Ship carrying test system for evaluating signal quality of airborne communication equipment
By employing a structure of casters, pressure strips, and moving components in the ship-mounted testing system, combined with a base plate and suction cups for fixation, the stability problem of the equipment in the turbulent environment of a ship was solved, and efficient signal quality assessment was achieved.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2025-05-09
- Publication Date
- 2026-03-31
AI Technical Summary
Existing ship-mounted testing systems have poor stability, making it difficult to effectively fix airborne communication equipment signal quality assessment devices in turbulent environments.
It adopts a structure of casters, pressure strips and moving components. The pressure strips are driven by elastic telescopic rods to squeeze the wheels to achieve a braking effect. The base plate contacts the ground to increase the support area, and suction cups are used for fixation to improve stability.
This improved the stability of the shipboard testing system and ensured the efficiency and accuracy of signal quality assessment for airborne communication equipment.
Smart Images

Figure CN224068677U_ABST
Abstract
Description
Technical Field
[0001] This utility model relates to the technical field of ship-borne testing systems, and in particular to a ship-borne testing system for evaluating the signal quality of airborne communication equipment. Background Technology
[0002] On ships, it is necessary to use a ship-borne testing system to evaluate the signal quality of airborne communication equipment in order to ensure the safety of ship navigation. The ship-borne testing system also needs to be mobile to cooperate with airborne communication equipment located in different positions.
[0003] Because ships are prone to turbulence when sailing in water, existing ship-mounted testing systems typically rely solely on the braking structure of the casters for fixation, resulting in generally poor stability and reduced efficiency.
[0004] Therefore, it is necessary to propose a ship-borne testing system for evaluating the signal quality of airborne communication equipment to solve the above problems. Utility Model Content
[0005] The purpose of this invention is to provide a ship-borne testing system for evaluating the signal quality of airborne communication equipment, in order to solve the problem that existing ship-borne testing systems typically rely solely on the braking structure of casters for fixation, resulting in generally poor stability and lower efficiency.
[0006] To achieve the above objectives, this utility model provides the following technical solution: a ship-borne testing system for evaluating the signal quality of airborne communication equipment, including a testing platform, wherein universal wheels are provided at the four corners of the bottom of the testing platform;
[0007] The caster wheel includes a frame and a wheel body. The frame is rotatably mounted on the bottom of the testing machine, and the wheel body is rotatably connected to the frame.
[0008] The top of the frame has a through hole that extends through the bottom of the testing machine. An elastic telescopic rod is slidably installed inside the through hole. A pressure strip is fixedly connected to the bottom end of the elastic telescopic rod, and the pressure strip is pressed against the wheel.
[0009] The testing machine is equipped with a base plate underneath, and the base plate and the pressure strip move up and down synchronously using a moving component.
[0010] Preferably, the moving component includes a square frame, a circular groove, a sliding column, and a horizontal plate. The square frame is slidably disposed inside the testing machine platform. The top end of the elastic telescopic rod is rotatably connected to the square frame. The circular groove is opened at the bottom of the testing machine platform. The sliding column is slidably disposed inside the circular groove. The horizontal plate is fixedly connected to the top end of the sliding column. The horizontal plate is fixedly connected to the square frame. The bottom plate is fixedly connected to the bottom end of the sliding column.
[0011] Preferably, a vertical cylinder is fixedly connected to the frame, a round rod is slidably arranged inside the vertical cylinder, a disc is fixedly connected to the bottom end of the round rod, a sliding channel for the pressure strip to pass through is opened on the vertical cylinder, and the pressure strip is fixedly connected to the top of the round rod.
[0012] Preferably, the bottom of the base plate has a groove, and a suction cup is installed inside the groove.
[0013] Preferably, the sliding column has a suction channel inside, and the suction channel is connected to the suction cup.
[0014] The technical effects and advantages of this utility model are as follows:
[0015] 1. This utility model, by setting up structures such as universal wheels, pressure strips and moving components, uses pressure strips to squeeze and limit the wheel body to achieve a braking effect. At the same time, the base plate contacts the ground, expanding the support area, improving the stability of use, ensuring the stability of the ship-mounted testing system, and improving the efficiency of signal quality assessment of airborne communication equipment.
