Meteorological and sounding rocket storage, transportation and hoisting device

Abstract

The utility model discloses a storing, transporting and hoisting device for meteorological and sounding rockets. The storing, transporting and hoisting device comprises a launching platform, a rotating seat assembly, a launching track, a fixing assembly and a hoisting assembly. Due to the fact that the meteorological sounding rocket storing, transporting and hoisting device is fixedly connected to the transportation tool and provided with the fixing assembly and the hoisting assembly, when the meteorological sounding rocket is transported, the meteorological sounding rocket is fixedly connected to the launching track through the fixing assembly, and after the meteorological sounding rocket reaches the destination, the fixing assembly is detached and stored. And then the hoisting assembly is installed on the launching platform, the meteorological and sounding rocket is hoisted through the hoisting assembly, the meteorological and sounding rocket is accurately installed on the launching track, and the hoisting assembly is disassembled and stored. According to the storing, transporting and hoisting device for the meteorological and sounding rockets, the meteorological and sounding rockets can be conveniently transported and can also be conveniently hoisted, so that the use of special transport vehicles and cranes is avoided, and the effect of saving space and cost is achieved.

Description

Technical Field

[0001] This application relates to the field of rocket transportation equipment technology, and in particular to a meteorological sounding rocket storage, transportation and hoisting device. Background Technology

[0002] Near space refers to the Earth's atmosphere at altitudes between 20km and 100km. Atmospheric parameters in near space, such as temperature, pressure, density, wind speed, and wind direction, have important applications in spacecraft flight tests. Currently, there are three types of methods for detecting near-space atmospheric parameters: space-based detection, mainly atmospheric sounding satellites; ground-based detection, mainly mid-frequency radar, MST radar, and lidar; and in-situ detection, mainly meteorological sounding rockets and sounding balloons. Of these three methods, space-based and ground-based methods use certain physical principles to invert and obtain atmospheric parameters, while in-situ detection uses sensors to directly detect the atmosphere as it passes through, thus having an inherent advantage in reliability. In China, balloon sounding is relatively mature, but its altitude generally only reaches about 30km, with specially designed large balloons reaching about 45km. Meteorological sounding rockets, on the other hand, can reach altitudes of up to 60km, meeting the needs of specific scenarios such as aerospace.

[0003] Meteorological sounding rockets are a very important means of in-situ measurement of the near-space atmospheric environment. They use unguided rockets to send payloads (sondesk and parachute packs) to altitudes above 70km. During the descent of the radiosonde and parachute, they can detect in-situ atmospheric temperature, pressure, density, wind speed and wind direction data in the near-space region between 20km and 60km.

[0004] Its working process is as follows: After the rocket ignites, the main engine and boosters ignite and work simultaneously, generating a predetermined thrust. Under the action of the thrust, the rocket leaves the launch rail. After leaving the rail, the rocket continues to ascend along the predetermined trajectory under the action of the thrust. When the main engine shuts down, the rocket reaches its maximum speed. Then, the rocket continues to ascend by its inertia. At the pre-set separation time, the payload separates from the rocket body. After separation, the payload continues to fly by inertia, and the trajectory is similar to a parabola. It first climbs to the top and then descends. During the descent, the speed increases. When the dynamic pressure of the parachute is satisfied, the parachute opens and decelerates rapidly. Then, the parachute carries the radiosonde and slowly drifts down with the wind. During the descent, the atmospheric temperature, air pressure, density, wind speed and wind direction along the drift trajectory are measured and the data is sent to the ground receiving system.

