CN111220023A - Self-adaptive artificial precipitation hail-suppression rocket launcher and control system - Google Patents
Self-adaptive artificial precipitation hail-suppression rocket launcher and control system Download PDFInfo
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- CN111220023A CN111220023A CN202010163762.9A CN202010163762A CN111220023A CN 111220023 A CN111220023 A CN 111220023A CN 202010163762 A CN202010163762 A CN 202010163762A CN 111220023 A CN111220023 A CN 111220023A
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- 238000001556 precipitation Methods 0.000 title claims abstract description 20
- 230000001629 suppression Effects 0.000 claims abstract description 20
- 230000007246 mechanism Effects 0.000 claims abstract description 19
- 238000009434 installation Methods 0.000 claims description 12
- 230000003044 adaptive effect Effects 0.000 claims description 9
- 238000011161 development Methods 0.000 description 5
- 230000008859 change Effects 0.000 description 3
- 238000000034 method Methods 0.000 description 3
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- 230000004888 barrier function Effects 0.000 description 2
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
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- A—HUMAN NECESSITIES
- A01—AGRICULTURE; FORESTRY; ANIMAL HUSBANDRY; HUNTING; TRAPPING; FISHING
- A01G—HORTICULTURE; CULTIVATION OF VEGETABLES, FLOWERS, RICE, FRUIT, VINES, HOPS OR SEAWEED; FORESTRY; WATERING
- A01G15/00—Devices or methods for influencing weather conditions
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Abstract
The invention discloses a self-adaptive artificial precipitation and hail suppression rocket launcher and a control system, which comprise a plurality of large orbit groups, wherein each large orbit group comprises a first orbit, a second orbit and a small orbit group positioned between the first orbit and the second orbit, each small orbit group comprises a third orbit and a fourth orbit, the cross sections of the third orbit and the fourth orbit are U-shaped, the axes of the third orbit and the fourth orbit are parallel, and openings of the third orbit and the fourth orbit are opposite; the small track group is connected with an adjusting mechanism, and the adjusting mechanism adjusts the distance between the third track and the fourth track under the driving of the driving device. Through on original launcher basis, increased a set of adjustable little track group on every track group, through adopting two sets of big or small track groups, big track group fixes the specification, and little track group is adjustable specification, realizes the fixed mounting of the rainfall bullet of various specifications, so, use a launcher alright general when going out the operation, solve current rainfall bullet launcher and used inconvenient problem to the rainfall bullet of fixed specification.
Description
Technical Field
The invention belongs to a rainfall bomb launcher, and particularly relates to a self-adaptive artificial rainfall enhancement and hail suppression rocket launcher and a control system.
Background
At present, weather-influenced (hereinafter referred to as 'figure') operation rocket projectiles and launching frames are various in types, different in form, more and more complex and long-term, form figure equipment industry barriers and local monopoly gradually, and are not beneficial to further development of the whole figure industry. In order to break through the situation, the discussion of realizing standardization and universalization of the rocket launcher and further realizing separation of the missile launcher in the whole figure industry has been long, and the universal rocket launcher has not been popularized in the ground for various reasons. In order to break the situation of ridge breaking and industry barriers of the figure equipment and the magazine rack, the magazine rack separation needs to be promoted, and the aim of more rapid development of the figure industry is promoted.
In order to solve the problems of various rocket projectiles and launching frames, different standards, large volume, heavy weight, large potential safety hazard, low operation efficiency and the like in the current figure operation, a standardized universal rocket launching frame is developed to serve the figure career.
Disclosure of Invention
The invention provides a self-adaptive artificial precipitation enhancement and hail suppression rocket launcher and a control system, and solves the problems that the existing rainfall bomb launcher is inconvenient to use for rainfall bombs with fixed specifications in the face of rainfall bombs with various specifications along with the development of the rainfall bombs, and only one specification of rainfall bomb launcher is generally carried in one-time outgoing operation, so that the rainfall bombs with other specifications are inconvenient to replace after going out.
The technical scheme adopted by the invention is as follows:
the self-adaptive artificial precipitation hail-suppression rocket launcher comprises a plurality of large orbit groups, wherein the large orbit groups are fixed on a frame; the large track group comprises a first track and a second track with U-shaped cross sections, the axes of the first track and the second track are parallel, the openings of the first track and the second track are opposite, the large track group also comprises a small track group positioned between the first track and the second track, the small track group comprises a third track and a fourth track with U-shaped cross sections, and the axes of the third track and the fourth track are parallel, and the openings of the third track and the fourth track are opposite; the small track group is connected with an adjusting mechanism, and the adjusting mechanism adjusts the distance between the third track and the fourth track under the driving of the driving device. On the basis of the original launcher, a group of adjustable small track groups is added on each track group, so that when the rain bomb with the largest size is used, the large track group is adopted for installing the rain bomb; when the smaller rainfall bombs with other specifications are used, the small track group is adopted for fixed installation of rainfall, two groups of large and small track groups are adopted, the large track group is in fixed specifications, the small track group is in adjustable specifications, and fixed installation of the rainfall bombs with various specifications is realized.