[0016] 2. The four discs are located at the four corners of the test machine base and work together with the base plate to further improve the stability of use. Attached Figure Description
[0017] Figure 1 This is a schematic diagram of the ship-borne testing system for evaluating the signal quality of airborne communication equipment, based on this utility model.
[0018] Figure 2 This is a schematic diagram of the ship-borne testing system for evaluating the signal quality of airborne communication equipment, which is another perspective of the present invention.
[0019] Figure 3 This is a schematic diagram of the circular groove and horizontal plate structure of this utility model.
[0020] Figure 4 This utility model Figure 3 Enlarged schematic diagram of the structure at point A in the middle.
[0021] Figure 5 This utility model Figure 3 Enlarged schematic diagram of the structure at point B.
[0022] Figure 6 This is a schematic diagram of the rectangular frame structure of this utility model.
[0023] In the diagram: 1. Testing machine; 2. Casters; 201. Frame; 202. Wheel; 3. Vertical cylinder; 4. Round rod; 5. Disc; 6. Pressure strip; 7. Through hole; 8. Elastic telescopic rod; 9. Square frame; 10. Round groove; 11. Sliding column; 12. Base plate; 13. Suction cup; 14. Suction channel; 15. Horizontal plate; 16. Bottom groove. Detailed Implementation
[0024] This utility model provides, for example Figures 1-6 The ship-borne testing system shown is used for signal quality assessment of airborne communication equipment. It includes a test stand 1, which includes signal analysis instruments, power supply, etc. It tests VHF communication equipment, aviation satellite communication equipment, etc., mounted on ships, thereby realizing the signal quality assessment of airborne communication equipment. The test stand 1 and its working principle are common existing technologies, and will not be described in detail here.
[0025] To improve the ease of movement of the testing machine 1, casters 2 are provided at the four corners of the bottom of the testing machine 1. The casters 2 include a frame 201 and a wheel 202. The frame 201 is rotatably mounted on the bottom of the testing machine 1, and the wheel 202 is rotatably connected to the frame 201, which facilitates the movement of the testing machine 1.
[0026] Considering the susceptibility of ships to turbulence, a through hole 7 is provided at the top of the frame 201 to improve the stability of the test platform 1. The through hole 7 extends through the bottom of the test platform 1. An elastic telescopic rod 8 is slidably installed inside the through hole 7, and a pressure strip 6 is fixedly connected to the bottom end of the elastic telescopic rod 8. The pressure strip 6 engages with the wheel 202 through a pressing mechanism. When the elastic telescopic rod 8 moves downwards inside the through hole 7, it causes the pressure strip 6 to move downwards synchronously, thus pressing and limiting the wheel 202 to achieve a braking effect.
[0027] A base plate 12 is provided below the test machine 1, and the base plate 12 and the pressure strip 6 move up and down synchronously using a moving component. The moving component includes a square frame 9, a circular groove 10, a sliding column 11, and a horizontal plate 15. The square frame 9 is slidably disposed inside the test machine 1, and the top end of the elastic telescopic rod 8 is rotatably connected to the square frame 9. The circular groove 10 is opened at the bottom of the test machine 1, the sliding column 11 is slidably disposed inside the circular groove 10, the horizontal plate 15 is fixedly connected to the top end of the sliding column 11, the horizontal plate 15 is fixedly connected to the square frame 9, and the base plate 12 is fixedly connected to the bottom end of the sliding column 11.
[0028] Since the top of the elastic telescopic rod 8 is rotatably connected to the frame 9, the pressure strip 6 and the elastic telescopic rod 8 can rotate synchronously with the frame 201.
[0029] In addition, the test machine 1 is equipped with control components, including electric push rods, etc. The telescopic end of the electric push rod is connected to the horizontal plate 15 and is used to drive the frame 9 and the like to move up and down through the horizontal plate 15. The control components are common existing technologies and will not be described in detail here.
[0030] In actual use, when the test platform 1 moves to the designated position, the control components drive the horizontal plate 15 and the square frame 9 to move downward. The horizontal plate 15 drives the base plate 12 to move downward through the sliding column 11. The base plate 12 contacts the ground, expanding the support area and improving the stability of use. At the same time, the square frame 9 drives the elastic telescopic rod 8 to move downward inside the through hole 7, and the pressure strip 6 moves downward synchronously. The pressure strip 6 squeezes and limits the wheel body 202 to achieve the braking effect.
