning radar antenna acquisition and control system, it is characterized in that a through hole structure (321) is provided in the middle of the slip ring connecting flange (32) for accommodating the inner ring lead wire (3321); a through hole is provided in the middle of the second support plate (31) for accommodating the outer ring lead wire (3311); and through holes are provided at the ends of the motor mounting sleeve (43) and the rotating skeleton (51) for accommodating the motor wire (412).
CN202410337597.2A 2024-03-23 2024-03-23 Development test platform for in-hole omnibearing scanning radar antenna acquisition and control system Pending CN118169641A (en)

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