According to the technical preference, the adjusting mechanism comprises a moving assembly, the moving assembly is connected with the large track group in a sliding mode, and the axis of the sliding track is parallel to the axis of the large track group; the moving assembly is connected with the small track group in a sliding mode, an included angle is formed between the sliding track and the axis of the small track group, the small track group is located between the limiting mechanisms, and the limiting mechanisms are used for limiting the small track group not to displace in the moving direction of the moving assembly; so that the small track group moves longitudinally in the sliding track with the included angle when the moving assembly translates on the large track group. The moving assembly comprises a lower moving piece and an upper moving piece; the lower moving part is installed at the bottom of the first rail through a plurality of lower installation parts, and the upper moving part is installed at the top of the second rail through a plurality of upper installation parts which are in mirror symmetry with the lower installation parts. The large track group is used as a fixed base, the large track group is fixedly connected to the frame and does not move, the moving assembly is limited to move along the horizontal direction, the moving assembly is connected with the small track group in a sliding mode, the sliding track and the axis of the small track group form an included angle in mirror symmetry, and the small track group is located between limiting mechanisms for limiting the small track group not to displace in the moving direction of the moving assembly; when the moving assembly moves on the large track group in a translation mode, the two tracks of the small track group move along or away from each other, and the change adjustment of the small tracks is achieved.
According to the above technical preference, the lower mounting portion includes a moving member first mounting plate, a moving member second mounting plate, and a moving member attaching projection; the moving member first mounting plate and the moving member second mounting plate are arranged in parallel and symmetrically on two sides of the bottom of the first rail; a first sliding rail is arranged on the first mounting plate of the moving part; a second sliding rail is arranged on the second mounting plate of the moving part; the first sliding track and the second sliding track are parallel to the axis of the first track;
the bottom of the first rail is provided with a first limiting hole; the bottom of the third rail is provided with a moving part connecting bulge; the moving piece connecting bulge is positioned in the first limiting hole; the moving piece connecting bulge is provided with a third sliding track; the third sliding rail and the axis of the third rail form an included angle, the lower moving part comprises a lower moving part A and a lower moving part B, a pushing shaft is arranged between the lower moving part A and the lower moving part B, and the pushing shaft is arranged in the first sliding rail, the third sliding rail and the second sliding rail in a penetrating mode. When the moving member moves, the limiting hole enables the moving member to be connected with the protruding moving direction in a fixed mode and move up and down, the third rail is driven to move up and down under the action of the oblique third sliding rail when the pushing rod moves horizontally, the structure on the fourth rail is in mirror symmetry with the structure on the third rail, the third rail and the fourth rail move in the opposite direction or move away from each other when moving, and the rainfall bombs with various diameter specifications are achieved.
According to the technical preference, the driving device comprises an electric push rod, the electric push rod is fixed on the frame, and the end part of a movable push rod of the electric push rod is fixedly connected with the moving assembly.
According to the technical preference, the electric push rod is connected with the moving assembly through the connecting frame and the plurality of pushing shaft connecting rods; the connecting frame is connected with the end part of a movable push rod of the electric push rod, and at least two pushing shaft connecting rods which are respectively positioned at the top and the bottom of the large track group are simultaneously and fixedly connected with the moving assembly and the connecting frame; each pushing shaft connecting rod is connected with the moving assembly.
According to the technical preference, the electric push rod is a three-way 1200 micro push rod.
The control system of the self-adaptive artificial precipitation and hail suppression rocket launcher comprises a code scanning terminal for reading rainfall bullet type number information and an electric push rod control unit in signal connection with the code scanning terminal. The two-dimensional code containing the specification information of the mark on the rainfall bomb is read through the code scanning terminal, the information is sent to the control unit of the electric push rod, and the control unit adjusts the electric push rod according to the specification information, so that the small track group is matched with the current rainfall bomb, self-adaptive adjustment is achieved, and practicability is enhanced.