[0005] In related technologies, sounding rockets often use dedicated storage and transportation containers and cranes, which increases the complexity of the system equipment and the total cost, and also makes operation more complex. Utility Model Content

[0006] This application provides a storage, transportation, and hoisting device for meteorological sounding rockets, which solves the technical problem in the prior art that meteorological sounding rockets require specialized storage and transportation equipment and lifting equipment, resulting in large size and high complexity of the transportation and launch devices for meteorological sounding rockets. The technical solution is as follows:

[0007] A weather sounding rocket storage, transportation, and hoisting device, mounted on a transport vehicle, includes:

[0008] The launch platform is fixedly connected to the transport vehicle;

[0009] The rotating base assembly includes a fixed disk and a rotating disk arranged sequentially from bottom to top and sharing a central axis. The fixed disk is fixedly connected to the launch platform, and the rotating disk is rotatable relative to the fixed disk.

[0010] The launch track is provided with a groove along its length, which matches the slider on the weather sounding rocket; one end of the launch track is hinged to the rotating disk, and a pitch cylinder for adjusting the pitch angle of the launch track is provided between the launch track and the rotating disk.

[0011] A fixing component, detachably connected to the launch rail, is used to secure the weather sounding rocket;

[0012] And a hoisting assembly, which is detachably connected to the launch platform for hoisting the weather sounding rocket.

[0013] Optionally, the groove is a T-shaped groove located on the upper surface of the launch track, and the slider is a T-shaped slider disposed on the outer surface of the weather sounding rocket.

[0014] Optionally, the meteorological sounding rocket has two sliders, which are distributed along the length of the meteorological sounding rocket; and at least two sets of fixing components are distributed on the outside of the two sliders.

[0015] Optionally, the fixing assembly includes a lower clamp and an upper clamp, one end of the lower clamp and one end of the upper clamp are hinged together, the other end of the lower clamp is provided with a first connecting hole, and the other end of the upper clamp is provided with a second connecting hole; the fixing assembly also includes a first bolt for connecting the first connecting hole and the second connecting hole.

[0016] Optionally, the fixing component includes a lower clamp and an upper clamp, with a third connecting hole at each end of the lower clamp and a fourth connecting hole at each end of the upper clamp; the fixing component also includes a first bolt for connecting the third connecting hole and the fourth connecting hole.

[0017] Optionally, the fixing assembly includes a buffer pad disposed inside the upper clamp and the lower clamp; the fixing assembly also includes a shock absorber disposed between the lower clamp and the launch rail.

[0018] Optionally, the hoisting assembly includes a frame, a rail, and a lifting device. The rail is detachably connected to the frame, and the lifting device is movably connected to the rail and can move along the rail.

[0019] Optionally, the frame includes two front uprights and two rear uprights. The lower ends of the two front uprights and the two rear uprights are all threaded. The launch platform has four threaded holes that match the external threads. The two front uprights and the two rear uprights are all threadedly connected to the launch platform. The upper ends of the two front uprights are connected through a front crossbeam, and the upper ends of the two rear uprights are connected through a rear crossbeam. The hanging rail is fixedly connected to the front and rear crossbeams by a bolt group.

[0020] Optionally, the frame includes two front uprights and two rear uprights. The lower ends of the two front uprights are each provided with a first fixing plate, and the first fixing plate has a fifth connecting hole. The two front uprights are connected to the launch platform via second bolts. The lower ends of the two rear uprights are each provided with a second fixing plate, and the second fixing plate has a fifth connecting hole. The two rear uprights are connected to the launch platform via second bolts. The upper ends of the two front uprights are connected via a front crossbeam, and the upper ends of the two rear uprights are connected via a rear crossbeam. The hanging rail is fixedly connected to the front and rear crossbeams via a bolt group.

[0021] Optionally, the lifting device is a mobile pulley block, which includes a pulley block body and a hanging wheel connected to the pulley block body, and the pulley block body is connected to the hanging rail via the hanging wheel; or, the lifting device is an electric hoist, which is connected to the hanging rail.

