Servo driving device for radar photoelectric integrated investigation system

By designing a servo drive device for radar photoelectric integrated detection system, the existing system has solved the problems of large size, heavy weight, complex structure and equipment interference, and the use of portability, easy disassembly and independent non-interference in the sub-system is achieved, reducing the system complexity and facilitating production and maintenance.

CN222783293UActive Publication Date: 2025-04-22XIAN TIANYUAN ELECTRO-OPTICAL TECH CO LTD
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Patent Information

Application Number
CN202420747458.2
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-04-11
Publication Date
2025-04-22
Estimated Expiration
2034-04-11

AI Technical Summary

Technical Problem

The servo drive platform of the existing radar photoelectric reconnaissance system is large in size and heavy in weight, which is inconvenient for portability, complex structure, and many assembly links, making it inconvenient for system disassembly and assembly. The radar and optoelectronic equipment can only rotate along the way, which has interference problems.

Method used

A servo drive device for radar photoelectric integrated detection system is designed. Through the combination of corresponding shaft system, mechanical interface and shell, radar azimuth servo drive and photoelectric azimuth and pitch servo drive are realized, simplifying the system design and convenient for users to use.

Benefits of technology

It realizes the portability, easy disassembly and assembly of the radar photoelectric detection system and the independent and non-interference use of the sub-system, reducing the complexity of the system and facilitating production and maintenance.

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Abstract

The utility model belongs to the field of radar photoelectric investigation system design, and particularly relates to a servo driving device for a radar photoelectric integrated investigation system. A servo driving platform used by a radar photoelectric investigation system mainly depends on a vehicle-mounted or ship-borne servo driving platform, the size is large, the weight is heavy, the structure is complex, a radar and photoelectric investigation equipment can only rotate in a follow-up mode, and certain interference can be generated between the systems. The utility model designs a novel servo driving device for a radar photoelectric integrated investigation system, which comprises a photoelectric servo driving component at the lower part and a radar servo driving component at the upper part, radar azimuth servo drive and photoelectric azimuth and pitching servo drive can be combined into a servo drive system through a corresponding shaft system, a mechanical interface, a shell and the like, the design link and difficulty of a radar photoelectric investigation system can be greatly simplified, and convenience is brought to a user.
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Description

Technical Field

[0001] The utility model belongs to the field of radar photoelectric detection system design, and specifically relates to a servo drive device for a radar photoelectric integrated detection system. Background Art

[0002] At present, in the field of radar optoelectronic detection systems, the servo drive platform used by radar optoelectronic detection systems mainly relies on vehicle-mounted or ship-mounted systems. If it is to be applied to complex environments that are difficult for vehicles and ships to reach or scenarios where a single person is required to carry it, many problems will arise, including:

[0003] 1. Large size and heavy weight make it inconvenient to carry;

[0004] 2. The structure is complex and there are too many assembly links, which makes it inconvenient to disassemble and assemble the system;

[0005] 3. Radar and optoelectronic reconnaissance equipment can only rotate with the system, which will cause certain interference between the systems.

[0006] Therefore, a new type of servo drive device is needed to make the radar optoelectronic integrated detection system portable, easy to disassemble and assemble, and independent of subsystem interference. Utility Model Content

[0007] In response to the above needs, the utility model designs a new servo drive device for a radar optoelectronic integrated detection system, which can combine the radar azimuth servo drive, optoelectronic azimuth and pitch servo drives into a servo drive system through corresponding axis systems, mechanical interfaces and housings, which can greatly simplify the design links and difficulty of the radar optoelectronic detection system and is convenient for users.

