Radar shell impact resistance testing mechanism

By designing the matching structure of the movable seat and mounting seat and gear motor drive, a comprehensive impact resistance test of the radar shell at different angles is achieved, solving the problem that the impact resistance of the radar shell in the prior art cannot be comprehensively evaluated, and improving the comprehensiveness and accuracy of the test.

CN223122742UActive Publication Date: 2025-07-18QINGDAO ZHIFEI UAV AVIATION TECH DEV CO LTD
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Patent Information

Application Number
CN202421854872.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-08-01
Publication Date
2025-07-18
Estimated Expiration
2034-08-01

AI Technical Summary

Technical Problem

The prior art cannot conduct comprehensive testing of the impact resistance of the radar shell at different angles, and cannot meet the comprehensive safety and reliability evaluation of the radar shell in practical applications.

Method used

A radar housing impact resistance testing mechanism including a frame, a slam assembly and a fixed assembly is designed. Through the matching arc groove and positioning protruding structure of the movable seat and the mounting seat, combined with the gear motor driving the adjustment rack, impact detection at different angles is achieved.

Benefits of technology

A comprehensive impact resistance test of the radar shell at different angles is achieved, which improves the comprehensiveness and accuracy of the test, and ensures the safety and reliability of the radar shell in practical applications.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model relates to the technical field of radar shells, in particular to a radar shell impact resistance testing mechanism which comprises a rack, a downward smashing assembly and a fixed assembly, the fixed assembly comprises a mounting seat and a movable seat, the mounting seat is fixedly mounted at the lower end of the rack, the movable seat is movably connected with the mounting seat, the movable seat is of a semicircular structure, and the lower end of the movable seat is fixedly connected with the rack. An arc groove matched with the movable seat is formed in the top face of the mounting seat, a positioning protrusion is arranged in the middle of the arc groove, a positioning groove matched with the positioning protrusion is formed in the position, close to the positioning protrusion, of the outer arc face of the movable seat, a supporting plate is detachably arranged in the middle of the top face of the movable seat, and an adjusting rack is arranged on the side face of the movable seat. When impact detection at different angles is carried out, the gear motor is started, the gear motor drives the movable base to rotate through the adjusting rack, then the top face of the movable base is changed into an inclined face from a horizontal face, and then the impact detection effect at different angles is achieved.
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Description

Technical Field

[0001] The utility model relates to the technical field of radar housings, in particular to a radar housing impact resistance testing mechanism. Background Art

[0002] The radar housing is a key component in the radar system. Its design aims to protect the internal equipment of the radar from the external environment. This kind of housing is usually made of metal materials such as aluminum or steel to provide the necessary mechanical strength and corrosion resistance. The shape of the radar housing is usually cylindrical or spherical, which helps to reduce the scattering and reflection of radar signals, thereby reducing the impact on radar performance. In military applications, the radar housing may also have a stealth design to reduce the reflection characteristics of radar signals, thereby reducing the possibility of being detected. In summary, the radar housing plays a crucial role in the radar system, not only protecting the internal equipment, but also affecting the performance and concealment performance of the radar system.

[0003] Testing the impact resistance of metal sheets is a key material property assessment, aiming to comprehensively understand the behavior and response of materials when facing sudden and high-intensity external forces (i.e., impacts). This test is extremely important for ensuring the safety and reliability of metal products in practical applications. It not only evaluates the toughness of the material - the ability to resist fracture, especially in the presence of notches or defects, but also examines the quality of the material, revealing possible metallurgical defects such as inclusions, cracks, and non-metallic inclusions through energy absorption capacity and fracture analysis. In addition, the test verifies the effect of heat treatment to ensure that no additional brittleness is introduced, while evaluating the change in brittleness of the material under extreme temperature conditions, which is particularly important for materials operating at low or high temperatures to prevent failure due to increased brittleness caused by temperature.

[0004] Reference can be made to the patent with the publication number CN220729912U. This patent discloses an impact resistance testing device for a housing, including a testing cabinet. A wire releasing mechanism is fixedly connected to the top of the testing cabinet, and one end of the wire releasing mechanism penetrates into the interior of the testing cabinet and is fixedly connected to a counterweight mechanism. A clamping mechanism is slidably connected inside the testing cabinet, and a limiting mechanism is fixedly connected to one side of the testing cabinet. The wire releasing mechanism includes a wire releasing box, which is fixedly connected to the top end of the testing cabinet. A wire releasing roller is rotatably connected inside the wire releasing box. A rope is wound around the outside of the wire releasing roller, and the bottom of the rope penetrates above the testing cabinet. The bottom end of the rope is fixedly connected above the counterweight mechanism. This impact resistance testing device for the housing has advantages such as being able to automatically impact the housing.