[0022] The beneficial effects of the technical solutions provided in this application include at least the following:

[0023] A weather sounding rocket storage, transportation, and hoisting device includes: a launch platform, a rotating base assembly, a launch rail, a fixing assembly, and a hoisting assembly. Since the device comprises both a fixing assembly and a hoisting assembly, during transport, the weather sounding rocket is first secured to the launch rail using the fixing assembly. Upon arrival at the destination, the fixing assembly is removed and stored. Then, the hoisting assembly is installed on the launch platform, and the device is used to lift the weather sounding rocket, accurately placing it onto the launch rail. The hoisting assembly is then removed and stored. The rotating base assembly can be used to adjust the azimuth angle of the weather sounding rocket, and the pitch cylinder can be used to adjust the launch angle. Therefore, using the weather sounding rocket storage, transportation, and hoisting device provided in this application allows for convenient transportation and hoisting of the weather sounding rocket, avoiding the need for specialized transport vehicles and cranes, thus saving space and costs.

[0024] Other features and advantages of this disclosure will be described in detail in the following detailed description section. Attached Figure Description

[0025] To more clearly illustrate the technical solutions in the embodiments of this application, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0026] Figure 1 This is a 3D schematic diagram of a weather sounding rocket;

[0027] Figure 2 This is a three-dimensional schematic diagram of the meteorological sounding rocket storage, transportation, and hoisting device provided in the embodiments of this application;

[0028] Figure 3 This is a schematic diagram of fixing a meteorological sounding rocket to a meteorological sounding rocket storage, transportation and hoisting device provided in an embodiment of this application;

[0029] Figure 4 This is a three-dimensional schematic diagram of the fixed components in the meteorological sounding rocket storage, transportation and hoisting device provided in the embodiments of this application;

[0030] Figure 5 This is an exploded view of the fixed components in the meteorological sounding rocket storage, transportation and hoisting device provided in the embodiments of this application;

[0031] Figure 6 This is a three-dimensional schematic diagram of the hoisting components in the meteorological sounding rocket storage, transportation and hoisting device provided in the embodiments of this application when they are installed on the launch platform;

[0032] Figure 7 yes Figure 6 A magnified view of a section at point A in the middle;

[0033] Figure 8 This is a schematic diagram of a meteorological sounding rocket being lifted using the meteorological sounding rocket storage, transportation, and hoisting device provided in the embodiments of this application;

[0034] Figure 9 This is a rear view of a weather sounding rocket being placed on a weather sounding rocket storage, transportation, and hoisting device.

[0035] Figure 10 This is a schematic diagram of the meteorological sounding rocket provided in this application embodiment in a ready-to-launch state on the meteorological sounding rocket storage, transportation and hoisting device.

[0036] Explanation of reference numerals in the attached figures

[0037] 1-Weather sounding rocket; 11-Slider; 2-Launch platform; 3-Rotating seat assembly; 31-Fixed disk; 32-Rotating disk; 4-Launch track; 41-Slide groove; 5-Fixing assembly; 51-Lower clamp; 52-Upper clamp; 53-Buffer pad; 54-First bolt; 55-Shock absorber; 6-Lifting assembly; 61-Frame; 611-Front upright; 612-Rear upright; 613-Front crossbeam; 614-Rear crossbeam; 62-Lifting rail; 63-Lifting equipment; 631-Pulley block body; 632-Hanging wheel; 7-Pitch cylinder. Detailed Implementation

[0038] The specific embodiments of this disclosure will be described in detail below with reference to the accompanying drawings. It should be understood that the specific embodiments described herein are for illustration and explanation only and are not intended to limit this disclosure.

[0039] In this disclosure, unless otherwise stated, directional terms such as "upper" and "lower" generally refer to the relative positions of the corresponding components in the direction of gravity when they are in use, and "inner" and "outer" refer to their relative positions to the contours of the corresponding components themselves. Furthermore, the terms "first," "second," etc., used in this disclosure are for distinguishing one element from another and do not have sequential or importance implications. In the following description, when referring to the accompanying drawings, unless otherwise explained, the same reference numerals in different drawings denote the same or similar elements.

[0040] According to the embodiments of this application, refer to Figures 1 to 10 As shown, a weather sounding rocket storage, transportation and hoisting device is installed on a transport vehicle, which can be a truck, train or ship, etc.