[0008] In order to achieve the above tasks, the technical solutions adopted by the utility model are as follows:

[0009] A servo drive device for a radar optoelectronic integrated detection system comprises a lower optoelectronic servo drive component and an upper radar servo drive component, wherein

[0010] The photoelectric servo drive component includes a photoelectric servo base plate fixed on a tripod or other mounting platform, and a photoelectric drive movement assembly is provided in a shield on the upper part of the photoelectric servo base plate, wherein the photoelectric azimuth servo motor assembly drives the shield to rotate synchronously, wherein the photoelectric pitch servo motor assembly and the load pitch axis driven by it rotate synchronously with the photoelectric azimuth servo motor assembly, and the load pitch axis extends out of the shield to be connected with the photoelectric detection system;

[0011] The radar servo drive component is installed on the optoelectronic servo interface base through the radar servo base, and the optoelectronic servo interface base is fixedly connected to the rotor part of the optoelectronic azimuth servo motor assembly; the radar servo drive component also includes a radar servo motor assembly, whose stationary part is installed on the radar servo base, and a rotor mounting plate is installed on the top of its rotor part, and a radar servo assembly cover is installed on the lower side of the rotor mounting plate, and the upper side is connected to the radar sensor.

[0012] Advantageously, the photoelectric drive movement assembly further comprises a substrate, through which a photoelectric azimuth servo motor assembly is installed, wherein a stator portion of the motor is fixedly connected to the substrate, and a rotor portion is connected to the bottom base structure.

[0013] Advantageously, a load pitch axis and a photoelectric pitch servo motor assembly are respectively installed on the upper part of the substrate and on both sides of the photoelectric azimuth servo motor assembly, and the pitch motor axis of the photoelectric pitch servo motor assembly is connected to the load pitch axis via a C-shaped axis.

[0014] Advantageously, a bearing bracket is installed at one end of the base plate, on which a deep groove ball bearing is installed through a bearing cover to support the load pitch axis, and is limited by two limiters on the bearing bracket; a motor bracket is installed at the other end of the base plate, on which an optoelectronic pitch servo motor assembly is installed, and the pitch motor shaft is installed on the rotor of the optoelectronic pitch servo motor assembly.

[0015] Advantageously, a limit column is installed at one end of the C-shaped shaft close to the bearing bracket.

[0016] Advantageously, the protective cover includes a protective cover under the photoelectric servo platform and a protective cover on the photoelectric servo platform. The lower end of the protective cover under the photoelectric servo platform is installed on the photoelectric servo bottom plate through a photoelectric servo base. The photoelectric servo base is the base of the photoelectric drive component and is a bowl-shaped structure with installation space reserved for wires and circuit components.

[0017] Advantageously, a tube-in-tube structure is provided between the radar servo base and the optoelectronic servo interface base, which are clamped and connected via a locking device base and a rapid indexing locking device.

[0018] Advantageously, a cable shield is also installed in the space of the optoelectronic servo interface base.

[0019] Advantageously, a wire binding rack is provided at the lower end of the radar servo base.

[0020] Advantageously, during operation, the upper radar servo drive component controls the radar sensor to rotate in azimuth independently of the optoelectronic servo drive component, and the lower optoelectronic servo drive component controls the optoelectronic detection system to rotate in azimuth and elevation directions.

[0021] Beneficial effects:

[0022] 1. The overall structure of the utility model is compact, adopts new non-metallic materials, is small in size, light in weight, and easy to carry and transport;

[0023] 2. The motor assembly with integrated slip ring and encoder is used internally, which reduces a lot of adapters and improves the system shaft system accuracy;

[0024] 3. Modular design is adopted to reduce the complexity of the system and facilitate production and maintenance;

[0025] 4. The quick disassembly and assembly mechanical interface is adopted, which can complete the installation and construction of the system conveniently and quickly;

[0026] 5. The radar and optoelectronic drive parts can work together or independently, and the subsystems do not interfere with each other.

[0027] The features, functions, and advantages that have been discussed can be achieved independently in various examples or may be combined in yet other examples. BRIEF DESCRIPTION OF THE DRAWINGS

[0028] The following description with reference to the accompanying drawings can provide a more complete understanding of the content of the present invention.

[0029] Figure 1 It is an oblique view of the servo drive device of the utility model;

[0030] Figure 2 This is a front view of the servo drive device of the utility model;

[0031] Figure 3 for Figure 2 AA section view;

[0032] Figure 4 It is a structural schematic diagram of the photoelectric servo drive component;

[0033] Figure 5 Schematic diagram of the bottom of the optoelectronic servo drive component.

