Radar unit transport shock mitigation apparatus and method
By designing a shock-absorbing device for the overall transportation of radar, and utilizing frame components and shock absorbers to achieve flexible connection of the radar, the shock absorption problem during the transportation of large fixed radars was solved, reducing transportation costs and improving the shock absorption effect.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- XTR SOLUTIONS
- Filing Date
- 2023-12-26
- Publication Date
- 2026-07-03
Smart Images

Figure CN117755646B_ABST
Abstract
Description
Technical Field
[0001] This invention relates to the field of radar transport equipment, and in particular to a radar overall transport shock absorption device and shock absorption method. Background Technology
[0002] In the existing civilian radar service sector, large-scale fixed radar systems are transported over long distances and in poor road conditions, thus requiring effective shock absorption measures.
[0003] In the market, precision instruments and radars are usually transported using special vehicles with specialized air suspension systems, which result in higher transportation costs. In addition, since the radar itself is an irregular shape, including a radar base, a radar antenna head, and a radar turntable connecting the radar base and the radar antenna head, the irregular shape of the radar is not convenient for direct transport using special vehicles, and additional transport supports that are compatible with the radar are still required. Summary of the Invention
[0004] This invention aims to at least solve one of the technical problems existing in the prior art. To this end, this invention proposes a radar overall transportation shock absorption device, which can effectively reduce vibration during the overall transportation of radar, achieving shock-absorbing transportation without the need for special vehicles, thus saving transportation costs.
[0005] The present invention also proposes a vibration reduction method using the above-mentioned radar integrated transportation vibration reduction device.
[0006] According to a first aspect of the present invention, a radar overall transport shock absorption device includes: a frame assembly including a bottom frame and two side frames, the bottom frame being horizontally arranged, and the two side frames being vertically arranged and parallel to each other on the left and right sides of the bottom frame; a chassis being horizontally arranged on the bottom frame, the chassis being used to support a radar base and being detachably connected to the radar base; a first connecting rod being arranged in a left-right direction between the two side frames, the middle portion of the first connecting rod being detachably connected to the radar antenna head; a second connecting rod being arranged in a left-right direction between the two side frames, the middle portion of the second connecting rod being detachably connected to the radar turntable; and shock absorbers, the chassis and the bottom frame being connected by a plurality of shock absorbers, the shock absorbers being provided at both ends of the first connecting rod and both ends of the second connecting rod, and the first connecting rod and the second connecting rod being connected to the side frames through the shock absorbers.
[0007] The invention offers at least the following advantages: In the shock-absorbing device of this invention, multiple shock absorbers are provided between the chassis supporting the radar base and the bottom frame. Both ends of the first connecting rod supporting the radar antenna head are connected to the two side frames via shock absorbers, and both ends of the second connecting rod supporting the radar turntable are also connected to the two side frames via shock absorbers. The radar overall transportation shock-absorbing device of this invention can also function as a transportation support. By combining it with ordinary transport vehicles, radar transportation can be achieved without the need for special transport vehicles, greatly reducing transportation costs. Furthermore, by setting shock absorbers, the bottom and top of the radar can be elastically connected to the frame components, significantly improving the shock absorption effect compared to traditional rigid connections.
[0008] According to some embodiments of the present invention, one end of the shock absorber located on the first connecting rod and the second connecting rod is connected to the end of the first connecting rod or the second connecting rod, and the other end is provided with a connector. The side frame is provided with a guide post extending in a vertical direction, and the guide post is provided with a threaded hole. The connector is provided with a waist-shaped groove extending in a vertical direction, and a fastening bolt is inserted in the waist-shaped groove. The fastening bolt can slide along the waist-shaped groove and can be threadedly connected to the threaded hole.
