A test equipment for multiple types of missile-mounted servos

The multi-model missile-mounted servo test device addresses the limitations of single-category testing by offering intuitive and portable servo testing with real-time data processing and clear results, facilitating versatile servo testing across different models.

CN114442588BActive Publication Date: 2025-01-03CHANGJIE INFORMATION SYSTEMS (SHANGHAI) CO LTD
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Patent Information

Application Number
CN202111576380.X
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2021-12-22
Publication Date
2025-01-03
Estimated Expiration
2041-12-22

AI Technical Summary

Technical Problem

Current servo test equipment is limited to single test categories and provides non-intuitive test results, necessitating a multi-model missile-mounted servo test device with intuitive testing capabilities.

Method used

A multi-model missile-mounted servo test device comprising a device housing with a servo test system, connected to a loading and unloading device, signal conditioning unit, data acquisition channel, and computer control system, featuring a PCI bus controller, intuitive display, and modular design for testing various servo types.

Benefits of technology

Enables real-time data collection and processing of servo performance parameters, providing clear and concise test results through a human-machine interface, with enhanced portability and ease of operation due to a movable keyboard and multiple USB interfaces.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present invention relates to the field of servo test technology, and discloses a multi-model missile-mounted servo test device, including a device housing and a servo test system, wherein the servo test system is electrically connected to a loading and unloading device, wherein the loading and unloading device is electrically connected to a loading and unloading control device, and wherein the loading and unloading control device is electrically connected to a signal conditioning unit. During the test, the multi-model missile-mounted servo test device firstly performs a series of mechanical actions such as loading and unloading in accordance with the test requirements, the test system outputs a control signal corresponding to the detection task, the test product completes the specified action in accordance with the instruction requirements, and each signal is output to a data acquisition component through an electrical interface, and under the control of a computer, data is collected for each action signal, instruction information, and each analog and digital variable from the beginning of the work, the data is received by a controller module and a computer, and finally the computer control system performs real-time storage and processing, and displays the processing results at the same time.
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Description

Technical Field

[0001] The invention relates to the technical field of servo testing, in particular to a multi-model missile-mounted servo testing device. Background Art

[0002] As a servo actuator, electric servos are increasingly widely used in drones, guided bombs and spacecraft. Servos are important flight control actuators for aircraft and are a type of high-precision displacement control system. In order to ensure the research and development quality of servos, servo test equipment is required to test various indicators of servos under actual working conditions.

[0003] The current servo test equipment has problems such as single test category and non-intuitive test results. It can be seen that there is an urgent need for a multi-model missile-mounted servo test equipment. Summary of the invention

[0004] 1. Technical issues to be solved

[0005] In view of the deficiencies in the prior art, the present invention provides a multi-model missile-mounted servo test device, which has the advantages of intuitive test structure and the like, and solves the problem that the prior test results are not intuitive.

[0006] (II) Technical solution

[0007] To achieve the above-mentioned purpose, the present invention provides the following technical solutions: a multi-model missile-mounted servo test equipment, comprising a device housing and a servo test system, the servo test system is electrically connected to a loading and unloading device, the loading and unloading device is electrically connected to a loading and unloading control device, the loading and unloading control device is electrically connected to a signal conditioning unit, the signal conditioning unit is electrically connected to a computer control system, the loading and unloading device is also electrically connected to a data acquisition channel, the data acquisition channel is electrically connected to the signal conditioning unit, the servo test system is also electrically connected to an electrical interface output, the electrical interface output is electrically connected to the data acquisition channel, the servo test system is also electrically connected to an electrical interface input, the electrical interface input is electrically connected to a signal source module, and the servo test system is also electrically connected to an isolation protection plug and an electrical interface test device.

[0008] Preferably, a display screen is provided on the front of the device housing, and a keyboard is provided on the front of the display screen.

[0009] Preferably, a metal hinge is hinged at the bottom end of the keyboard, and the other end of the metal hinge is fixedly connected to the device housing.

