Shadow rocket launching seat with high compatibility

Abstract

The utility model discloses a weather modification rocket launching seat with high compatibility, relates to the field of weather modification equipment, and is used for solving the problem that the ejection angle offset of a rocket projectile is large in the continuous ground operation process. The figure rocket launching seat with high compatibility comprises a supporting plate, a rotating pressing plate, an embedded plate, a mounting plate, a connecting column and a limiting piece; two sliding grooves are formed in the bottom wall of the supporting plate in the length direction of the supporting plate in an extending mode, the two sliding grooves are arranged in parallel, and limiting holes are further formed in the sliding grooves. The rotary pressing plate is rotationally arranged on the supporting plate, and the rotary pressing plate rotates along the width edge of one side of the supporting plate; the pre-buried plate is used for being buried in soil; the mounting plate is arranged between the supporting plate and the embedded plate, the sliding block can extend into the sliding groove in the extending direction of the sliding groove, and a matching hole is further formed in the mounting plate; the connecting column is arranged between the mounting plate and the pre-embedded plate and is used for fixedly connecting the mounting plate and the pre-embedded plate; the limiting pieces are arranged in the limiting holes and the matching holes and used for enabling the supporting plate and the mounting plate to be relatively fixed.

Description

Technical Field

[0001] This application relates to the field of weather modification equipment, and particularly to a weather modification rocket launcher with high compatibility. Background Art

[0002] Weather modification means artificial weather influence. According to the physical characteristics of different clouds, appropriate timing is selected to disperse catalysts such as dry ice, silver iodide, and salt powder into the clouds by aircraft or rocket launchers, so as to cause cloud precipitation or increase precipitation, relieve farmland drought, increase reservoir irrigation water volume or water supply capacity.

[0003] In order to make the rocket launch angle easier to adjust and the loading speed faster, a Chinese patent with the application date of January 4, 2023 and the publication number of CN218916091U, a weather modification rocket launcher with high compatibility, discloses a structure. This weather modification rocket launcher has characteristics such as high loading efficiency and can improve operation efficiency.

[0004] However, weather modification operations are sometimes carried out on vehicles and sometimes on the ground. When operating on soft soil ground, the support plate of the rocket launcher is prone to local depression, especially in its rear seat area, resulting in a large deviation in the firing angle of the rocket projectile during continuous operation. Summary of the Utility Model

[0005] This application provides a weather modification rocket launcher with high compatibility, which is used to solve the problem of large deviation in the firing angle of rocket projectiles during continuous ground operation.

[0006] This application provides a weather modification rocket launcher with high compatibility, including a support plate, a rotating pressing plate, an embedded plate, a mounting plate, a connecting column, and a limiting member; two sliding grooves are formed on the bottom wall of the support plate and extend along its length direction, the two sliding grooves are arranged in parallel, and limiting holes are also provided on the sliding grooves; the rotating pressing plate is rotatably arranged on the support plate, and the rotating pressing plate rotates along one side width edge of the support plate; the embedded plate is used to be embedded in the soil; the mounting plate is arranged between the support plate and the embedded plate, a sliding block is provided on the mounting plate, and the sliding block can extend into the sliding groove along the extension direction of the sliding groove, and a matching hole is also provided on the mounting plate; the connecting column is arranged between the mounting plate and the embedded plate, and the connecting column is used to fixedly connect the mounting plate and the embedded plate; the limiting member is arranged in the limiting hole and the matching hole, and the limiting member is used to relatively fix the support plate and the mounting plate.

[0007] In this application, the support plate and the rotating pressure plate are used for angular deviation and loading and launching of rockets. The embedded parts are buried underground and fixedly connected to the mounting plate through connecting columns. The sliding grooves at the bottom of the support plate can correspond to the sliders on the mounting plate, and the support plate and the mounting plate are relatively fixed by limit pieces. When the rocket is launched, the impact on the mounting seat can be absorbed by the support plate, avoiding angular deviation of the rocket caused by relative movement between the support plate and the ground during continuous rocket launches, thus making the launch angle of the rocket more stable and the stability of the support plate during operation higher.