[0034] 1- photoelectric servo base plate, 2- photoelectric servo base, 3- photoelectric servo platform lower shield, 4- photoelectric drive movement assembly, 5- photoelectric servo platform upper shield, 6- photoelectric servo interface base, 7- locker base, 8- fast indexing locker, 9- cable shield, 10- wire tie rack, 11- radar servo base, 12- radar servo motor assembly, 13- radar servo assembly housing, 14- rotor mounting plate, 401- base plate, 402- load pitch axis, 403- bearing bracket, 404- deep groove ball bearing, 405- bearing cover, 406- C-type shaft, 407- limit column, 408- limiter, 409- pitch motor shaft, 410- motor bracket, 411- photoelectric azimuth servo motor assembly, 412- photoelectric pitch servo motor assembly DETAILED DESCRIPTION

[0035] The disclosed examples will be more fully described with reference to the accompanying drawings, in which some (but not all) of the disclosed examples are shown. In fact, many different examples may be described and these examples should not be construed as limited to the examples set forth herein. On the contrary, describing these examples makes the disclosure of the present invention thorough and complete and will fully convey the scope of the present disclosure to those skilled in the art.

[0036] like Figure 1-3 As shown, the servo drive device for the radar optoelectronic integrated detection system corresponding to this embodiment includes a lower optoelectronic servo drive component and an upper radar servo drive component as a whole, specifically including an optoelectronic servo bottom plate 1, an optoelectronic servo base 2, an optoelectronic servo platform lower shield 3, an optoelectronic drive movement assembly 4, an optoelectronic servo platform upper shield 5, a light mine servo interface base 6, a locking device base 7, a rapid indexing locking device 8, a cable shield 9, a wire tie rack 10, a radar servo base 11, a radar servo motor assembly 12, a radar servo assembly housing 13, and a rotor mounting plate 14.

[0037] The photoelectric servo drive component is composed of the photoelectric servo bottom plate 1, the photoelectric servo base 2, the photoelectric servo platform lower shield 3, the photoelectric servo platform upper shield 5, the light mine servo interface base 6, the locker base 7, the fast indexing locker 8 and the cable shield 9 around the photoelectric drive movement assembly 4. The radar servo drive component is composed of the wire binding rack 10, the radar servo base 11, the radar servo assembly housing 13 and the rotor mounting plate 14 around the radar servo motor assembly 12. The two components are docked through a cylindrical mechanical interface with a limiter and positioned and locked with an indexing locker.

[0038] The photoelectric servo base plate 1 is an adapter plate between the servo drive device and the tripod or other mounting platform, and corresponding mounting holes can be designed as needed. The photoelectric servo base 2 is the base of the photoelectric drive component, which is a bowl-shaped structure with reserved installation space for wires and circuit components. The lower shield 3 of the photoelectric servo platform and the upper shield 5 of the photoelectric servo platform are protective covers, which are printed with new non-metallic materials, which can not only reduce weight but also facilitate production and manufacturing. They are fixed to the photoelectric drive movement assembly 4 by screws and move with the photoelectric drive movement assembly 4. The photoelectric servo interface base 6 is the mechanical interface between the photoelectric servo drive component and the radar servo drive component. It is installed on the photoelectric drive movement assembly 4 by screws and locating pins, and is docked and locked with the radar servo base 11 at the upper end. It does not move with the photoelectric drive movement assembly 4, and can realize the rotational movement of the photoelectric detection system in the azimuth and pitch directions.

[0039] The locking device base 7 and the fast indexing locking device 8 are fixed on the light-ray servo interface base 6 by screws to form a quick disassembly mechanism. The cable shield 9 is installed on the light-ray servo interface base 6 to protect the internal cables.

