Weather modification catalyst launching control platform

Abstract

The utility model provides a kind of weather modification catalyst launch adjustment platform, the utility model relates to weather modification technical field, including pedestal, pedestal is embedded with a pair of angle axle seat, transmission cooperation has bearing seat between two angle axle seats and pedestal, and the one end of angle axle seat relative to bearing seat extends with double axle wheel outside, and the two sections of shaft body of coaxial core are formed with double axle wheel outside extension;The utility model has the beneficial effect that: in pedestal, the rail frame extended with fixed end portion of bearing structure connection and the lateral extension lateral foot seat structure, the elevation end of bearing seat in structure is connected with rail frame by double axle wheel, the relative elevation angle between rail frame and pedestal is adjusted by axial rotation, the fixed plane of vehicle-mounted structure is fixed with pedestal, to complete the support fixing of adjustment structure simultaneously, compared with traditional adjustment platform, the adjustment structure stability and overall structure strength of the adjustment platform are improved, and it is adapted to the launch adjustment of catalyst in complex scene.

Description

Technical Field

[0001] This utility model relates to the field of weather modification technology, and more specifically, to a weather modification catalyst emission adjustment platform. Background Technology

[0002] Artificial weather modification is the use of scientific methods to regulate meteorological processes. One of its core elements is the precise delivery of catalysts. Currently, it mainly employs a variety of methods, including aircraft seeding, rocket / artillery shell launches, ground generators, and drones. The appropriate method is selected based on the characteristics of the target cloud. Aircraft carrying silver iodide flares or hygroscopic particles can directly penetrate the cloud layer to carry out large-scale catalysis, which is suitable for rain enhancement and fog dissipation. Rocket systems are rapidly deployed via vehicle-mounted launchers and use ballistic calculations to deliver catalysts to the supercooled water-rich areas of the cloud, demonstrating high efficiency in hail suppression operations. In mountainous areas, ground-based smoke generators burn silver iodide, and the catalysts are naturally transported to the cloud base by updrafts.

[0003] Typically, ground-based catalyst launchers are vehicle-mounted structures. The launcher is primarily adjusted by the platform's elevation angle. Traditional launchers use a folded structure consisting of a main support frame and a secondary support frame to assemble the catalyst launcher. The elevation angle of this structure is mainly maintained by counterweights to ensure structural stability. However, when facing rugged launch scenarios such as mountainous areas, if the elevation angle is too large, the support strength itself is limited by the stability of the platform surface, resulting in corresponding shaking of the frame during launch and affecting launch accuracy. Utility Model Content

[0004] The technical problem to be solved by this utility model is that the existing launch pad adjustment structure uses counterweight to adjust the elevation angle of the frame. The stability of the support structure itself is easily affected by the stability of the platform surface, which leads to structural vibration and affects the launch stability and accuracy. In view of the problems existing in the prior art, an artificial weather modification catalyst launch adjustment pad is provided.

[0005] The purpose and effect of this utility model are achieved by the following specific technical means: including a base, on which a pair of corner bearings are embedded, and a bearing seat is connected to the base for transmission between the two corner bearings and the base. A double shaft wheel extends outward from one end of the corner bearing relative to the bearing seat. Two shafts with coaxial cores are formed on the outer side of the double shaft wheel. One shaft is fixed with a support shaft, and the other shaft passes through the outer side of the corner bearing and is fixedly provided with a rail frame.

[0006] The rail frame is provided with a groove with a custom toothed interval size, and a mounting rail plate is slidably fitted in the groove. The mounting rail plate is provided with a matching slide table on the groove, and an adjusting shaft is fixed at the inner end of the mounting rail plate. A hydraulic groove is left between the end of the adjusting shaft and the rail frame.

[0007] A side foot seat is fixedly installed on the outside of the support shaft.

[0008] Furthermore, the platform surface of the pedestal extends to form two platform plates that match the rail frame.

[0009] A further preferred embodiment: the platform plate is fixedly positioned to the bottom surface of the support shaft and the corner shaft seat.