[0005] Although this patent has an effect on the impact test of the outer shell, during the test, it can only test the impact resistance of the outer shell when it is placed flat, and it does not have the function of testing the impact resistance of the outer shell at different angles, so it is impossible to conduct a comprehensive test on the outer shell. Therefore, the inventor of the present invention proposes an impact resistance test mechanism for the radar outer shell to solve the above-mentioned technical problems. Summary of the Utility Model

[0006] The purpose of the present utility model is achieved in the following way: An impact resistance test mechanism for a radar outer shell includes a frame, a downward impact component, and a fixing component. The downward impact component is connected to the frame, and the fixing component is installed at the lower end of the frame. The fixing component includes a mounting seat and a movable seat. The mounting seat is fixedly installed at the lower end of the frame, and the movable seat is movably connected to the mounting seat. The movable seat is in a semi-circular structure. An arc groove matching the movable seat is opened on the top surface of the mounting seat. A positioning protrusion is provided in the middle of the arc groove. A positioning groove matching the positioning protrusion is opened at a position on the outer arc surface of the movable seat close to the positioning protrusion. A support plate is detachably arranged in the middle of the top surface of the movable seat. An adjustment rack is provided on the side surface of the movable seat, and a gear motor is meshed and connected to the middle of the lower end of the adjustment rack.

[0007] In the above description, as a further solution, a locking groove is opened in the middle of the inner arc surface of the movable seat, and the locking groove extends through toward the direction of the positioning groove. A threaded hole is provided at a position on the middle of the arc groove close to the positioning groove. A locking member is provided on the locking groove. A fixed pressing block is movably provided in the middle of the locking member. The locking member passes through the locking groove and is connected to the threaded hole. Pressing blocks and locking bolts are provided at both ends of the top surface of the movable seat; the locking member and the pressing blocks are used to fix and lock the movable seat to prevent deviation during the test.

[0008] In the above description, as a further solution, the downward impact component includes a movable plate, a connecting seat, and an impact hammer. Guide columns are provided on both sides of the mounting seat. The lower ends of the guide columns are fixedly connected to the lower end of the frame, and the tops of the guide columns are fixedly connected to the top of the frame through a connecting frame. The movable plate is movably arranged between the guide columns, and both ends of the movable plate are connected to the guide columns. The connecting seat is fixed to the middle of the bottom surface of the movable plate, and the impact hammer is detachably connected to the connecting seat; the connecting seat is used to provide the effect of replacing impact hammers of different materials.

[0009] In the above description, as a further solution, a buffer spring for preventing the impact hammer from damaging the movable seat is sleeved on the lower end of the guide rod, and a matching block is detachably installed at the top of the buffer spring; the detachable matching block is used to correspond to impact hammers of different lengths and sizes.

[0010] In the above description, for a further solution, a tractor is provided in the middle of the top surface of the movable plate. A guide wheel is provided on one side of the upper end of the frame. A driving wheel is provided on one side of the lower end of the frame close to the guide wheel. A driving motor is provided on one side of the driving wheel. The tractor, the guide wheel and the driving wheel are all connected by belts; the driving wheel and the motor drive the movable plate through the belt.

[0011] In the above description, for a further solution, storage rods are installed on both sides of the tractor. The bottom surface of the storage rod is fixedly connected to the top surface of the movable plate. Weights for increasing weight are sleeved on the storage rods; the weights are used to provide weight gain and enhance the impact strength.

[0012] Compared with the prior art, the beneficial effect of the present utility model is: through the design of the movable seat and the mounting seat, an arc groove matching the movable seat is provided on the top surface of the mounting seat. A positioning protrusion is provided in the middle of the arc groove. A positioning groove matching the positioning protrusion is provided at a position on the outer arc surface of the movable seat close to the positioning protrusion. And an adjusting rack is provided on the side surface of the movable seat. A gear motor is meshed and connected to the middle of the lower end of the adjusting rack. When performing impact tests at different angles, by turning on the gear motor, the gear motor drives the movable seat to perform a U-shaped rotation through the adjusting rack, and then changes the top surface of the movable seat from a horizontal plane to an inclined plane, thereby achieving the effect of impact tests at different angles. BRIEF DESCRIPTION OF THE DRAWINGS

[0013] Figure 1 is a three-dimensional structural schematic diagram of a radar housing impact resistance testing mechanism of the present utility model;

[0014] Figure 2 is a three-dimensional structural schematic diagram of another perspective of a radar housing impact resistance testing mechanism of the present utility model;

[0015] Figure 3 is a three-dimensional structural schematic diagram of a fixing component in a radar housing impact resistance testing mechanism of the present utility model;

[0016] Figure 4 is an exploded structural schematic diagram of a fixing component in a radar housing impact resistance testing mechanism of the present utility model;

[0017] Figure 5 is a cross-sectional view of a fixing component in a radar housing impact resistance testing mechanism of the present utility model;