[0010] Preferably, a heat dissipation portion is provided on one side of the device housing, a power status observation column is provided at the bottom of the heat dissipation portion, and a USB interface is provided on the side of the power status observation column.

[0011] Preferably, a switch is provided on the other side of the device housing, and a network cable interface is provided on the side of the switch.

[0012] Preferably, rounded corners are provided on both sides of the front top of the keyboard, and keyboard fixing buckles are provided on both sides of the device housing.

[0013] Preferably, a handle is fixedly mounted on the top of the device housing.

[0014] Preferably, the keyboard fixing buckle includes a keyboard fixing base fixedly connected to the device housing, a synchronization bar is provided on the front of the keyboard fixing base, a telescopic column is fixedly installed on one side of the back of the synchronization bar, and the other end of the telescopic column is fixedly connected to the front wall of the device housing.

[0015] Preferably, a synchronization column is fixedly installed on the other side of the back of the synchronization bar, the other end of the synchronization column passes through the front wall of the keyboard fixing seat and is fixedly connected to a limiting spring, and a synchronization plate is fixedly installed on the side of the synchronization column.

[0016] Preferably, the other end of the synchronization plate passes through the inner wall of the keyboard fixing seat and is fixedly connected to a connecting rod, and the other end of the connecting rod is hinged to a limiting seat.

[0017] Preferably, a sliding block is fixedly installed on the back of the limiting seat, and the other end of the sliding block is slidably connected to the keyboard fixing seat. A spring rod is fixedly installed on the side of the limiting seat, and the other end of the spring rod is fixedly connected to the limiting plate.

[0018] Compared with the prior art, the present invention provides a multi-model missile-mounted servo test device, which has the following beneficial effects:

[0019] 1. This multi-model missile-mounted servo test equipment adopts a PCI bus controller. According to the system test task requirements, the control system first performs a self-check of the equipment. After the self-check is normal, the product performance parameter test can be performed. During the test, the loading and unloading switching mechanism first completes a series of mechanical actions such as loading and unloading according to the test requirements. The test system outputs a control signal corresponding to the detection task. The test product completes the specified action according to the instruction requirements. Each signal is output to the data acquisition component through the electrical interface. Under the control of the computer, data is collected for each action signal, instruction information, and each analog and digital variable from the beginning of work. The data is received by the controller module and the computer, and finally stored and processed in real time by the computer control system, and the processing results are displayed at the same time. There are multiple USB interfaces, and various types of servos can be tested by replacing the connecting wires, which has strong applicability.

[0020] 2. In this multi-model missile-mounted servo test equipment, the keyboard fixing buckle is used to fix the keyboard on the front side of the device housing. The metal hinge allows the keyboard to be movable, thereby ensuring the keyboard's storability. When the keyboard needs to be used, the keyboard fixing buckle is released to fix the keyboard, and the keyboard is flipped to a vertical state with the device housing. The keyboard can be used to perform related operations, making the entire device simple to install, light and easy to operate, light in size, and easy to carry. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] Figure 1 It is a schematic diagram of the working principle of the present invention;

[0022] Figure 2 It is a front view schematic diagram of the structure of the present invention;

[0023] Figure 3 It is a left side schematic diagram of the structure of the present invention;

[0024] Figure 4 It is a right side schematic diagram of the structure of the present invention;

[0025] Figure 5 This is a schematic diagram of the keyboard fixing buckle structure of the present invention;

[0026] Figure 6 It is a top view schematic diagram of the keyboard fixing buckle structure of the present invention.