[0009] According to some embodiments of the present invention, a support rod is also included, the support rod comprising a bottom connecting seat, a support rod body and a top connecting seat, the bottom connecting seat being fixedly connected to the chassis, the lower end of the support rod body being hinged to the bottom connecting seat, the upper end of the support rod body being hinged to the top connecting seat, and the top connecting seat being detachably connected to the radar antenna head.
[0010] According to some embodiments of the present invention, six shock absorbers are provided between the chassis and the bottom frame, and the six shock absorbers are arranged in an array in the horizontal plane.
[0011] According to some embodiments of the present invention, the bottom frame is square, and uprights are vertically arranged at the four corners of the bottom frame. A connecting joint is provided at the top of the uprights, and the bottom of the side frame is detachably connected to the uprights through the connecting joints.
[0012] According to some embodiments of the present invention, the connecting joint includes two end plates arranged in a front-rear direction. Each end plate has a shaft hole in the front-rear direction. The bottom of the side frame has a hinge shaft extending in the front-rear direction. The front and rear ends of the hinge shaft pass through the shaft holes on the two end plates and are hinged to the shaft holes. A first connecting plate is provided at the lower part between the two end plates, and a second connecting plate is provided at the upper part between the two end plates. The first connecting plate and the second connecting plate are located on opposite sides of the end plates in the left-right direction. Fasteners are provided on both the first connecting plate and the second connecting plate. The fasteners on the first connecting plate can be connected to the upright, and the fasteners on the second connecting plate can be connected to the bottom of the side frame.
[0013] According to some embodiments of the present invention, the bottom end of the bottom frame is provided with a plurality of support columns, and the bottom surface of the support columns is provided with a rubber pad.
[0014] According to some embodiments of the present invention, the shock absorber includes an elastic rope, two retainers and two fixing plates. The two retainers are arranged in parallel. The elastic rope alternately passes through the two retainers. The elastic rope extends in a spiral trajectory along the length direction of the retainers. The retainers on the shock absorber between the chassis and the bottom frame extend in the left-right direction. The retainers on the shock absorbers at both ends of the first connecting rod and the two ends of the second connecting rod extend in the front-back direction.
[0015] According to a second aspect of the present invention, a vibration reduction method using a radar overall transport vibration reduction device according to a first aspect embodiment includes the following steps: Step S1, setting the bottom frame horizontally, connecting multiple vibration dampers to the bottom frame, and then setting the chassis horizontally and connecting it to the multiple vibration dampers; Step S2, hoisting the radar assembly onto the chassis and connecting the radar base to the chassis; Step S3, installing two side frames on the left and right sides of the bottom frame respectively; Step S4, preparing multiple vibration dampers, connecting the multiple vibration dampers to both ends of a first connecting rod and both ends of a second connecting rod, then connecting the first connecting rod to the radar antenna head, connecting the second connecting rod to the radar turntable, and finally connecting each vibration damper to the corresponding side frame.
[0016] The invention offers at least the following advantages: In the vibration reduction method of this invention, the bottom-up installation method prevents interference with the upper side frame, first connecting rod, and second connecting rod when fixing the radar. Furthermore, by installing multiple shock absorbers under the chassis and at both ends of the first and second connecting rods, the radar can be effectively vibration-damped. This method eliminates the need for air suspension systems used in special vehicles, making installation convenient, quick, and highly effective.
[0017] According to some embodiments of the present invention, after step S2, the following steps are further included: preparing a support rod, the support rod including a support rod body and a bottom connecting seat and a top connecting seat respectively hinged to both ends of the support rod body, fixing the bottom connecting seat to the chassis, and connecting the top connecting seat to the radar antenna head.