[0041] The weather sounding rocket storage, transportation and hoisting device may include: launch platform 2, rotating seat assembly 3, launch rail 4, fixing assembly 5, and hoisting assembly 6.

[0042] The launch platform 2 is fixedly connected to the transport vehicle. The rotating base assembly 3 may include a fixed disk 31 and a rotating disk 32 arranged sequentially from bottom to top and sharing a central axis. The fixed disk 31 is fixedly connected to the launch platform 2, and the rotating disk 32 can rotate relative to the fixed disk 31.

[0043] The launch track 4 is provided with a groove 41 along its length, which matches the slider 11 on the meteorological sounding rocket 1. When the meteorological sounding rocket 1 is launched, the slider 11 matches the groove 41, ensuring that the meteorological sounding rocket 1 slides accurately along the groove 41 of the launch track 4. One end of the launch track 4 is hinged to a rotating disk 32, and a pitch cylinder 7 for adjusting the pitch angle of the launch track 4 is provided between the launch track 4 and the rotating disk 32. By providing the pitch cylinder 7, the launch angle of the meteorological sounding rocket 1 can be easily controlled.

[0044] The fixing component 5 is detachably connected to the launch track 4. During the transportation of the weather sounding rocket 1, the fixing component 5 is used to fix the weather sounding rocket 1. After the weather sounding rocket 1 reaches its destination, the fixing component 5 can be removed from the launch platform 2 and stored in the transport vehicle.

[0045] The hoisting assembly 6 is detachably connected to the launch platform 2. After the meteorological sounding rocket 1 is transported to its destination, the hoisting assembly 6 is installed on the launch platform 2 and used to hoist the meteorological sounding rocket 1. After the meteorological sounding rocket 1 is hoisted, the hoisting assembly 6 can be disassembled and stored in the transport vehicle.

[0046] In the above embodiments, the meteorological sounding rocket storage, transportation, and hoisting device is fixed to the transport vehicle. Since the device has a fixing component 5 and a hoisting component 6, when transporting the meteorological sounding rocket 1, the fixing component 5 is first used to fix the rocket 1 to the launch track 4. After reaching the destination, the fixing component 5 is removed and stored. Then, the hoisting component 6 is installed on the launch platform 2, and the hoisting component 6 is used to lift the meteorological sounding rocket 1, accurately installing it onto the launch track 4. The hoisting component 6 is then removed. The rotating seat component 3 of the meteorological sounding rocket storage, transportation, and hoisting device can be used to adjust the azimuth angle of the rocket 1, and the pitch cylinder 7 can be used to adjust the launch angle of the rocket 1. Therefore, using the meteorological sounding rocket storage, transportation, and hoisting device provided in this application embodiment, the meteorological sounding rocket 1 can be transported and hoisted conveniently, thus avoiding the use of specialized transport vehicles and cranes, thereby achieving the effect of saving space and cost.

[0047] According to the embodiments of this application, refer to Figure 2 and Figure 9 As shown, the groove 41 is a T-shaped groove located on the upper surface of the launch track 4, and the slider 11 is a T-shaped slider 11 disposed on the outer surface of the weather sounding rocket 1. In other embodiments, the groove 41 can also be a dovetail groove, and correspondingly, the slider 11 can be a dovetail slider; this application does not impose any limitations on this.

[0048] According to the embodiments of this application, refer to Figure 3 As shown, the meteorological sounding rocket 1 has two sliders 11, which are distributed along the length of the meteorological sounding rocket 1. Therefore, there are at least two sets of fixing components 5, which are distributed on the outside of the two sliders 11. In this way, during transportation, the two fixing components 5 can lock the two sliders 11, preventing the meteorological sounding rocket 1 from moving back and forth.