The invention has the following advantages and beneficial effects:
1. the self-adaptive artificial precipitation enhancement hail suppression rocket launcher is characterized in that a group of adjustable small orbit groups are added on each orbit group on the basis of the original launcher, so that when the original largest specification rain bomb is used, the large orbit group is adopted to install the rain bomb; when smaller rainfall bombs of other specifications are used, the small track group is adopted for fixed installation of rainfall, and through the adoption of two groups of large and small track groups, the large track group is fixed in specification, and the small track group is adjustable in specification, the fixed installation of the rainfall bombs of various specifications is realized, so that the rainfall bombs can be universally used during outgoing operation, and the problem that the existing rainfall bomb launcher is inconvenient to use for the rainfall bombs of fixed specification in the face of the rainfall bombs of various specifications along with the development of the rainfall bombs, and generally only one specification of the rainfall bomb launcher is carried in one outgoing operation, so that the rainfall bombs of other specifications are inconvenient to replace after going out is solved;
2. the invention relates to a self-adaptive artificial precipitation hail suppression rocket launcher, which adopts a large orbit group as a fixed base, wherein the large orbit group is fixedly connected to a frame and does not move, and simultaneously limits a moving assembly to move along the horizontal direction; when the moving assembly moves on the large track group in a translation manner, the two tracks of the small track group move along or away from each other, so that the change adjustment of the small tracks is realized;
3. the control system of the self-adaptive artificial precipitation enhancement and hail suppression rocket launcher has the main functions of compatibly launching rocket projectiles of various types, realizing 'one-projectile multi-projectile' launching, and realizing one-time operation and quick filling of different projectile varieties by scanning two-dimensional codes; the launching frame is provided with the self-adaptive bullet seed orientator, so that the operation is convenient and fast; the tool-free design is adopted structurally, so that the launcher operating system can rapidly, efficiently, accurately and safely carry out artificial rain enhancement and hail suppression operation.
Drawings
The accompanying drawings, which are included to provide a further understanding of the embodiments of the invention and are incorporated in and constitute a part of this application, illustrate embodiment(s) of the invention and together with the description serve to explain the principles of the invention. In the drawings:
fig. 1 is a schematic view of the overall structure of the present invention.
Fig. 2 is an enlarged structural view of the lower half of the present invention.
Fig. 3 is an exploded view of the lower mounting portion of the present invention.
FIG. 4 is a schematic diagram of the right-view structure of the present invention.
Fig. 5 is a front view structural schematic diagram of the present invention.
Reference numbers and corresponding part names in the drawings:
1-large track group, 2-frame, 3-small track group, 4-moving assembly, 5-lower mounting part, 6-upper mounting part, 7-electric push rod, 8-connecting frame, 9-pushing shaft connecting rod, 10-pushing shaft, 101-first track, 102-second track, 301-third track, 302-fourth track, 401-lower moving part, 402-upper moving part, 4011-lower moving part A, 4012-lower moving part B, 501-moving part first mounting plate, 502-moving part second mounting plate, 503-moving part connecting boss, 5011-first sliding track, 5021-second sliding track, 5031-third sliding track.
Detailed Description
In order to make the objects, technical solutions and advantages of the present invention more apparent, the present invention is further described in detail below with reference to examples and accompanying drawings, and the exemplary embodiments and descriptions thereof are only used for explaining the present invention and are not meant to limit the present invention.
It should be understood that the terms first, second, etc. are used merely for distinguishing between descriptions and are not intended to indicate or imply relative importance. Although the terms first, second, etc. may be used herein to describe various elements, these elements should not be limited by these terms. These terms are only used to distinguish one element from another. For example, a first element could be termed a second element, and, similarly, a second element could be termed a first element, without departing from the scope of example embodiments of the present invention.
It should be understood that the term "and/or" herein is merely one type of association relationship that describes an associated object, meaning that three relationships may exist, e.g., a and/or B may mean: a exists alone, B exists alone, and A and B exist at the same time, and the term "/and" is used herein to describe another association object relationship, which means that two relationships may exist, for example, A/and B, may mean: a alone, and both a and B alone, and further, the character "/" in this document generally means that the former and latter associated objects are in an "or" relationship.
It is to be understood that in the description of the present invention, the terms "upper", "vertical", "inside", "outside", and the like, refer to an orientation or positional relationship that is conventionally used for placing the product of the present invention, or that is conventionally understood by those skilled in the art, and are used merely for convenience in describing and simplifying the description, and do not indicate or imply that the device or element referred to must have a particular orientation, be constructed in a particular orientation, and be operated, and therefore should not be considered as limiting the present invention.