[0018] Additional aspects and advantages of the invention will be set forth in part in the description which follows, and in part will be obvious from the description, or may be learned by practice of the invention. Attached Figure Description
[0019] The present invention will be further described below with reference to the accompanying drawings and embodiments, wherein:
[0020] Figure 1 This is a schematic diagram of the structure of an embodiment of the present invention;
[0021] Figure 2 for Figure 1 A schematic diagram of the local structure at point A in the middle;
[0022] Figure 3 for Figure 1 A schematic diagram of the local structure at point B;
[0023] Figure 4 This is a schematic diagram of the bottom frame structure in an embodiment of the present invention;
[0024] Figure 5 This is a schematic diagram of the chassis structure in an embodiment of the present invention;
[0025] Figure 6 This is a schematic diagram of the connecting joint structure in an embodiment of the present invention;
[0026] Figure 7 This is a schematic diagram of the support rod in an embodiment of the present invention;
[0027] Figure 8 This is a schematic diagram of the shock absorber in an embodiment of the present invention.
[0028] Icon labels:
[0029] Frame assembly 100, bottom frame 110, upright 111, support column 112, rubber pad 113, side frame 120, guide column 121, hinge shaft 122, crossbar 130;
[0030] Chassis 200;
[0031] Shock absorber 300, elastic rope 310, cage 320, fixing plate 330;
[0032] First connecting rod 400;
[0033] Second connecting rod 500;
[0034] Connector 600, slotted groove 610, fastening bolt 620;
[0035] Support rod 700, bottom connecting seat 710, support rod body 720, top connecting seat 730;
[0036] Connecting joint 800, end plate 810, shaft hole 811, first connecting plate 820, second connecting plate 830, fastener 840;
[0037] Radar 900, radar base 910, radar antenna head 920, radar turntable 930, radar boom 940. Detailed Implementation
[0038] Embodiments of the present invention are described in detail below. Examples of these embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The embodiments described below with reference to the accompanying drawings are exemplary and are only used to explain the present invention, and should not be construed as limiting the present invention.
[0039] In the description of this invention, it should be understood that the orientation descriptions, such as up, down, front, back, left, right, etc., are based on the orientation or positional relationship shown in the accompanying drawings. They are only for the convenience of describing this invention and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation. Therefore, they should not be construed as limiting this invention.
[0040] In the description of this invention, the use of "first" and "second" is for the purpose of distinguishing technical features only, and should not be construed as indicating or implying relative importance or implicitly indicating the number of technical features indicated or the order of the technical features indicated.
[0041] In the description of this invention, unless otherwise explicitly defined, terms such as "set up," "install," and "connect" should be interpreted broadly, and those skilled in the art can reasonably determine the specific meaning of the above terms in this invention in conjunction with the specific content of the technical solution.
[0042] like Figures 1 to 8 As shown, the present invention discloses a radar overall transportation shock absorption device, including a frame assembly 100, a chassis 200, a first connecting rod 400, a second connecting rod 500, and a shock absorber 300.
[0043] The frame assembly 100 includes a bottom frame 110 and two side frames 120. The bottom frame 110 is horizontally positioned, and the two side frames 120 are vertically positioned and parallel to each other on the left and right sides of the bottom frame 110. A chassis 200 is horizontally positioned on the bottom frame 110 and is used to support the radar base 910 and is detachably connected to the radar base 910. A first connecting rod 400 is positioned between the two side frames 120 in a left-right direction, with the middle of the first connecting rod 400... The second connecting rod 500 is detachably connected to the radar antenna head 920 and is located between the two side frames 120 in the left-right direction. The middle part of the second connecting rod 500 is detachably connected to the radar turntable 930. The chassis 200 and the bottom frame 110 are connected by multiple shock absorbers 300. Both ends of the first connecting rod 400 and both ends of the second connecting rod 500 are provided with shock absorbers 300. Both the first connecting rod 400 and the second connecting rod 500 are connected to the side frame 120 through shock absorbers 300.