[0049] According to an embodiment of this application, the fixing component 5 includes a lower clamp 51 and an upper clamp 52. One end of the lower clamp 51 and one end of the upper clamp 52 are hinged (not shown in the figures). The other end of the lower clamp 51 is provided with a first connecting hole, and the other end of the upper clamp 52 is provided with a second connecting hole. The fixing component 5 also includes a first bolt 54 for connecting the first connecting hole and the second connecting hole. This fixing method allows for faster opening of the fixing component 5 and release of the weather sounding rocket 1.

[0050] According to another embodiment of this application, reference is made to Figure 4 and Figure 5 As shown, the fixing assembly 5 includes a lower clamp 51 and an upper clamp 52. The lower clamp 51 has third connecting holes at both ends, and the upper clamp 52 has fourth connecting holes at both ends. The fixing assembly 5 also includes a first bolt 54 for connecting the third and fourth connecting holes. This fixing method allows for more reliable securing of the weather sounding rocket 1.

[0051] According to the embodiments of this application, refer to Figure 4 and Figure 5 As shown, the fixing component 5 includes a buffer pad 53, which is disposed inside the upper clamp 52 and the lower clamp 51. Please refer to [reference needed]. Figure 5 The fixing assembly may also include a shock absorber 55, which is disposed between the lower clamp 51 and the launch rail 4. The shock absorber 55 may be a hydraulic shock absorber, a pneumatic shock absorber, or an electronic shock absorber, and this application does not limit this.

[0052] According to the embodiments of this application, refer to Figure 2 and Figure 6As shown, the hoisting assembly 6 includes a frame 61, a hoisting rail 62, and a hoisting device 63. The hoisting rail 62 is detachably connected to the frame 61, and the hoisting device 63 is movably connected to the hoisting rail 62. The hoisting device 63 can move along the hoisting rail 62.

[0053] According to one embodiment of this application, reference is made to... Figure 6 As shown, the frame 61 includes two front uprights 611 and two rear uprights 612. The lower ends of the two front uprights 611 and the two rear uprights 612 are all threaded. The launch platform 2 has four threaded holes that match the external threads. The two front uprights 611 and the two rear uprights 612 are all threadedly connected to the launch platform 2. The upper ends of the two front uprights 611 are connected through a front crossbeam 613, and the upper ends of the two rear uprights 612 are connected through a rear crossbeam 614. The lifting rail 62 is fixedly connected to the front crossbeam 613 and the rear crossbeam 614 by a set of bolts 7. Since the lifting assembly 6 is detachable, it can be disassembled and placed on the transport vehicle during the transportation of the sounding rocket, thereby reducing the space occupied. When the meteorological sounding rocket 1 arrives at its destination, the lifting assembly 6 can be quickly assembled onto the launch platform 2 and used to lift the meteorological sounding rocket 1.

[0054] According to another embodiment of this application, the frame 61 includes two front uprights 611 and two rear uprights 612. The lower ends of the two front uprights 611 are respectively provided with a first fixing plate (not shown in the figure), and the first fixing plate is provided with a fifth connecting hole (not shown in the figure). The two front uprights 611 are connected to the launch platform 2 by a second bolt 7. The lower ends of the two rear uprights 612 are respectively provided with a second fixing plate (not shown in the figure), and the second fixing plate is provided with a fifth connecting hole (not shown in the figure). The two rear uprights 612 are connected to the launch platform 2 by a second bolt 7. The upper ends of the two front uprights 611 are connected by a front crossbeam 613, and the upper ends of the two rear uprights 612 are connected by a rear crossbeam 614. The hanging rail 62 is fixedly connected to the front crossbeam 613 and the rear crossbeam 614 by a set of bolts 7.

[0055] It should be noted that in other embodiments, the frame 61 may also be other forms of detachable and easy-to-assemble frame 61, and the embodiments of this application do not limit this.