[0010] A further preferred embodiment: a displacement slide tube is sleeved on the adjusting shaft, and a displacement sensor matching the rail frame slide groove is rotatably mounted on the displacement slide tube.

[0011] A further preferred embodiment: a plug rod is inserted into the slide, and a connecting rod frame fixed to the plug rod is provided between the left and right sides of the slide.

[0012] A further preferred embodiment: The upper end and front end of the side foot seat are both provided with slot structures for limiting and fixing.

[0013] The beneficial effects of this utility model are:

[0014] This type of artificial weather modification catalyst launch adjustment platform features a base with a bearing structure connecting a fixed end rail frame to a laterally extending side foot structure. The bearing seat connects the support shaft and the elevation angle end of the rail frame via dual-axle wheels. Axial rotation adjusts the relative elevation angle between the rail frame and the platform. While meeting structural adjustment requirements, the laterally fixed side foot structure limits the position of the dual-axle wheels along the support shaft. The position of the side foot platform indirectly suspends the dual-axle wheels, thus limiting and supporting the rail frame structure fixed at the other end of the dual-axle wheels. Combined with the fixed plane of the platform and the vehicle-mounted structure, this simultaneously supports and fixes the adjustment structure. Compared to traditional adjustment platforms, this improves the stability and overall structural strength of the adjustment structure, making it suitable for catalyst launch adjustment in complex scenarios. Attached Figure Description

[0015] The present invention will be further described below with reference to the accompanying drawings.

[0016] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0017] Figure 2 This is a schematic diagram of the rail frame and mounting rail plate structure of this utility model;

[0018] Figure 3 This is a schematic diagram of the internal planar structure of the base of this utility model.

[0019] Figures 1-3 In the middle: 1. Base, 2. Side foot seat, 3. Platform plate, 4. Rail frame, 5. Mounting rail plate, 6. Slide table, 7. Angle shaft seat, 8. Adjusting shaft, 9. Displacement slide tube, 10. Connecting rod frame, 11. Insert rod, 12. Support shaft, 13. Double shaft wheel, 14. Bearing seat. Detailed Implementation

[0020] To better understand the above-mentioned objectives, features, and advantages of this utility model, the following description is provided in conjunction with the accompanying drawings. Figures 1-3 The present invention will be further described in detail below with specific embodiments. The following embodiments are merely examples for implementing the present invention. It must be noted that the disclosed embodiments do not limit the scope of the present invention. On the contrary, any modifications and refinements made without departing from the scope of the present invention are within the patent protection scope of the present invention.

[0021] A weather modification catalyst launch and adjustment platform includes a base 1, on which a pair of corner bearings 7 are embedded. The two corner bearings 7 are connected to the base 1 by bearing seats 14. A double-shaft wheel 13 extends outward from one end of the corner bearing 7 relative to the bearing seat 14. Two coaxial shafts extend outward from the outer side of the double-shaft wheel 13. One shaft is fixed with a support shaft 12, and the other shaft passes through the outer side of the corner bearing 7 and is fixedly mounted with a rail frame 4.

[0022] The rail frame 4 has a groove with a custom-made toothed interval size. The mounting rail plate 5 is slidably fitted in the groove. The mounting rail plate 5 has a matching slide table 6 on the groove. The inner end of the mounting rail plate 5 is fixed with an adjusting shaft 8. A hydraulic groove is left between the end of the adjusting shaft 8 and the rail frame 4.

[0023] A side foot seat 2 is fixedly installed on the outer side of the support shaft 12;

[0024] In this artificial weather modification catalyst launcher, the platform 1 serves as a base platform, and its bottom surface is assembled and fixed to the vehicle structure by bolting. The rail frame 4 and the outwardly extending mounting rail plate 5 serve as the mounting platform for the catalyst launcher. The angle between the angle bearing 7 and the inner angle between the rail frame 4 and the platform surface of the platform 1 is adjusted by the hinged rotation of the angle bearing 7 on the bearing seat 14, that is, the elevation angle between the launcher on the mounting rail plate 5 and the platform surface of the platform 1 is adjusted.