[0008] In some embodiments of this application, the connecting column is a hydraulic telescopic column. The hydraulic telescopic column can facilitate the adjustment of the height of the mounting plate, thus facilitating the grounding of the mounting plate and avoiding unstable connection of the connecting column due to too large a distance between the mounting plate and the ground.

[0009] In some embodiments of this application, the connecting column, the mounting plate and the embedded plate form a set of embedded components. Two sets of embedded components are provided, and the two sets of embedded components are spaced apart along the width direction of the support plate. The two sliders on the two sets of embedded components are correspondingly distributed with the two sliding grooves at the bottom of the support plate, and the sliders slide into the corresponding sliding grooves.

[0010] The two sets of embedded parts can respectively support the two sliding grooves. At the same time, when the two sets of embedded parts are installed under the support plate, the impact during rocket launch can be absorbed more evenly, avoiding damage due to insufficient strength of a single mounting plate and connecting column.

[0011] In some embodiments of this application, the highly compatible rocket launcher for human shadow also includes a first level. The first level is arranged on the side of the embedded plate close to the mounting plate, and the first level is strip-shaped. The first level can make the embedded plate more horizontal during embedding, which helps the horizontal setting of the mounting plate.

[0012] In some embodiments of this application, the highly compatible rocket launcher for human shadow also includes a second level. The second level is arranged on the side wall of the support plate, and the second level is strip-shaped. The second level can determine the horizontality of the support plate after the support plate is installed, which helps to stabilize the launch angle of the rocket and evenly absorb the recoil force, thus improving safety.

[0013] In some embodiments of this application, the highly compatible rocket launcher for human shadow also includes a pre-installed plate. The bottom of the pre-installed plate is provided with two sliding grooves, and the widths of the two sliding grooves at the bottom of the pre-installed plate are equal to the widths of the two sliding grooves at the bottom of the support plate. The pre-installed plate can pre-determine the installation interval and parallelism of the two mounting plates before the support plate and the mounting plate are installed, which helps the quick and stable installation of the support plate.

[0014] In some embodiments of the present application, a third level is formed on the pre-installed plate, and the third level is disposed on the top wall of the pre-installed plate. The third level can assist in judging the horizontal state of the support plate, so as to adjust in advance, reduce the workload after the installation of the support plate, and contribute to the efficient progress of the operation.

[0015] In some embodiments of the present application, pulleys are provided at the bottom of the support plate, and a plurality of pulleys are provided. The plurality of pulleys are spaced apart on the bottom wall of the support plate. The pulleys can make it more convenient for the support plate and the rotating pressing plate to move.

[0016] In some embodiments of the present application, receiving grooves are formed on the bottom wall of the support plate, and a plurality of receiving grooves are provided. The receiving grooves correspond to the pulleys one by one, and the pulleys are disposed in the corresponding receiving grooves and part of the pulleys extend outside the receiving grooves. The receiving grooves can reduce the lowest height of the support plate and prevent the pulleys from affecting the assembly of the support plate. Description of the Drawings

[0017] The drawings are used to provide a further understanding of the technical solutions of the present invention, and constitute a part of the specification. Together with the embodiments of the present application, they are used to explain the technical solutions of the present invention, and do not constitute a limitation to the technical solutions of the present invention.

[0018] Figure 1 It is a schematic diagram of a high-compatibility human-shaped rocket launcher provided by an embodiment of the present application.

[0019] Reference numerals: 1 - support plate; 11 - sliding groove; 12 - limiting hole; 13 - second level; 14 - pulley; 15 - receiving groove; 2 - rotating pressing plate; 3 - embedded plate; 31 - first level; 4 - soil; 5 - mounting plate; 51 - slider; 6 - connecting column; 7 - limiting member. Detailed Description of the Invention

[0020] Next, the technical solutions in the embodiments of the present application will be clearly and completely described with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present application without creative efforts shall fall within the protection scope of the present application.