[0056] According to the embodiments of this application, refer to Figure 6 and Figure 7 As shown, the lifting device 63 is a movable pulley block, which includes a pulley block body 631 and a hanging wheel 632 connected to the pulley block body 631. The pulley block body 631 is connected to the hanging rail 62 through the hanging wheel 632; Reference Figure 8 and Figure 9As shown, the main body 631 of the pulley block can be a single fixed pulley or a pulley block composed of fixed pulleys and movable pulleys. Workers can lift the meteorological sounding rocket 1 by pulling ropes, thus avoiding the use of a professional crane.

[0057] In another possible embodiment, the lifting device 63 can also be an electric hoist, and the lifting rail 62 can be a matching rail 62, with the electric hoist connected to the lifting rail 62. This design further facilitates the lifting and moving of the meteorological sounding rocket 1 by personnel, thereby avoiding the need for a specialized crane.

[0058] Once the weather sounding rocket 1 is accurately installed onto the launch track 4, the hoisting assembly 6 can be removed and stored in the transport vehicle. By controlling the rotating seat assembly 3 and the pitch cylinder 7, the staff can precisely control the azimuth and launch angle of the weather sounding rocket 1.

[0059] refer to Figure 1 and Figure 10 As shown below, the implementation principle of the meteorological sounding rocket storage, transportation, and hoisting device of this application is explained with specific operating steps:

[0060] The first step is to securely attach the weather sounding rocket storage, transportation, and hoisting equipment to a transport vehicle, such as a truck.

[0061] The second step is to install the three lower clamps 51 onto the launch track 4, and then place the weather sounding rocket 1 onto the three lower clamps 51, with the two sliders 11 located on the inner side of the two lower clamps 51 at the ends respectively.

[0062] The third step is to connect the three upper clamps 52 to the three lower clamps 51 respectively through the three first bolts 54 to reliably fix the meteorological sounding rocket 1;

[0063] The fourth step is to start the truck to transport the weather sounding rocket 1 to its destination;

[0064] Fifth step: Assemble the frame 61 of the hoisting component 6 and install it on the launch platform 2, install the hoisting rail 62 on the frame 61, and install the lifting equipment 63, such as the movable pulley block, on the hoisting rail 62;

[0065] Step 6: Unlock the first bolt 54 connecting the upper clamp 52 and the lower clamp 51, use the movable pulley system to lift the meteorological sounding rocket 1 and install the meteorological sounding rocket 1 onto the launch track 4;

[0066] Step 7: Remove hoisting component 6 and store it in the transport vehicle;

[0067] Step 8: Adjust the azimuth angle and launch pad of the weather sounding rocket 1 using the rotating seat assembly 3 and the pitch cylinder 7, and wait for the launch command;

[0068] Step 9: Launch meteorological sounding rocket 1.

[0069] The preferred embodiments of this disclosure have been described in detail above with reference to the accompanying drawings. However, this disclosure is not limited to the specific details of the above embodiments. Within the scope of the technical concept of this disclosure, various simple modifications can be made to the technical solutions of this disclosure, and these simple modifications all fall within the protection scope of this disclosure.

[0070] It should also be noted that the various specific technical features described in the above embodiments can be combined in any suitable manner without contradiction. To avoid unnecessary repetition, this disclosure will not describe the various possible combinations separately.

[0071] Furthermore, various different embodiments of this disclosure can be combined in any way, as long as they do not violate the spirit of this disclosure, they should also be regarded as the content disclosed in this disclosure.

Claims

1. A storage, transportation, and hoisting device for meteorological sounding rockets, mounted on a transport vehicle, characterized in that, include: Launch platform (2) is fixedly connected to the transport vehicle; The rotating base assembly (3) includes a fixed disk (31) and a rotating disk (32) arranged sequentially from bottom to top and sharing a central axis. The fixed disk (31) is fixedly connected to the launch platform (2), and the rotating disk (32) can rotate relative to the fixed disk (31). The launch track (4) is provided with a groove (41) along the length of the launch track (4), and the groove (41) matches the slider (11) on the meteorological sounding rocket (1); one end of the launch track (4) is hinged to the rotating disk (32), and a pitch cylinder (7) for adjusting the pitch angle of the launch track (4) is provided between the launch track (4) and the rotating disk (32); A fixing component (5) is detachably connected to the launch rail (4) for fixing the weather sounding rocket (1); And a hoisting assembly (6), which is detachably connected to the launch platform (2) for hoisting the meteorological sounding rocket (1).

2. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 1, characterized in that, The groove (41) is a T-shaped groove located on the upper surface of the launch track (4), and the slider (11) is a T-shaped slider (11) set on the outer surface of the weather sounding rocket (1).

3. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 2, characterized in that, The meteorological sounding rocket (1) has two sliders (11), which are distributed along the length of the meteorological sounding rocket (1); the number of fixing components (5) is at least two sets, which are distributed on the outside of the two sliders (11).

4. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 1, characterized in that, The fixing component (5) includes a lower clamp (51) and an upper clamp (52). One end of the lower clamp (51) and one end of the upper clamp (52) are hinged together. The other end of the lower clamp (51) is provided with a first connecting hole, and the other end of the upper clamp (52) is provided with a second connecting hole. The fixing component (5) also includes a first bolt (54) for connecting the first connecting hole and the second connecting hole.

5. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 1, characterized in that, The fixing component (5) includes a lower clamp (51) and an upper clamp (52). The lower clamp (51) has a third connecting hole at each end, and the upper clamp (52) has a fourth connecting hole at each end. The fixing component (5) also includes a first bolt (54) for connecting the third connecting hole and the fourth connecting hole.

6. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 4 or 5, characterized in that, The fixing component (5) includes a buffer pad (53), which is disposed on the inner side of the upper clamp (52) and the lower clamp (51); The fixing assembly also includes a shock absorber (55) disposed between the lower clamp (51) and the launch rail (4).

7. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 1, characterized in that, The hoisting assembly (6) includes a frame (61), a hoisting rail (62), and a lifting device (63). The hoisting rail (62) is detachably connected to the frame (61), and the lifting device (63) is movably connected to the hoisting rail (62). The lifting device (63) can move along the hoisting rail (62).

8. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 7, characterized in that, The frame (61) includes two front uprights (611) and two rear uprights (612). The lower ends of the two front uprights (611) and the two rear uprights (612) are all threaded. The launch platform (2) has four threaded holes that match the external threads. The two front uprights (611) and the two rear uprights (612) are all threadedly connected to the launch platform (2). The upper ends of the two front uprights (611) are connected by a front crossbeam (613), and the upper ends of the two rear uprights (612) are connected by a rear crossbeam (614); the hanging rail (62) is fixedly connected to the front crossbeam (613) and the rear crossbeam (614) by a bolt group.

9. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 7, characterized in that, The frame (61) includes two front uprights (611) and two rear uprights (612). The lower ends of the two front uprights (611) are respectively provided with a first fixing plate, and the first fixing plate is provided with a fifth connecting hole. The two front uprights (611) are connected to the launch platform (2) by a second bolt. The lower ends of the two rear uprights (612) are respectively provided with a second fixing plate, and the second fixing plate is provided with a fifth connecting hole. The two rear uprights (612) are connected to the launch platform (2) by a second bolt. The upper ends of the two front uprights (611) are connected by a front crossbeam (613), and the upper ends of the two rear uprights (612) are connected by a rear crossbeam (614); the hanging rail (62) is fixedly connected to the front crossbeam (613) and the rear crossbeam (614) by a bolt group.

10. The meteorological sounding rocket storage, transportation, and hoisting device according to claim 7, characterized in that, The lifting equipment (63) is a movable pulley block, which includes a pulley block body (631) and a hanging wheel (632) connected to the pulley block body (631). The pulley block body (631) is connected to the hanging rail (62) through the hanging wheel (632). Alternatively, the lifting device (63) may be an electric hoist connected to the lifting rail (62).

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