[0018] Figure 6 is a cross-sectional view of a downward impact component in a radar housing impact resistance testing mechanism of the present utility model;

[0019] In the figure: 1-frame, 2-mounting seat, 3-movable seat, 4-arc groove, 5-positioning protrusion, 6-positioning groove;

[0020] 7 - Support plate, 8 - Adjusting rack, 9 - Gear motor, 10 - Locking groove, 11 - Threaded hole, 12 - Locking piece;

[0021] 13 - Fixed pressing block, 14 - Lower pressing block, 15 - Locking bolt, 16 - Movable plate, 17 - Connecting seat;

[0022] 18 - Impact hammer, 19 - Guide post, 20 - Connecting frame, 21 - Buffer spring, 22 - Dispensing block;

[0023] 23 - Tractor, 24 - Guide wheel, 25 - Driving wheel, 26 - Driving motor, 27 - Belt, 28 - Object placing rod; 29 - Weight. Specific embodiments

[0024] The present invention will be further described in detail below in conjunction with the accompanying drawings and specific embodiments.

[0025] In this embodiment, please refer to Figures 1-6 , a test mechanism for the impact resistance of a radar housing in its specific implementation, includes a frame 1, a downward impact component, and a fixing component. The downward impact component is connected to the frame 1, and the fixing component is installed at the lower end of the frame 1. The fixing component includes a mounting seat 2 and a movable seat 3. The mounting seat 2 is fixedly installed at the lower end of the frame 1, and the movable seat 3 is movably connected to the mounting seat 2. The movable seat 3 is in a semi - circular structure. The top surface of the mounting seat 2 is provided with an arc groove 4 matching the movable seat 3. A positioning protrusion 5 is provided in the middle of the arc groove 4. A positioning groove 6 matching the positioning protrusion 5 is provided at a position on the outer arc surface of the movable seat 3 close to the positioning protrusion 5. A support plate 7 is detachably arranged in the middle of the top surface of the movable seat 3. An adjusting rack 8 is arranged on the side surface of the movable seat 3. The middle of the lower end of the adjusting rack 8 is meshed and connected with a gear motor 9.

[0026] A locking groove 10 is provided in the middle of the inner arc surface of the movable seat 3, and the locking groove 10 extends through towards the direction of the positioning groove 6. A threaded hole 11 is provided at a position on the middle of the arc groove 4 close to the positioning groove 6. A locking piece 12 is provided on the locking groove 10. A fixed pressing block 13 is movably arranged in the middle of the locking piece 12. The locking piece 12 passes through the locking groove 10 and is connected to the threaded hole 11. Lower pressing blocks 14 and locking bolts 15 are arranged at both ends of the top surface of the movable seat 3.

[0027] The downward impact component includes a movable plate 16, a connecting seat 17, and an impact hammer 18. Guide posts 199 are provided on both sides of the mounting seat 2. The lower ends of the guide posts 199 are fixedly connected to the lower end of the frame 1, and the tops of the guide posts 199 are fixedly connected to the top of the frame 1 through a connecting frame 20. The movable plate 16 is movably arranged between the guide posts 199, and both ends of the movable plate 16 are connected to the guide posts 199. The connecting seat 17 is fixed in the middle of the bottom surface of the movable plate 16. The impact hammer 18 is detachably connected to the connecting seat 17.

[0028] A buffer spring 21 for preventing the impact hammer 18 from damaging the movable seat 3 is sleeved on the lower end of the guide rod, and a dispensing block 22 is detachably installed on the top of the buffer spring 21.

[0029] A tractor 23 is provided in the middle of the top surface of the movable plate 16. A guide wheel 24 is provided on one side of the upper end of the frame 1. A driving wheel 25 is provided on one side of the lower end of the frame 1 close to the guide wheel 24. A driving motor 26 is provided on one side of the driving wheel 25. The tractor 23, the guide wheel 24 and the driving wheel 25 are all connected by a belt 27.

[0030] Object placing rods 28 are installed on both sides of the tractor 23. The bottom surface of the object placing rod 28 is fixedly connected to the top surface of the movable plate 16. Weights 29 for increasing weight are sleeved on the object placing rods 28.

[0031] The working process of the present utility model: After placing the sample with a metal shell on the support plate 7, place the pressing block 14 on the sample, then rotate the locking bolt 15 to press down the pressing block 14 to achieve the effect of fixing the sample. After confirmation of fixation, check whether the fixing pressing block 13 and the locking member 12 are tightened to ensure that the movable seat 3 does not shift. After the inspection is completed, turn on the driving motor 26. The driving motor 26 drives the movable plate 16 to slowly move downward toward the sample through the belt 27. When it is confirmed that the impact hammer 18 contacts the sample, place the dispensing block 22 at the position between the movable plate 16 and the buffer spring 21. After placing, turn on the driving motor 26 again to pull the movable plate 16 to move upward. After moving to the top, the driving motor 26 stops applying force, and the movable plate 16 naturally falls due to gravity to conduct an impact test on the sample.