It will be understood that when an element is referred to as being "connected," "connected," or "coupled" to another element, it can be connected or coupled to the other element or intervening elements may be present. In contrast, when an element is referred to as being "directly adjacent" or "directly coupled" to another element, there are no intervening elements present. Other words used to describe the relationship between elements should be interpreted in a similar manner (e.g., "between … …" versus "directly between … …", "adjacent" versus "directly adjacent", etc.).
In the description of the present invention, it should also be noted that, unless otherwise explicitly specified or limited, the terms "disposed," "mounted," and "connected" are to be construed broadly, e.g., as meaning fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.
The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of example embodiments of the invention. As used herein, the singular forms "a", "an" and "the" are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms "comprises," "comprising," "includes," and/or "including," when used herein, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, numbers, steps, operations, elements, components, and/or groups thereof.
Example 1:
as shown in fig. 1 and fig. 2, the present embodiment provides an adaptive artificial precipitation and hail suppression rocket launcher, comprising a plurality of large orbit groups 1, wherein a plurality of large orbit groups 1 are fixed on a frame 2; the large track group 1 comprises a first track 101 and a second track 102 with U-shaped cross sections, the axes of the first track 101 and the second track 102 are parallel, the openings of the first track 101 and the second track 102 are opposite, the large track group also comprises a small track group 3 positioned between the first track 101 and the second track 102, the small track group 3 comprises a third track 301 and a fourth track 302 with U-shaped cross sections, and the axes of the third track 301 and the fourth track 302 are parallel, and the openings of the third track 301 and the fourth track 302 are opposite; the small track group 3 is connected with an adjusting mechanism, and the adjusting mechanism adjusts the distance between the third track 301 and the fourth track 302 under the driving of the driving device.
In specific implementation, the adjusting mechanism comprises a moving assembly 4, the moving assembly 4 is connected with the large track group 1 in a sliding mode, and the sliding track is parallel to the axis of the large track group 1; the moving assembly 4 is connected with the small track group 3 in a sliding mode, and an included angle is formed between the sliding track and the axis of the small track group 3, so that the small track group 3 can move longitudinally when the moving assembly 4 translates on the large track group 1.
In specific implementation, as shown in fig. 3 and 4, the moving assembly 4 includes a lower moving member 401 and an upper moving member 402; the lower moving part 401 is mounted at the bottom of the first rail 101 by a plurality of lower mounting parts 5, and the upper moving part 402 is mounted at the top of the second rail 102 by a plurality of upper mounting parts 6 which are mirror-symmetrical to the plurality of lower mounting parts 5.
In specific implementation, as shown in fig. 3, the lower mounting portion 5 includes a moving member first mounting plate 501, a moving member second mounting plate 502 and a moving member connecting protrusion; the moving member first mounting plate 501 and the moving member second mounting plate 502 are arranged in parallel and symmetrically on two sides of the bottom of the first rail 101; a first sliding rail 5011 is arranged on the moving member first mounting plate 501; a second sliding rail 5021 is arranged on the second mounting plate 502 of the moving part; the first sliding rail 5011 and the second sliding rail 5021 are parallel to the axis of the first rail 101;
the bottom of the first rail 101 is provided with a first limiting hole; a moving member connecting bulge 503 is arranged at the bottom of the third rail 301; the moving member connecting projection 503 is located in the first limit hole; the moving member connecting projection 503 is provided with a third slide rail 5031; the third sliding rail 5031 forms an included angle with the axis of the third rail 301, the lower moving part 401 includes a lower moving part a4011 and a lower moving part B4012, a pushing shaft 10 is disposed between the lower moving part a4011 and the lower moving part B4012, and the pushing shaft 10 is disposed in the first sliding rail 5011, the third sliding rail 5031 and the second sliding rail 5021 in a penetrating manner.
In specific implementation, as shown in fig. 2, the driving device includes an electric push rod 7, the electric push rod 7 is fixed on the frame 2, and a movable push rod end of the electric push rod 7 is fixedly connected to the moving assembly 4. In specific implementation, the driving device can be set to be driven manually.
In specific implementation, the electric push rod 7 is connected with the moving assembly 4 through a connecting frame 8 and a plurality of push shaft connecting rods 9; the connecting frame 8 is connected with the end part of a movable push rod of the electric push rod 7, and at least two pushing shaft connecting rods 9 respectively positioned at the top and the bottom of the large track group 1 are fixedly connected with the moving assembly 4 and the connecting frame 8; each push shaft link 9 is connected to the moving assembly 4.
In specific implementation, the electric push rod 7 is a three-way 1200 micro push rod.