[0027] Among them: 1. Device shell; 2. Display screen; 3. Keyboard; 4. Metal hinge; 5. Heat dissipation; 6. Power status observation bar; 7. USB interface; 8. Switch; 9. Network cable interface; 10. Rounded corners; 11. Keyboard fixing buckle; 111. Keyboard fixing seat; 112. Synchronization bar; 113. Telescopic column; 114. Synchronization column; 115. Limit spring; 116. Synchronization plate; 117. Connecting rod; 118. Limit seat; 119. Sliding block; 120. Spring rod; 121. Limit plate; 12. Handle. DETAILED DESCRIPTION

[0028] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0029] See also Figure 1-6A multi-model missile-mounted servo test device includes a device housing 1 and a servo test system, the servo test system is electrically connected to a loading and unloading device, the loading and unloading device is electrically connected to a loading and unloading control device, the loading and unloading control device is electrically connected to a signal conditioning unit, the signal conditioning unit is telecommunication-connected to a computer control system, the loading and unloading device is also electrically connected to a data acquisition channel, the data acquisition channel is telecommunication-connected to the signal conditioning unit, the servo test system is also electrically connected to an electrical interface output, the electrical interface output is electrically connected to the data acquisition channel, the servo test system is also electrically connected to an electrical interface input, the electrical interface input is electrically connected to a signal source module, and the servo test system is also electrically connected to an isolation protection plug and an electrical interface test device.

[0030] In the above technical solution, the test equipment can provide the working environment required for the normal operation of the servo drive controller, including working power supply, load unit and component simulation, etc. The test equipment has the functions of collecting, storing and analyzing the analog signals output by the servo control driver. It has a good human-machine interface, which can conveniently set the working status of the product and display the working status of the product. It also has data analysis and judgment functions, power-on self-test and overload protection, and is equipped with a metering interface, which can conveniently measure the test equipment.

[0031] This equipment uses a PCI bus controller. According to the system test task requirements, the operating control system first performs a self-check of the equipment. After the self-check is normal, the product performance parameter test can be performed. During the test, the loading and unloading switching mechanism first completes a series of mechanical actions such as loading and unloading according to the test requirements. The test system outputs a control signal corresponding to the test task. The test product completes the specified action according to the instruction requirements. Each signal is output to the data acquisition component through the electrical interface. Under the control of the computer, data is collected from each action signal, instruction information, and each analog and digital variable from the beginning of the work. The data is received by the controller module and the computer, and finally stored and processed in real time by the computer control system, and the processing results are displayed at the same time.

[0032] The equipment uses computer real-time control to accurately adjust various test conditions. Control instructions are transmitted through CNC power supply and communication lines. After receiving the instructions, the servo drives act according to the instructions. The generated feedback signal is fed back to the computer through the acquisition card for processing and then the output result is displayed in real time on the operation interface and stored in the database. It can be played back after the test is completed. At the same time, the test data can be generated into a PDF report display, which is concise and clear.

[0033] The input instructions are transmitted to the control unit through the computer to operate the CNC power supply, storage device and acquisition card to complete the servo test.

[0034] Specifically, a display screen 2 is provided on the front of the device housing 1, a keyboard 3 is provided on the front of the display screen 2, a metal hinge 4 is hinged at the bottom end of the keyboard 3, the other end of the metal hinge 4 is fixedly connected to the device housing 1, rounded corners 10 are provided on both sides of the top front of the keyboard 3, and keyboard fixing buckles 11 are provided on both sides of the device housing 1.

[0035] In the above technical solution, the keyboard fixing buckle 11 is used to fix the keyboard 3 on the front side of the device housing 1. The setting of the metal hinge 4 allows the keyboard 3 to be movable, thereby ensuring the storability of the keyboard 3. When the keyboard needs to be used, the keyboard fixing buckle 11 is released to fix the keyboard 3, and the keyboard 3 is flipped to a vertical state with the device housing 1, and the keyboard 3 can be used to perform related operations.

[0036] This arrangement makes it very convenient to store the keyboard 3, and there is no need to carry a keyboard with you.

[0037] Specifically, a heat dissipation portion 5 is provided on one side of the device housing 1, a power status observation column 6 is provided at the bottom of the heat dissipation portion 5, a USB interface 7 is provided on the side of the power status observation column 6, a switch 8 is provided on the other side of the device housing 1, a network cable interface 9 is provided on the side of the switch 8, and a handle 12 is fixedly installed on the top of the device housing 1.