[0044] It is understood that in the shock absorption device of the present invention, multiple shock absorbers 300 are provided between the chassis 200 supporting the radar base 910 and the bottom frame 110. The two ends of the first connecting rod 400 supporting the radar antenna head 920 are connected to the two side frames 120 via shock absorbers 300, and the two ends of the second connecting rod 500 supporting the radar turntable 930 are also connected to the two side frames 120 via shock absorbers 300. The radar overall transportation shock absorption device of the present invention can also function as a transportation support. By combining it with ordinary transport vehicles, the radar 900 can be transported without the need for special transport vehicles, greatly reducing transportation costs. Furthermore, by setting shock absorbers 300, the bottom and top of the radar 900 can be elastically connected to the frame assembly 100, which significantly improves the shock absorption effect compared to traditional rigid connections.
[0045] Reference Figure 1 and Figure 2In an embodiment of the present invention, one end of the shock absorber 300 located on the first connecting rod 400 and the second connecting rod 500 is connected to the end of the first connecting rod 400 or the second connecting rod 500, and the other end is provided with a connector 600. A guide post 121 extending vertically is provided on the side frame 120, and a threaded hole is provided on the guide post 121. A waist-shaped groove 610 extending vertically is provided on the connector 600, and a fastening bolt 620 passes through the waist-shaped groove 610. The fastening bolt 620 can slide along the waist-shaped groove 610 and can be threadedly connected to the threaded hole. By providing the guide post 121, the position of the connector 600 in the vertical direction can be adjusted, thereby allowing the positions of the first connecting rod 400 and the second connecting rod 500 in the vertical direction to be adjusted respectively, thus enabling the device to adapt to radars 900 of more sizes and specifications. Furthermore, multiple guide posts 121 can be provided on the side frame 120, and the multiple guide posts 121 are arranged in the front-back direction. The connector 600 can be installed on the guide posts 121 at different positions so that the positions of the first connecting rod 400 and the second connecting rod 500 in the front-back direction can also be adjusted, which can further expand the applicability of this equipment.
[0046] Reference Figure 1 and Figure 7 In embodiments of the present invention, a support rod 700 may also be included. The support rod 700 includes a bottom connecting seat 710, a support rod body 720, and a top connecting seat 730. The bottom connecting seat 710 is fixedly connected to the chassis 200. The lower end of the support rod body 720 is hinged to the bottom connecting seat 710, and the upper end of the support rod body 720 is hinged to the top connecting seat 730. The top connecting seat 730 is detachably connected to the radar antenna head 920. Specifically, after the radar base 910 is fixed to the chassis 200, the support rod 700 can be erected between the chassis 200 and the radar antenna head 920 to support the radar antenna head 920. Further, two support rods 700 may be provided and located on the left and right sides of the chassis 200, respectively.
[0047] like Figure 1 As shown, in this embodiment of the invention, six shock absorbers 300 are provided between the chassis 200 and the bottom frame 110. The six shock absorbers 300 are arranged in an array in the horizontal plane, with two shock absorbers 300 located at the left and right ends of the front of the chassis 200, two more shock absorbers 300 located at the left and right ends of the middle of the chassis 200, and the remaining two shock absorbers 300 located at the left and right ends of the rear of the chassis 200.
[0048] In this embodiment of the invention, reference is made to Figure 1 and Figure 4The bottom frame 110 is square, with uprights 111 vertically installed at each of its four corners. A connecting joint 800 is located at the top of each upright 111. The bottom of the side frame 120 is detachably connected to the uprights 111 via the connecting joints 800. By using the connecting joints 800, the uprights 111 and the side frame 120 become a detachable structure. Before installing the side frame 120, the radar 900 can be hoisted onto the chassis 200 and secured, and then the side frame 120 and uprights 111 can be installed. This improves the hoisting efficiency of the radar 900 and prevents collisions between the radar 900 and the side frame 120 during hoisting.