[0025] Specifically, during adjustment, the bearing seat 14 and the angle shaft seat 7 are mainly connected by the transmission between the bearing seat 14 and the double shaft wheel 13 to achieve the hinged movement of the angle shaft seat 7. The bearing seat 14 and the double shaft wheel 13 are adjusted by rotating the external motor shaft based on the wheel and axle structure. The adjustment end uses the angle shaft seat 7 as the bearing. The relative rotation angle of the double shaft wheel 13 in the angle shaft seat 7 is linked with the rotation of the angle shaft seat 7. That is, during adjustment, if the angle shaft seat 7 is turned to 30°, the two ends of the shaft of the opposite double shaft wheel 13 drive the rail frame 4 to rotate relative to each other by 30°. The other end is simultaneously adjusted by rotating the support shaft 12 to adjust the relative angle of the external side foot seat 2. After the angle is determined, the side foot seat 2 is fixed by bolting the external structure to suspend and fix the angle of the support shaft 13, that is, to limit the angle between the double shaft wheel 13 and the angle shaft seat 7.

[0026] In this adjustment platform, the mounting rail plate 5 extending to the end of the rail frame 4 serves as the loading structure for the catalytic launcher. The mounting rail plate 5 has several bolt holes for docking and fixing the frame structure. The mounting rail plate 5 can slide axially along the slide groove of the rail frame 4. The sliding structure is based on hydraulic feeding. The adjustment shaft 8 is pushed outward along the direction of the hydraulic groove by feeding into the hydraulic groove of the rail frame 4 through an external hydraulic pump. With the guidance of the slide table 6, the length of the mounting rail plate 5 relative to the rail frame 4 is adjusted along the slide groove, that is, the height of the launcher on the mounting rail plate 5 is adjusted.

[0027] Compared to traditional launcher adjustment platform structures, this adjustment platform is based on a fixed platform structure and vehicle-mounted structure, with the fixed end of the platform serving as a counterweight end. During subsequent adjustment activities, the external side feet 2 are further fixed to limit the elevation angle of the rail frame 4 in conjunction with the internal axial structure. Together with the platform surface of the base 1, the launcher is limited and fixed. While ensuring structural strength, the lateral limiting structure, together with the platform surface of the base 1, can effectively support the elevation angle load of the launcher, and the overall stability of the adjustment structure is improved by limiting the elevation angle.

[0028] Furthermore, two platform plates 3 that match the rail frame 4 are extended from the end of the platform surface of the pedestal 1. The platform plates 3 extend the platform surface of the pedestal 1 to expand the fixing surface between the platform surface of the pedestal 1 and the vehicle structure, thereby improving the stability of the entire platform structure of the pedestal 1.

[0029] Based on the above, the platform plate 3 is fixed to the bottom surface of the support shaft 12 and the corner shaft seat 7. The platform plate 3 and the rail frame 4 are combined to form a shear arm structure with a relatively matched length. With the bidirectional support at the end of the corner shaft seat 7, the bottom surface of the support shaft 12 is effectively supported, which further expands the support structure strength of the rail frame 4 and improves the overall stability of the adjustment platform.

[0030] Furthermore, a displacement slide tube 9 is sleeved on the adjusting shaft 8, and a displacement sensor that matches the slide groove of the rail frame 4 is rolled on the displacement slide tube 9. The displacement amount of the adjusting shaft 8 during the advance displacement can be recorded and fed back by the extended displacement slide tube 9. By matching the displacement of the rolling end of the displacement sensor with the toothed displacement of the slide groove of the rail frame 4, the number of rotations of the displacement sensor reflects the toothed displacement of the slide groove. That is, the advance stroke of the displacement slide tube 9 along with the entire adjusting shaft 8 is fed back, which makes it convenient for the staff to make precise adjustments by the feedback displacement of the hydraulic pump equipment and control terminal.

[0031] Furthermore, a plug rod 11 is inserted into the slide 6, and a connecting rod frame 10 fixed to the plug rod 11 is provided between the left and right slides 6 to expand the structure of the connecting rod frame 10 provided on the two slides 6 to connect the mounting rail frame 5 laterally. The bolt holes on the connecting rod frame 10 are used as the lateral frame assembly structure of the launcher. While fixing the mounting rail frame 5 to the launcher, the stability of the mounting rail frames 5 on the left and right sides is improved.