[0038] In the above technical scheme, the heat dissipation part 5 is used to ensure the basic heat dissipation function of the device casing 1, the power status observation bar 6 is used to observe the power status, the switch 8 is used to turn the device on and off, the network cable interface 9 is used to connect to the network cable, the USB interface 7 is used to connect external devices, and the handle 12 ensures the portability of the device. There are multiple USB interfaces 7 to meet the usage requirements in different situations. By replacing the connecting wires, various types of servos can be tested, and the applicability is strong.

[0039] Such arrangement makes the whole device easy to install, light and easy to operate, light in size and easy to carry.

[0040] Specifically, the keyboard fixing buckle 11 includes a keyboard fixing seat 111 fixedly connected to the device housing 1, a synchronization bar 112 is provided on the front of the keyboard fixing seat 111, a telescopic column 113 is fixedly installed on one side of the back of the synchronization bar 112, and the other end of the telescopic column 113 is fixedly connected to the front wall of the device housing 1, a synchronization column 114 is fixedly installed on the other side of the back of the synchronization bar 112, the other end of the synchronization column 114 passes through the front wall of the keyboard fixing seat 111 and is fixedly connected to a limiting spring 115, a synchronization plate 116 is fixedly installed on the side of the synchronization column 114, the other end of the synchronization plate 116 passes through the inner side wall of the keyboard fixing seat 111 and is fixedly connected to a connecting rod 117, the other end of the connecting rod 117 is hinged to a limiting seat 118, a sliding block 119 is fixedly installed on the back of the limiting seat 118, the other end of the sliding block 119 is slidably connected to the keyboard fixing seat 111, a spring rod 120 is fixedly installed on the side of the limiting seat 118, and the other end of the spring rod 120 is fixedly connected to the limiting plate 121.

[0041] In the above technical solution, when the keyboard 3 needs to be stored, the keyboard 3 is flipped to the front of the synchronization bar 112 and the synchronization bar 112 is pressed. The telescopic column 113 is set to ensure the stability of the synchronization bar 112 during movement. The synchronization column 114 moves synchronously, thereby driving the synchronization plate 116 to move, thereby driving the connecting rod 117 to move. The connecting rod 117 then converts the vertical movement of the synchronization plate 116 into the horizontal movement of the limit seat 118, and the limit plate 121 then moves toward the direction of the keyboard 3 until it moves to the front of the keyboard 3, thereby achieving fixed limit of the keyboard 3.

[0042] The setting of the spring rod 120 allows the limit plate 121 to have a certain adjustable range, so that when the limit plate 121 is released from limiting the keyboard 3, it is only necessary to manually move the limit plate 121 in a direction away from the keyboard 3. After the limit plate 121 is released from limiting the keyboard 3, the keyboard 3 can be flipped to a state perpendicular to the device housing 1. Under the action of the limit spring 115, the synchronization bar 112 will be reset synchronously, thereby facilitating the subsequent continued limiting.

[0043] The sliding block 119 is used to connect the keyboard fixing seat 111 and the limiting seat 118 , so as to ensure the stability of the limiting seat 118 when moving, and also play a certain limiting role on the limiting seat 118 .

[0044] When in use and testing, the loading and unloading switching mechanism first completes a series of mechanical actions such as loading and unloading according to the test requirements. The test system outputs a control signal corresponding to the detection task, and the test product completes the specified action according to the instruction requirements. Each signal is output to the data acquisition component through the electrical interface, and under the control of the computer, data is collected for each action signal, instruction information, and each analog and digital variable from the beginning of work. The data is received by the controller module and the computer, and finally stored and processed in real time by the computer control system, and the processing results are displayed at the same time.

[0045] The keyboard fixing buckle 11 is used to fix the keyboard 3 on the front side of the device housing 1. The setting of the metal hinge 4 allows the keyboard 3 to be movable, thereby ensuring the storability of the keyboard 3. When the keyboard needs to be used, the keyboard fixing buckle 11 is released to fix the keyboard 3, and the keyboard 3 is flipped to a vertical state with the device housing 1, and the keyboard 3 can be used to perform related operations.