[0021] It should be noted that all the directional indications (such as up, down, left, right, front, back...) in the embodiments of the present invention are only used to explain the relative positional relationship and movement conditions between components in a specific posture (as shown in the drawings). If the specific posture changes, the directional indications will also change accordingly.

[0022] The terms "first" and "second" are used for descriptive purposes only and should not be construed as indicating or implying relative importance or implicitly specifying the quantity of the indicated technical features. Thus, features defined with "first" and "second" may explicitly or implicitly include one or more of such features. In the description of this application, unless otherwise specified, the meaning of "a plurality" is two or more.

[0023] In the description of this application, it should be noted that unless otherwise clearly specified and defined, the terms "connected" and "coupled" should be understood in a broad sense. For example, it may be a fixed connection, a detachable connection, or an integral connection. For those of ordinary skill in the art, the specific meanings of the above terms in this application can be understood according to specific circumstances. Additionally, when describing pipelines, the terms "connected" and "coupled" used in this application have the meaning of conducting. The specific meaning needs to be understood in combination with the context.

[0024] In the embodiments of this application, words such as "exemplary" or "for example" are used to indicate examples, illustrations, or explanations. Any embodiment or design solution described as "exemplary" or "for example" in the embodiments of this application should not be construed as being more preferred or having more advantages than other embodiments or design solutions. Rather, the use of words such as "exemplary" or "for example" is intended to present relevant concepts in a specific manner.

[0025] Artificial weather modification, also known as cloud seeding, is based on the physical characteristics of different cloud layers. At an appropriate time, dry ice, silver iodide, salt powder and other catalysts are scattered into the clouds by airplanes or rocket launchers, causing the clouds to produce precipitation or increase the precipitation amount, so as to alleviate farmland drought, increase the water storage capacity of reservoirs or the water supply capacity.

[0026] In order to make it easier to adjust the rocket launch angle and increase the loading speed, a Chinese patent with an application date of January 4, 2023 and a publication number of CN218916091U, a highly compatible artificial weather modification rocket launcher, discloses a structure. This artificial weather modification rocket launcher has features such as high loading efficiency and can improve the operation efficiency.

[0027] However, artificial weather modification operations are sometimes carried out on vehicles and sometimes on the ground. When operating on soft soil ground, the support plate of the rocket launcher is prone to local depression, especially in its rear seat area, resulting in a large deviation in the firing angle of the rocket projectile during continuous operations.

[0028] To this end, please refer to Figure 1 , this application provides a highly compatible artificial weather modification rocket launcher, including a support plate 1, a rotating pressure plate 2, an embedded plate 3, a mounting plate 5, a connecting column 6 and a limiting member 7.

[0029] Please refer to Figure 1, two sliding grooves 11 are formed on the bottom wall of the support plate 1 along its length direction. The two sliding grooves 11 are arranged in parallel, and limiting holes 12 are also provided on the sliding grooves 11. The support plate 1 can be a conventional support plate 1. The sliding grooves 11 at the bottom of the support plate 1 can be slidably connected to the sliders 51 in the vehicle compartment, and can be limited by the limiting holes 12 at the same time to ensure stability during transportation.

[0030] Please refer to Figure 1 , the rotating pressing plate 2 is rotatably arranged on the support plate 1, and the rotating pressing plate 2 rotates along one side width edge of the support plate 1. The rotating pressing plate 2 can be a conventional rotating pressing plate 2, and its rotating structure can be the cooperation of a hydraulic column and a hinge.