[0049] It is understandable that, such as Figure 3 and Figure 6 As shown, the connecting joint 800 in this embodiment of the invention includes two end plates 810 arranged in the front-back direction. Each end plate 810 has a shaft hole 811 passing through it in the front-back direction. The bottom of the side frame 120 has a hinge shaft 122 extending in the front-back direction. The front and rear ends of the hinge shaft 122 pass through the shaft holes 811 on the two end plates 810 respectively and are hinged to the shaft holes 811. A first connecting plate 820 connecting the two end plates 810 is provided at the lower part between them, and a second connecting plate 830 connecting the two end plates 810 is provided at the upper part between them. The first connecting plate 820 and the second connecting plate 830 are located on opposite sides of the end plates 810 in the left-right direction. Fasteners 840 are provided on both the first connecting plate 820 and the second connecting plate 830. The fasteners 840 on the first connecting plate 820 can be connected to the upright 111, and the fasteners 840 on the second connecting plate 830 can be connected to the bottom of the side frame 120. It should be noted that the connecting joints 800 on the four uprights 111 can all be rotated outwards around the hinge axis 122 to a horizontal state, or rotated in the opposite direction to a vertical state. During installation, the shaft hole 811 on the connecting joint 800 can be engaged with the hinge axis 122, then the first connecting plate 820 can be connected to the uprights 111 on the bottom frame 110, and finally the second connecting plate 830 can be connected to the bottom of the side frame 120. This achieves an indirect connection between the bottom frame 110 and the side frame 120, and fixes the relative position and angle between the bottom frame 110 and the side frame 120.
[0050] like Figure 1 As shown, in this embodiment of the invention, the bottom end of the bottom frame 110 is provided with multiple support columns 112, and the bottom surface of the support columns 112 is provided with rubber pads 113. The rubber pads 113 can play a shock absorption role between the frame assembly 100 and the transport vehicle.
[0051] like Figure 8As shown, the shock absorber 300 in this embodiment of the invention includes an elastic rope 310, two retainers 320, and two fixing plates 330. The two retainers 320 are arranged in parallel, and the elastic rope 310 alternately passes through the two retainers 320. The elastic rope 310 can be a rope with a certain strength and elasticity, including but not limited to steel wire rope. The elastic rope 310 extends in a spiral trajectory along the length direction of the retainers 320. The retainers 320 on the shock absorber 300 between the chassis 200 and the bottom frame 110 extend in the left-right direction. This part of the shock absorber 300 mainly bears the vertical vibration force, and can also bear a certain amount of vibration force in the left-right and front-back directions. The retainers 320 on the shock absorbers 300 at both ends of the first connecting rod 400 and the second connecting rod 500 extend in the front-back direction. This part of the shock absorber 300 mainly bears the left-right vibration force, and can also bear a certain amount of vibration force in the front-back and up-down directions.
[0052] like Figures 1 to 8 As shown, the present invention also discloses a vibration reduction method, using a radar integrated transport vibration reduction device from the foregoing embodiments of the present invention, comprising the following steps:
[0053] Step S1: Horizontally set the bottom frame 110, connect multiple shock absorbers 300 to the bottom frame 110, and then horizontally set the chassis 200 and connect it to the multiple shock absorbers 300.
[0054] Step S2: Hoist the radar 900 onto the chassis 200 and connect the radar base 910 to the chassis 200.
[0055] Step S3: Install the two side frames 120 on the left and right sides of the bottom frame 110 respectively;
[0056] Step S4: Prepare multiple shock absorbers 300, and connect the multiple shock absorbers 300 to both ends of the first connecting rod 400 and the two ends of the second connecting rod 500 respectively. Then connect the first connecting rod 400 to the radar antenna head 920, connect the second connecting rod 500 to the radar turntable 930, and finally connect each shock absorber 300 to the corresponding side frame 120.
[0057] It is understood that in the vibration reduction method of the present invention, the bottom-up installation method ensures that the fixed radar 900 will not interfere with the upper side frame 120, the first connecting rod 400, and the second connecting rod 500. Furthermore, by installing multiple shock absorbers 300 under the chassis 200, and by installing shock absorbers 300 at both ends of the first connecting rod 400 and the second connecting rod 500, the radar 900 can be effectively vibration-damped. The vibration reduction method of the present invention does not require the vibration reduction method implemented through an air suspension system in special vehicles; it is convenient and quick to install, and the vibration reduction effect is significant.