[0032] To make the objectives, technical solutions and advantages of the embodiments of the present utility model clearer, the technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are some, but not all, of the embodiments of the present utility model. All other embodiments obtained by those skilled in the art based on the embodiments of the present utility model without creative efforts shall fall within the protection scope of the present utility model.

[0033] In addition, in the description of the embodiments of the present utility model, unless otherwise clearly defined and limited, the terms "installation", "connection", and "coupling" should be understood in a broad sense. For example, it can be a fixed connection, a detachable connection, or an integral connection; it can be a mechanical connection or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium, and it can be the communication inside two components. For those skilled in the art, the specific meanings of the above terms in the present utility model can be understood according to specific situations. In the description of the present utility model, it should be noted that the orientation or positional relationship indicated by the terms "center", "upper", "lower", "left", "right", "vertical", "horizontal", "inner", "outer", etc. is based on the orientation or positional relationship shown in the drawings, and is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or component referred to must have a specific orientation, be constructed and operated in a specific orientation, and thus should not be construed as a limitation to the present utility model. In addition, the terms "first", "second", and "third" are only used for descriptive purposes and should not be construed as indicating or implying relative importance.

[0034] Finally, it should be noted that the above embodiments are only specific implementation manners of the present utility model, used to illustrate the technical solutions of the present utility model, rather than limiting it. The protection scope of the present utility model is not limited thereto. Although the present utility model has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that any person skilled in the art within the technical scope disclosed by the present utility model can still modify the technical solutions recorded in the foregoing embodiments, or can easily think of changes, or make equivalent replacements for some of the technical features; and these modifications, changes or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present utility model, and should all be covered within the protection scope of the present utility model. Therefore, the protection scope of the present utility model should be subject to the protection scope of the claims.

Claims

1. A radar housing impact resistance testing mechanism, comprising a frame, a downward impact component and a fixing component. The downward impact component is connected to the frame, and the fixing component is installed at the lower end of the frame, characterized in that: The fixed component includes a mounting base and a movable seat. The mounting base is fixedly installed at the lower end of the frame, and the movable seat is movably connected to the mounting base. The movable seat is in a semi-circular structure. An arc groove matching the movable seat is provided on the top surface of the mounting base. A positioning protrusion is provided in the middle of the arc groove. A positioning groove matching the positioning protrusion is provided at a position on the outer arc surface of the movable seat close to the positioning protrusion. A support plate is detachably arranged in the middle of the top surface of the movable seat. An adjusting rack is provided on the side surface of the movable seat, and a gear motor is meshed and connected to the middle of the lower end of the adjusting rack.

2. The impact resistance test mechanism for a radar housing according to claim 1, wherein: A locking groove is provided in the middle of the inner arc surface of the movable seat, and the locking groove extends through towards the direction of the positioning groove. A threaded hole is provided at a position in the middle of the arc groove close to the positioning groove. A locking member is provided on the locking groove, and a fixed pressing block is movably provided in the middle of the locking member. The locking member passes through the locking groove and is connected to the threaded hole. Pressing blocks and locking bolts are provided at both ends of the top surface of the movable seat.

3. The impact resistance test mechanism for a radar housing according to claim 1, characterized in that: The downward impact component includes a movable plate, a connecting seat and a hammer. Guide columns are provided on both sides of the mounting base. The lower ends of the guide columns are fixedly connected to the lower end of the frame, and the tops of the guide columns are fixedly connected to the top of the frame through a connecting frame. The movable plate is movably arranged between the guide columns, and both ends of the movable plate are connected to the guide columns. The connecting seat is fixed in the middle of the bottom surface of the movable plate, and the hammer is detachably connected to the connecting seat.

4. A radar housing impact resistance testing mechanism according to claim 3, characterized in that: A buffer spring for preventing the hammer from damaging the movable seat is sleeved on the lower end of the guide column, and a dispensing block is detachably installed at the top of the buffer spring.

5. The impact resistance testing mechanism for a radar housing according to claim 3, characterized in that: A tractor is provided in the middle of the top surface of the movable plate. A guide wheel is provided on one side of the upper end of the frame, and a driving wheel is provided on the side of the lower end of the frame close to the guide wheel. A driving motor is provided on one side of the driving wheel. The tractor, the guide wheel and the driving wheel are all connected by belts.

6. The impact resistance test mechanism for a radar housing according to claim 5, characterized in that: Object placing rods are installed on both sides of the tractor, the bottom surfaces of the object placing rods are fixedly connected to the top surface of the movable plate, and weights for increasing weight are sleeved on the object placing rods.

Citation Information

Patent Citations

  • Shock resistance testing device for shell

    CN220729912U