[0031] Please refer to Figure 1 , the embedded plate 3 is used to be embedded in the soil 4. The embedded plate 3 can be a metal plate. The embedded plate 3 can have relatively high strength, and its material can be iron, steel, or other metal materials. The area of the embedded plate 3 can be smaller than the area of the support plate 1, and the thickness of the embedded plate 3 can be equal everywhere.

[0032] Please refer to Figure 1 , the mounting plate 5 is arranged between the support plate 1 and the embedded plate 3. The mounting plate 5 is provided with a slider 51, and the slider 51 can extend into the sliding groove 11 along the extension direction of the sliding groove 11. The mounting plate 5 is also provided with a mating hole. The area of the mounting plate 5 can be smaller than the area of the embedded plate 3, and the mounting plate 5 can be projected onto the middle of the embedded plate 3. The mounting plate 5 can be arranged parallel to the embedded plate 3. The slider 51 on the mounting plate 5 can be integrally formed with the mounting plate 5, or can be bolted or welded. The mating hole can be a threaded hole or a pin hole.

[0033] Please refer to Figure 1 , the connecting column 6 is arranged between the mounting plate 5 and the embedded plate 3. The connecting column 6 is used to fixedly connect the mounting plate 5 and the embedded plate 3. The connecting column 6 can be a conventional metal column, such as an iron column, or can be a telescopic column. The axis of the connecting column 6 can be perpendicular to the plate surface of the embedded plate 3 to make its supporting effect better.

[0034] Please refer to Figure 1 , the limiting member 7 is arranged in the limiting hole 12 and the mating hole. The limiting member 7 is used to relatively fix the support plate 1 and the mounting plate 5. The limiting member 7 can be a threaded member or a pin shaft, and can be set according to the mating hole.

[0035] Please refer to Figure 1, in this application, the support plate 1 and the rotating pressure plate 2 are used for angle deviation and loading and launching rockets. The embedded parts are buried underground and fixedly connected to the mounting plate 5 through the connecting column 6. The sliding groove 11 at the bottom of the support plate 1 can correspond to the slider 51 on the mounting plate 5, and the support plate 1 and the mounting plate 5 are relatively fixed by the limiting part 7. When the rocket is launched, the impact on the mounting seat can be absorbed by the support plate 1, avoiding the relative movement between the support plate 1 and the ground during continuous rocket launches, which may cause the angle deviation of the rocket, so that the firing angle of the rocket is more stable and the stability of the support plate 1 during operation is higher.

[0036] Please refer to Figure 1 , in some examples, when the embedded plate 3 is underground, the connecting column 6 can be completely buried in the soil 4, or the connecting column 6 can be partially exposed. At this time, the main supporting area of the support plate 1 connected to the mounting plate 5 is the embedded plate 3 and the soil 4 under the embedded plate 3. The soil 4 buried outside can prevent the embedded plate 3 from sliding.

[0037] Please refer to Figure 1 , in some examples, the limiting hole 12 on the sliding groove 11 can penetrate the sliding groove 11 along the thickness direction of the support plate 1, or can be horizontally arranged along the two side edges of the sliding groove 11.

[0038] Please refer to Figure 1 , in some examples, the connecting column 6 is a hydraulic telescopic column. The hydraulic telescopic column can facilitate the adjustment of the height of the mounting plate 5, so as to facilitate grounding of the mounting plate 5 and avoid unstable connection of the connecting column 6 due to too large a distance between the mounting plate 5 and the ground.

[0039] In some examples, the hydraulic telescopic column can be set to one, or can be set to multiple. Multiple hydraulic telescopic columns can improve the stability between the mounting plate 5 and the embedded plate 3.

[0040] Please refer to Figure 1 , in some examples, the connecting column 6, the mounting plate 5 and the embedded plate 3 form a set of embedded components. The embedded components are set to two groups, and the two groups of embedded components are spaced apart along the width direction of the support plate 1. The two sliders 51 on the two groups of embedded components are correspondingly distributed with the two sliding grooves 11 at the bottom of the support plate 1, and the sliders 51 slide into the corresponding sliding grooves 11.