[0058] In this embodiment of the invention, after step S2, the following steps are further included: preparing a support rod 700, the support rod 700 including a support rod body 720 and a bottom connecting seat 710 and a top connecting seat 730 respectively hinged to both ends of the support rod body 720; fixing the bottom connecting seat 710 to the chassis 200; and connecting the top connecting seat 730 to the radar antenna head 920. The support rod 700 can support the radar antenna head 920. Further, two support rods 700 can be provided and located on the left and right sides of the chassis 200 respectively.
[0059] The vibration reduction method in this embodiment of the invention specifically includes the following steps:
[0060] Step S1: Fix the rubber pad 113 to the bottom surface of the support column 112, set the bottom frame 110 horizontally, connect the multiple shock absorbers 300 to the bottom frame 110, and then set the chassis 200 horizontally and connect it to the multiple shock absorbers 300.
[0061] Step S2: Use radar boom 940 to hoist radar 900 onto chassis 200, fix radar base 910 to chassis 200, and then adjust radar antenna head 920 to a horizontal position.
[0062] Step S2.1: Prepare the support rod 700. The support rod 700 includes a support rod body 720 and a bottom connecting seat 710 and a top connecting seat 730 respectively hinged to both ends of the support rod body 720. After adjusting the support rod body 720 to a suitable length, fix the bottom connecting seat 710 to the chassis 200 and fix the top connecting seat 730 to the radar antenna head 920.
[0063] Step S3: Install the four connecting joints 800 onto the uprights 111 at the four corners of the bottom frame 110, and fix the two side frames 120 to the corresponding connecting joints 800, so that the two side frames 120 are installed on the left and right sides of the bottom frame 110 respectively.
[0064] Step S4: Prepare multiple shock absorbers 300, and connect the multiple shock absorbers 300 to both ends of the first connecting rod 400 and the two ends of the second connecting rod 500 respectively. Then, fix the first connecting rod 400 to the radar antenna head 920, fix the second connecting rod 500 to the radar turntable 930, and finally fix each shock absorber 300 to the corresponding side frame 120.
[0065] Step S5: Prepare two crossbars 130, set the crossbars 130 in the left and right direction, and fix the two ends of the crossbars 130 to the two side frames 120 respectively. One crossbar 130 is located at the front end of the side frame 120, and the other crossbar 130 is located at the rear end of the side frame 120.
[0066] The technical features of the above embodiments can be combined in any way. For the sake of brevity, not all possible combinations of the technical features in the above embodiments are described. However, as long as there is no contradiction in the combination of these technical features, they should be considered to be within the scope of this specification.
[0067] Of course, the present invention is not limited to the above-described embodiments. Those skilled in the art can make equivalent modifications or substitutions without departing from the spirit of the present invention. All such equivalent modifications or substitutions are included within the scope defined by the claims of this application.
Claims
1. A radar unit transport shock absorbing apparatus, characterized by, include: A frame assembly includes a bottom frame and two side frames. The bottom frame is horizontally positioned, and the two side frames are vertically positioned and parallel to each other on the left and right sides of the bottom frame. A chassis is horizontally mounted on the bottom frame, and the chassis is used to support the radar base and is detachably connected to the radar base. The first connecting rod is disposed between the two side frames in the left-right direction, and the middle part of the first connecting rod is detachably connected to the radar antenna head. The second connecting rod is disposed between the two side frames in the left-right direction, and the middle part of the second connecting rod is detachably connected to the radar turntable. Shock absorbers are provided at both ends of the first connecting rod and both ends of the second connecting rod, and the first connecting rod and the second connecting rod are connected to the side frame through the shock absorbers. The support rod includes a bottom connecting seat, a support rod body, and a top connecting seat. The bottom connecting seat is fixedly connected to the chassis. The lower end of the support rod body is hinged to the bottom connecting seat, and the upper end of the support rod body is hinged to the top connecting seat. The top connecting seat is detachably connected to the radar antenna head.