[0031] Furthermore, anti-slip pads or similar materials can be installed on the lower surface of the base plate 12 to achieve an anti-slip effect.
[0032] This utility model incorporates a swivel wheel 2, a pressure strip 6, and a moving component. The pressure strip 6 compresses and limits the wheel body 202, achieving a braking effect. Simultaneously, the base plate 12 contacts the ground, expanding the support area and improving stability during use. This ensures the stability of the ship-mounted testing system and enhances the efficiency of signal quality assessment for airborne communication equipment.
[0033] A vertical cylinder 3 is fixedly connected to the frame 201. A round rod 4 is slidably installed inside the vertical cylinder 3. A disc 5 is fixedly connected to the bottom end of the round rod 4. A sliding channel for a pressure strip 6 to pass through is opened on the vertical cylinder 3. The pressure strip 6 is fixedly connected to the top of the round rod 4. When the pressure strip 6 moves downward, it will drive the round rod 4 to move downward synchronously. The disc 5 contacts the ground. The four discs 5 are distributed at the four corners below the testing machine platform 1 and cooperate with the base plate 12 to further improve the stability of use.
[0034] The bottom of the base plate 12 has a groove 16, and a suction cup 13 is installed inside the groove 16. The sliding column 11 has a suction channel 14 inside, which is connected to the suction cup 13. The control components inside the test machine 1 also include a pump body, a solenoid valve, etc. The pump body is connected to the suction channel 14 and works in conjunction with it to suction the suction cup 13.
[0035] When the base plate 12 comes into contact with the ground, the suction cup 13 adheres to the ship's ground. The suction channel 14 draws suction from the inside of the suction cup 13, thereby adsorbing and fixing the base plate 12 to the ship's ground and maintaining this adsorption state to ensure the stability of the test machine 1.
[0036] If it is necessary to move the test machine 1 to another location on the ship, release the suction cup 13 to fix it, and move the frame 9 and other structures upwards. The disc 5 and the base plate 12 will detach from the ship's ground and move by means of the casters 2.
Claims
1. A shipborne test system for signal quality evaluation of airborne communication equipment, comprising a test bench (1), characterized in that: The universal wheel (2) is arranged at the four corners of the bottom of the test platform (1); The universal wheel (2) comprises a frame body (201) and a wheel body (202), the frame body (201) is rotationally arranged at the bottom of the test platform (1), and the wheel body (202) is rotationally connected to the frame body (201); A through hole (7) is formed in the top of the frame body (201) and penetrates the bottom of the test platform (1), an elastic telescopic rod (8) is slidably arranged in the through hole (7), the bottom end of the elastic telescopic rod (8) is fixedly connected with a pressing strip (6), and the pressing strip (6) is in extrusion fit with the wheel body (202); A bottom plate (12) is arranged below the test platform (1) and moves up and down synchronously with the pressing strip (6) by means of a moving assembly.
2. The shipboard test system for airborne communications equipment signal quality evaluation of claim 1, wherein: The moving assembly comprises a square box (9), a circular groove (10), a slide column (11) and a horizontal plate (15), the square box (9) is slidably arranged in the test platform (1), the top end of the elastic telescopic rod (8) is rotationally connected to the square box (9), the circular groove (10) is formed in the bottom of the test platform (1), the slide column (11) is slidably arranged in the circular groove (10), the horizontal plate (15) is fixedly connected to the top end of the slide column (11), the horizontal plate (15) is fixedly connected to the square box (9), and the bottom plate (12) is fixedly connected to the bottom end of the slide column (11).
3. The shipboard test system for airborne communications equipment signal quality evaluation of claim 1, wherein: The frame body (201) is fixedly connected with a vertical cylinder (3), a circular rod (4) is slidably arranged in the vertical cylinder (3), the bottom end of the circular rod (4) is fixedly connected with a disc (5), a sliding channel is formed in the vertical cylinder (3) and passes through the pressing strip (6), and the pressing strip (6) is fixedly connected to the top of the circular rod (4).
4. The shipboard test system for signal quality evaluation of airborne communication equipment of claim 2, wherein: A bottom groove (16) is formed in the bottom of the bottom plate (12), and a suction disc (13) is mounted in the bottom groove (16).
5. The shipboard test system for airborne communications equipment signal quality evaluation of claim 4, wherein: A suction channel (14) is formed in the slide column (11) and communicates with the suction disc (13).