[0041] The two groups of embedded parts can respectively support the two sliding grooves 11. At the same time, when the two groups of embedded parts are installed under the support plate 1, the impact during rocket launch can be absorbed more evenly, avoiding damage due to insufficient strength of a single mounting plate 5 and connecting column 6.

[0042] In some other examples, the embedded components are set to two groups, and two groups of embedded components are arranged in each sliding groove 11, and the two groups of embedded components are spaced apart along the length direction of the support plate 1.

[0043] Please refer to Figure 1 , in some examples, the high-compatibility human-shaped rocket launcher further includes a first level 31. The first level 31 is disposed on one side of the embedded plate 3 close to the mounting plate 5, and the first level 31 is strip-shaped. The first level 31 can make the embedded plate 3 more horizontal during embedding, which helps the horizontal setting of the mounting plate 5.

[0044] In some examples, the first level 31 can be embedded in the embedded plate 3 or can also be adhered to the embedded plate 3.

[0045] Please refer to Figure 1 , in some examples, the high-compatibility human-shaped rocket launcher further includes a second level 13. The second level 13 is disposed on the side wall of the support plate 1, and the second level 13 is strip-shaped. The second level 13 can determine the horizontality of the support plate 1 after the support plate 1 is installed, which helps the stability of the rocket launch angle and the uniform absorption of the recoil force, thereby improving safety.

[0046] In some examples, the second level 13 can be disposed on the edge in the length direction of the support plate 1, or can be disposed on the edge in the width direction of the support plate 1, or can be set to two. The two second levels 13 can be respectively distributed on the two edges in the length direction and the width direction.

[0047] The second level 13 can be the same as the first level 31. It can be embedded in the support plate 1 or can also be adhered to the support plate 1.

[0048] , in some examples, the high-compatibility human-shaped rocket launcher further includes a pre-mounted plate. Two chutes 11 are provided at the bottom of the pre-mounted plate. The widths of the two chutes 11 at the bottom of the pre-mounted plate are equal to those of the two chutes 11 at the bottom of the support plate 1. The pre-mounted plate can pre-determine the installation interval and parallelism of the two mounting plates 5 before the support plate 1 and the mounting plate 5 are installed, which helps the quick and stable installation of the support plate 1.

[0049] In some examples, the pre-mounted plate can be a non-metallic cardboard, such as an acrylic plate, or can be other types of light-transmitting plastic plates, so as to facilitate judging the embedding state of the mounting plate 5 and facilitating the confirmation of the embedding time of the pre-mounted plate.

[0050] Please refer to Figure 1 , in some examples, a third level is formed on the pre-mounted plate. The third level is disposed on the top wall of the pre-mounted plate. The third level can assist in judging the horizontal state of the support plate 1, so as to pre-adjust, reduce the workload after the support plate 1 is installed, and help the efficient progress of the operation.

[0051] In some examples, the third level can be strip-shaped, and the installation position of the third level can be in the central area of the pre-installed board. At this time, two third levels can be provided, and the two third levels are arranged crosswise, which helps to judge the levelness of the pre-installed board.

[0052] Please refer to Figure 1 , in some examples, pulleys 14 are provided at the bottom of the support plate 1. A plurality of pulleys 14 are provided, and the plurality of pulleys 14 are spaced apart and distributed on the bottom wall of the support plate 1. The pulleys 14 can make it more convenient for the support plate 1 and the rotating pressing plate 2 to move.

[0053] In some examples, the number of pulleys 14 can be set to 4 or 6, preferably 6.

[0054] Please refer to Figure 1 , in some examples, receiving grooves 15 are formed on the bottom wall of the support plate 1. A plurality of receiving grooves 15 are provided, and the receiving grooves 15 correspond to the pulleys 14 one by one. The pulleys 14 are arranged in the corresponding receiving grooves 15 and part of the pulleys 14 extend out of the receiving grooves 15. The receiving grooves 15 can reduce the lowest height of the support plate 1 and prevent the pulleys 14 from affecting the assembly of the support plate 1.