2. The radar overall transportation shock absorption device according to claim 1, characterized in that, One end of the shock absorber located on the first connecting rod and the second connecting rod is connected to the end of the first connecting rod or the second connecting rod, and the other end is provided with a connector. The side frame is provided with a guide post extending in the vertical direction, and the guide post is provided with a threaded hole. The connector is provided with a waist-shaped groove extending in the vertical direction, and a fastening bolt is inserted in the waist-shaped groove. The fastening bolt can slide along the waist-shaped groove and can be threadedly connected to the threaded hole.
3. The radar overall transportation shock absorption device according to claim 1, characterized in that, Six shock absorbers are provided between the chassis and the bottom frame, and the six shock absorbers are arranged in an array in the horizontal plane.
4. The radar overall transportation shock absorption device according to claim 1, characterized in that, The bottom frame is square, and each of the four corners of the bottom frame is vertically supported by a pole. The top of each pole is provided with a connecting joint, and the bottom of the side frame is detachably connected to the pole through the connecting joint.
5. A radar overall transportation shock absorption device according to claim 4, characterized in that, The connecting joint includes two end plates arranged in a front-to-back direction. Each end plate has a shaft hole in the front-to-back direction. The bottom of the side frame has a hinge shaft extending in the front-to-back direction. The front and rear ends of the hinge shaft pass through the shaft holes on the two end plates and are hinged to the shaft holes. A first connecting plate is provided at the lower part between the two end plates, and a second connecting plate is provided at the upper part between the two end plates. The first connecting plate and the second connecting plate are located on opposite sides of the end plates in the left-to-right direction. Fasteners are provided on both the first connecting plate and the second connecting plate. The fasteners on the first connecting plate can be connected to the upright, and the fasteners on the second connecting plate can be connected to the bottom of the side frame.
6. The radar overall transportation shock absorption device according to claim 1, characterized in that, The bottom frame has multiple support columns at its bottom end, and the bottom surface of each support column is provided with a rubber pad.
7. The radar overall transportation shock absorption device according to claim 1, characterized in that, The shock absorber includes an elastic rope, two retainers, and two fixing plates. The two retainers are arranged in parallel, and the elastic rope alternately passes through the two retainers. The elastic rope extends in a spiral trajectory along the length direction of the retainers. The retainers on the shock absorber between the chassis and the bottom frame extend in the left-right direction, and the retainers on the shock absorbers at both ends of the first connecting rod and the two ends of the second connecting rod extend in the front-back direction.
8. A vibration reduction method, characterized in that, Using a radar integral transport shock absorption device as described in any one of claims 1 to 7 includes the following steps: Step S1: Horizontally set the bottom frame, connect multiple shock absorbers to the bottom frame, and then horizontally set the chassis and connect it to the multiple shock absorbers. Step S2: Hoist the entire radar onto the chassis and connect the radar base to the chassis; Step S3: Install the two side frames on the left and right sides of the bottom frame respectively; Step S4: Prepare multiple shock absorbers, and connect the multiple shock absorbers to both ends of the first connecting rod and both ends of the second connecting rod. Then connect the first connecting rod to the radar antenna head, connect the second connecting rod to the radar turntable, and finally connect each shock absorber to the corresponding side frame.
9. A vibration reduction method according to claim 8, characterized in that, The step S2 is followed by the following steps: preparing a support rod, the support rod including a support rod body and a bottom connecting seat and a top connecting seat respectively hinged to both ends of the support rod body, fixing the bottom connecting seat to the chassis, and connecting the top connecting seat to the radar antenna head.