[0046] When the keyboard 3 needs to be stored, the keyboard 3 is flipped to the front of the synchronization bar 112 and the synchronization bar 112 is pressed. The telescopic column 113 is set to ensure the stability of the synchronization bar 112 during movement. The synchronization column 114 moves synchronously, thereby driving the synchronization plate 116 to move, thereby driving the connecting rod 117 to move. The connecting rod 117 then converts the vertical movement of the synchronization plate 116 into horizontal movement of the limit seat 118, and the limit plate 121 then moves toward the direction of the keyboard 3 until it moves to the front of the keyboard 3, thereby achieving fixed limit of the keyboard 3.

[0047] The setting of the spring rod 120 allows the limit plate 121 to have a certain adjustable range, so that when the limit plate 121 is released from limiting the keyboard 3, it is only necessary to manually move the limit plate 121 in a direction away from the keyboard 3. After the limit plate 121 is released from limiting the keyboard 3, the keyboard 3 can be flipped to a state perpendicular to the device housing 1. Under the action of the limit spring 115, the synchronization bar 112 will be reset synchronously, thereby facilitating the subsequent continued limiting.

[0048] Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and that the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. A multi-model missile-mounted servo test device, comprising a device housing (1) and a servo test system, characterized in that: The steering gear test system is electrically connected to a loading and unloading device, the loading and unloading device is electrically connected to a loading and unloading control device, the loading and unloading control device is electrically connected to a signal conditioning unit, the signal conditioning unit is electrically connected to a computer control system, the loading and unloading device is also electrically connected to a data acquisition channel, the data acquisition channel is electrically connected to the signal conditioning unit, the steering gear test system is also electrically connected to an electrical interface output, the electrical interface output is electrically connected to the data acquisition channel, the steering gear test system is also electrically connected to an electrical interface input, the electrical interface input is electrically connected to a signal source module, and the steering gear test system is also electrically connected to an isolation protection plug and an electrical interface test device; A display screen (2) is arranged on the front of the device housing (1), a keyboard (3) is arranged on the front of the display screen (2), and a handle (12) is fixedly installed on the top of the device housing (1); The bottom end of the keyboard (3) is hinged with a metal hinge (4), and the other end of the metal hinge (4) is fixedly connected to the device housing (1); Rounded corners (10) are provided on both sides of the top front of the keyboard (3), and keyboard fixing buckles (11) are provided on both sides of the device housing (1); The keyboard fixing buckle (11) comprises a keyboard fixing seat (111) fixedly connected to the device housing (1), a synchronization bar (112) is arranged on the front of the keyboard fixing seat (111), a telescopic column (113) is fixedly installed on one side of the back of the synchronization bar (112), and the other end of the telescopic column (113) is fixedly connected to the front wall of the device housing (1); A synchronization column (114) is fixedly installed on the other side of the back of the synchronization bar (112); the other end of the synchronization column (114) passes through the front wall of the keyboard fixing seat (111) and is fixedly connected to a limit spring (115); and a synchronization plate (116) is fixedly installed on the side of the synchronization column (114); The other end of the synchronization plate (116) passes through the inner wall of the keyboard fixing seat (111) and is fixedly connected to a connecting rod (117), and the other end of the connecting rod (117) is hinged to a limiting seat (118); A sliding block (119) is fixedly mounted on the back of the limiting seat (118), and the other end of the sliding block (119) is slidably connected to the keyboard fixing seat (111). A spring rod (120) is fixedly mounted on the side of the limiting seat (118), and the other end of the spring rod (120) is fixedly connected to the limiting plate (121).

2. The multi-model missile-mounted servo test equipment according to claim 1, characterized in that: A heat dissipation portion (5) is provided on one side of the device housing (1), a power status observation column (6) is provided at the bottom of the heat dissipation portion (5), and a USB interface (7) is provided on the side of the power status observation column (6).

3. The multi-model missile-mounted servo test equipment according to claim 1, characterized in that: A switch (8) is arranged on the other side of the device housing (1), and a network cable interface (9) is arranged on the side of the switch (8).