[0040] like Figure 4-5 As shown, the photoelectric drive movement assembly 4 includes a base plate 401, a load pitch axis 402, a bearing bracket 403, a deep groove ball bearing 404, a bearing cover 405, a C-shaped axis 406, a limit column 407, a limiter 408, a pitch motor axis 409, a motor bracket 410, a photoelectric azimuth servo motor assembly 411 and a photoelectric pitch servo motor assembly 412. The inner ring of the deep groove ball bearing 404 is coaxially fixedly connected to the load pitch axis 402, and the outer ring is fixedly connected to the bearing bracket 403. The load pitch axis 402, the C-shaped axis 406, the pitch motor axis 409 and the photoelectric pitch servo motor assembly 412 are coaxially fixedly connected, and the load pitch axis 402 can be docked to install a photoelectric detection system.

[0041] The bearing bracket 403 is fixed to the base plate 401 by screws and locating pins, the outer ring of the deep groove ball bearing 404 is fixed to the bearing bracket 403 by a bearing cover 405, two limiters 408 are installed on the bearing bracket 403 at a certain angle, the load pitch axis 402 cooperates with the inner ring of the deep groove ball bearing 404, and then is positioned and driven by a key with one end of the C-type axis 406, and a limiting column 407 is installed at this end of the C-type axis 406, and the other end of the C-type axis 406 is fixed to the pitch motor shaft 409 by keys and pins, and the pitch motor shaft 409 is installed on the rotor of the optoelectronic pitch servo motor assembly 412 by screws and locating pins, and the stator of the optoelectronic pitch servo motor assembly 412 is fixed to the motor bracket 410 by locating pins and screws, and the motor bracket 410 is installed on the base plate 401 by screws and locating pins.

[0042] The above components can form a pitch axis system, which drives the axis system to rotate in the pitch direction under the drive of the photoelectric pitch servo motor assembly 412. At the same time, the pitch angle range can be limited under the action of the limiter 408 to prevent excessive or uncontrolled rotation. After the pitch axis system is installed on the substrate 401, the substrate 401 is fixed on the photoelectric azimuth servo motor assembly 411. The photoelectric azimuth servo motor assembly 411 has a stator part on the outside and a rotor part on the inside. Under the drive of the photoelectric azimuth servo motor assembly 411, the substrate 401 can rotate in the azimuth direction.

[0043] Regarding the radar servo drive component, the wire tie rack 10 is installed inside the radar servo base 11 and is used to bundle the wire harness. The radar servo base 11 is the base of the drive component and is designed with a positioning guide structure, which can be used as a mechanical interface for docking with the optoelectronic drive component. The stationary part of the radar servo motor assembly 12 is installed on the radar servo base 11 by screws and positioning pins, the rotor mounting plate 14 is installed on the top of the rotor part of the radar servo motor assembly 12 by screws and positioning pins, the radar servo assembly cover 13 is fixed to the lower side of the outer ring of the rotor mounting plate 14 by screws, and the radar sensor is installed on the upper side of the rotor mounting plate 14 by a transition piece. The radar servo motor assembly 12 can drive the radar servo assembly cover 13, the rotor mounting plate 14 and the radar sensor to rotate stably at a certain speed.

[0044] When the entire drive device is working, the upper radar servo drive component can work independently of the optoelectronic servo drive component and rotate in the azimuth direction, and the lower optoelectronic servo drive component can rotate in the azimuth and pitch directions.

[0045] The purpose of the examples and descriptions presented has been to illustrate descriptions of different advantageous arrangements, but the descriptions are not intended to be exclusive or limited to examples of the disclosed form. Many modifications and variations will be apparent to those skilled in the art. In addition, different advantageous examples may be described as having different advantages compared to other advantageous examples. The selected example or examples are selected and described in order to best illustrate the principles of the examples, practical applications, and to enable those of ordinary skill in the art to understand the disclosure of various examples with various modifications suitable for the particular use contemplated.