[0032] Based on the above, both the upper and front ends of the side foot base 2 are provided with slot structures for limiting and fixing, such as... Figure 1 , 3 As shown, after the side foot seat 2 reaches the specified angle position during the adjustment process, the slot structure at the end can be bolted and fixed to the external frame. The fixing of the end of the side foot seat 2 can limit the side foot seat 2 in multiple directions, which facilitates the adjustment of the fixed position of the side foot seat 2.

[0033] Working principle:

[0034] The adjustment seat uses the flat ends of the base 1 and platform plate 3 as bolted and fixed ends to the vehicle structure, and the mounting rail plate 5 and the connecting rod frame 10 set above as bolted and fixed ends to the catalyst launcher. Before installation, when adjusting the elevation angle of the launcher, the relative rotation angle of the angle shaft seat 7 and bearing seat 14 can be adjusted by an external motor or by turning with tools. When the rotation angle changes, the rotation of both ends of the double shaft wheel 13 will synchronously drive the tilt angle of the rail frame 4 and the side foot seat 2 to change. Then, the position of the side foot seat 2 is bolted and fixed by the external frame, thereby fixing the elevation angle of the other end of the rail frame 4. At the same time, when adjusting the relative height of the launcher on the mounting rail plate 5, the external hydraulic pump equipment feeds into the hydraulic groove of the rail frame 4 to push the adjustment shaft 8 outward along the slide groove of the rail frame 4, and simultaneously causes the mounting rail plate 5 to make relative displacement along the slide groove of the rail frame 4. During the process, the displacement sensor on the displacement tube 9 rolls on the groove teeth to record and feedback the amount of pushing displacement, which is used by the staff to make precise adjustments based on the data.

[0035] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of this utility model and are not intended to limit it. Although this utility model has been described in detail with reference to preferred embodiments, those skilled in the art should understand that modifications or equivalent substitutions can be made to the technical solutions of this utility model without departing from the spirit and scope of the technical solutions of this utility model, and all such modifications or substitutions should be covered within the scope of the claims of this utility model.

Claims

1. A weather modification catalyst emission control platform, comprising a platform (1), characterized in that: A pair of corner bearings (7) are fitted on the pedestal (1). The two corner bearings (7) are connected to the pedestal (1) by a bearing seat (14). A double axle wheel (13) extends outward from one end of the corner bearing (7) relative to the bearing seat (14). The double axle wheel (13) extends outward to form two coaxial shafts. One shaft is fixed with a support shaft (12), and the other shaft passes through the outside of the corner bearing (7) and is fixedly mounted with a rail frame (4). The rail frame (4) has a groove with a custom toothed interval size, and a mounting rail plate (5) is slidably fitted in the groove. The mounting rail plate (5) has a matching slide table (6) on the groove, and an adjusting shaft (8) is fixed at the inner end of the mounting rail plate (5). A hydraulic groove is left between the end of the adjusting shaft (8) and the rail frame (4). A side foot seat (2) is fixedly installed on the outside of the support shaft (12).

2. The weather modification catalyst emission control station according to claim 1, characterized in that: The platform (1) extends to form two platform plates (3) that match the rail frame (4) at the end of the platform surface.

3. A weather modification catalyst launching control station according to claim 2, wherein: The platform plate (3) is fixed to the bottom surface of the support shaft (12) and the corner shaft seat (7).

4. The weather modification catalyst launch control pad of claim 1, wherein: The adjustment shaft (8) is sleeved with a displacement slide tube (9), and a displacement sensor matching the slide groove of the rail frame (4) is rolled on the displacement slide tube (9).

5. The weather modification catalyst emission control station according to claim 1, characterized in that: A rod (11) is inserted into the slide (6), and a connecting rod frame (10) fixed to the rod (11) is provided between the left and right sides of the slide (6).

6. The weather modification catalyst emission control station according to claim 1, characterized in that: The upper end and front end of the side foot seat (2) are provided with slot structures for limiting and fixing.

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