[0055] In some examples, the receiving grooves 15 can be slightly larger than the pulleys. At the same time, rounded corners can be provided in the sliding direction of the upper edge of the pulleys 14, and the radius of the rounded corners is greater than the radius of the pulleys 14, which is convenient for cleaning the soil entering the receiving grooves 15.

[0056] In the description of this specification, specific features, structures, materials or characteristics can be combined in a suitable manner in any one or more embodiments or examples.

[0057] The above is only the specific implementation manner of the present application, but the protection scope of the present application is not limited thereto. Any changes or substitutions within the technical scope disclosed in the present application should be covered by the protection scope of the present application. Therefore, the protection scope of the present application should be subject to the protection scope of the claims.

Claims

1. A highly compatible human-shaped rocket launcher, characterized in that: include: The support plate has two slide grooves extending along the length direction of the bottom wall, the two slide grooves are arranged in parallel, and the slide grooves are also provided with limiting holes; A rotating pressing plate is rotatably arranged on the supporting plate, and the rotating pressing plate rotates along a width edge of one side of the supporting plate; Embedded plate, used for burying in the soil; A mounting plate is arranged between the support plate and the embedded plate, a slider is arranged on the mounting plate, the slider can extend into the slide groove along the extension direction of the slide groove, and a matching hole is also arranged on the mounting plate; A connecting column is provided between the mounting plate and the embedded plate, and is used to fix the mounting plate and the embedded plate; A limiting member is arranged in the limiting hole and the matching hole, and the limiting member is used to relatively fix the supporting plate and the mounting plate.

2. The highly compatible human-shaped rocket launcher according to claim 1, characterized in that: The connecting column is a hydraulic telescopic column.

3. The highly compatible human-shaped rocket launcher according to claim 2, characterized in that: The connecting column, the mounting plate and the embedded plate form a group of embedded components, and the embedded components are arranged in two groups. The two groups of embedded components are spaced apart along the width direction of the support plate, and the two sliders on the two groups of embedded components are correspondingly distributed with the two slide grooves at the bottom of the support plate, and the sliders slide into the corresponding slide grooves.

4. The highly compatible human-shaped rocket launcher according to claim 3, characterized in that: The highly compatible human-shaped rocket launch base also includes a first spirit level, which is arranged on a side of the embedded plate close to the mounting plate, and the first spirit level is in a bar shape.

5. The highly compatible human-shaped rocket launcher according to claim 4, characterized in that: The highly compatible human-shaped rocket launch base also includes a second level, which is arranged on the side wall of the support plate and is in a strip shape.

6. The highly compatible human-shaped rocket launcher according to any one of claims 1 to 5, characterized in that: The highly compatible human-shaped rocket launch base also includes a pre-installed plate, and two slide grooves are arranged at the bottom of the pre-installed plate. The width of the two slide grooves at the bottom of the pre-installed plate is equal to the width of the two slide grooves at the bottom of the support plate.

7. The highly compatible human-shaped rocket launcher according to claim 6, characterized in that: A third level is formed on the pre-installed plate and is arranged on the top wall of the pre-installed plate.

8. The highly compatible human-shaped rocket launcher according to claim 1, characterized in that: A pulley is disposed at the bottom of the support plate, wherein the pulley is provided in plurality and the plurality of pulleys are distributed at intervals on the bottom wall of the support plate.

9. The highly compatible human-shaped rocket launcher according to claim 8, characterized in that: A receiving groove is formed on the bottom wall of the support plate. There are a plurality of receiving grooves, each of which corresponds to the pulley one by one. The pulley is disposed in the corresponding receiving groove and the pulley portion extends out of the receiving groove.

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