Claims

1. A servo drive device for a radar optoelectronic integrated detection system, characterized in that: The device comprises a lower optoelectronic servo drive component and an upper radar servo drive component, wherein The photoelectric servo drive component comprises a photoelectric servo base plate (1) fixed on a tripod or a mounting platform, a photoelectric drive movement assembly (4) is provided in a protective cover on the upper part of the photoelectric servo base plate (1), wherein the photoelectric azimuth servo motor assembly (411) drives the protective cover to rotate synchronously, the photoelectric pitch servo motor assembly (412) and the load pitch axis (402) driven by the photoelectric azimuth servo motor assembly (411) rotate synchronously with the photoelectric azimuth servo motor assembly (411), and the load pitch axis (402) extends out of the protective cover to connect with the photoelectric detection system; The radar servo drive component is mounted on an optoelectronic servo interface base (6) via a radar servo base (11), and the optoelectronic servo interface base (6) is fixedly connected to the rotor part of the optoelectronic azimuth servo motor assembly (411); the radar servo drive component also includes a radar servo motor assembly (12), the stationary part of which is mounted on the radar servo base (11), the top end of the rotor part of which is mounted with a rotor mounting plate (14), the lower side of which is mounted with a radar servo assembly cover (13), and the upper side of which is connected to a radar sensor.

2. The servo drive device for radar optoelectronic integrated detection system according to claim 1, characterized in that: The photoelectric drive movement assembly (4) further comprises a substrate (401), through which a photoelectric azimuth servo motor assembly (411) is installed, the stator portion of which is fixedly connected to the substrate (401), and the rotor portion of which is connected to the bottom base structure.

3. The servo drive device for the radar optoelectronic integrated detection system according to claim 2, characterized in that: A load pitch axis (402) and a photoelectric pitch servo motor assembly (412) are respectively installed on the upper part of the substrate (401) and on both sides of the photoelectric azimuth servo motor assembly (411); a pitch motor axis (409) of the photoelectric pitch servo motor assembly (412) is connected to the load pitch axis (402) via a C-shaped axis (406).

4. The servo drive device for the radar optoelectronic integrated detection system according to claim 3, characterized in that: A bearing bracket (403) is installed at one end of the base plate (401), on which a deep groove ball bearing (404) is installed through a bearing cover (405) to support the load pitch axis (402), and the bearing bracket (403) is limited by two limiters (408) on the bearing bracket (403); a motor bracket (410) is installed at the other end of the base plate (401), on which an optoelectronic pitch servo motor assembly (412) is installed, and the pitch motor shaft (409) is installed on the rotor of the optoelectronic pitch servo motor assembly (412).

5. The servo drive device for radar optoelectronic integrated detection system according to claim 4, characterized in that: A limiting column (407) is installed at one end of the C-shaped shaft (406) close to the bearing bracket (403).

6. The servo drive device for the radar optoelectronic integrated detection system according to claim 5, characterized in that: The protective cover comprises a protective cover (3) below the photoelectric servo platform and a protective cover (5) above the photoelectric servo platform. The lower end of the protective cover (3) below the photoelectric servo platform is mounted on the photoelectric servo base (1) via a photoelectric servo base (2). The photoelectric servo base (2) is the base of the photoelectric drive component and is a bowl-shaped structure. Space is reserved inside for mounting wires and circuit components.

7. The servo drive device for the radar optoelectronic integrated detection system according to claim 6, characterized in that: A tube-enclosed structure is provided between the radar servo base (11) and the photoelectric servo interface base (6), and is clamped and connected via a locking device base (7) and a rapid indexing locking device (8).

8. The servo drive device for the radar optoelectronic integrated detection system according to claim 7, characterized in that: A cable shield (9) is also installed in the space of the photoelectric servo interface base (6).

9. The servo drive device for the radar optoelectronic integrated detection system according to claim 8, characterized in that: A wire binding rack (10) is provided at the lower end of the radar servo base (11).

10. The servo drive device for a radar optoelectronic integrated detection system according to any one of claims 1 to 9, characterized in that: During operation, the upper radar servo drive component controls the rotation of the radar sensor in the azimuth direction independently of the optoelectronic servo drive component, and the lower optoelectronic servo drive component controls the rotation of the optoelectronic detection system in the azimuth and elevation directions.