In specific implementation, in order to realize the function of one multi-bullet, two groups of tracks are arranged, and the large track corresponds to a rocket bullet with a bullet diameter of 82 mm. The small tracks correspondingly launch rocket projectiles with the projectile diameters of 44mm, 56mm and 66mm, and the adaptation to different projectile diameters is realized by adjusting the distance between the small track groups. Therefore, the mechanism is essentially suitable for adjusting the distance between the upper U-shaped groove and the lower U-shaped groove of the small track set.
Example 2:
the control system of the adaptive artificial precipitation and hail suppression rocket launcher in embodiment 1 comprises a code scanning terminal for reading rainfall bullet type information, and an electric push rod 7 control unit in signal connection with the code scanning terminal. In specific implementation, the diameter of the launching track is adjusted in a self-adaptive mode by scanning the bullet type information and the self-adaptive bullet type adjusting mechanism. The operating personnel scans the rocket projectile two-dimensional code through the launch controller, acquires bullet kind information and sends into servo, and servo drives electric putter adjustment launch track to corresponding bullet kind diameter state. And after the adjustment is finished, automatically locking. The operating personnel push the rocket projectile into the launching track, and the projectile piece of the projectile blocking device can automatically block the tail wing of the rocket projectile. If the bullet-blocking device elastic sheet cannot automatically rebound due to an accident, the rocket projectile cannot be blocked, and at the moment, an operator needs to manually stir the bullet-blocking device elastic sheet to block the projectile tail wing. The process from the process of collecting the bomb and scanning the code to the process of loading the bomb is designed and controlled within 30 seconds.
In conclusion, the self-adaptive artificial rainfall enhancement and hail suppression rocket launcher is characterized in that a group of adjustable small orbit groups is added on each orbit group on the basis of the original launcher, so that when the original largest-size rainfall bomb is used, the large orbit group is adopted for installing the rainfall bomb; when smaller rainfall bombs of other specifications are used, the small track group is adopted for fixed installation of rainfall, and through the adoption of two groups of large and small track groups, the large track group is fixed in specification, and the small track group is adjustable in specification, the fixed installation of the rainfall bombs of various specifications is realized, so that the rainfall bombs can be universally used during outgoing operation, and the problem that the existing rainfall bomb launcher is inconvenient to use for the rainfall bombs of fixed specification in the face of the rainfall bombs of various specifications along with the development of the rainfall bombs, and generally only one specification of the rainfall bomb launcher is carried in one outgoing operation, so that the rainfall bombs of other specifications are inconvenient to replace after going out is solved; the self-adaptive artificial precipitation hail suppression rocket launcher adopts the large orbit group as a fixed base, the large orbit group is fixedly connected to the frame and does not move, the large orbit group limits the movement of the moving assembly along the horizontal direction, the moving assembly is connected with the small orbit group in a sliding manner, the sliding orbit and the axis of the small orbit group form a mirror symmetry included angle, and the small orbit group is positioned between limiting mechanisms which limit the small orbit group not to displace in the moving direction of the moving assembly; when the moving assembly moves on the large track group in a translation manner, the two tracks of the small track group move along or away from each other, so that the change adjustment of the small tracks is realized;
the two-dimensional code containing the specification information of the mark on the rainfall bomb is read through the code scanning terminal, the information is sent to the control unit of the electric push rod, and the control unit adjusts the electric push rod according to the specification information, so that the small track group is matched with the current rainfall bomb, self-adaptive adjustment is achieved, and practicability is enhanced.
The above-mentioned embodiments are intended to illustrate the objects, technical solutions and advantages of the present invention in further detail, and it should be understood that the above-mentioned embodiments are merely exemplary embodiments of the present invention, and are not intended to limit the scope of the present invention, and any modifications, equivalent substitutions, improvements and the like made within the spirit and principle of the present invention should be included in the scope of the present invention.
Claims (8)
1. Self-adaptation formula artificial precipitation hail suppression rocket mount, its characterized in that: the large track system comprises a plurality of large track groups (1), wherein the large track groups (1) are fixed on a frame (2); the large track group (1) comprises a first track (101) and a second track (102) which are U-shaped in cross section, and the axes of the first track (101) and the second track (102) are parallel and are oppositely opened; a small track group (3) is arranged between the first track (101) and the second track (102), the small track group (3) comprises a third track (301) and a fourth track (302) which are U-shaped in cross section, and the axes of the third track (301) and the fourth track (302) are parallel and are oppositely opened; the small track group (3) is connected with an adjusting mechanism, and the adjusting mechanism adjusts the distance between the third track (301) and the fourth track (302) under the driving of the driving device.
2. The adaptive artificial precipitation hail suppression rocket launcher according to claim 1, wherein: the adjusting mechanism comprises a moving assembly (4), the moving assembly (4) is connected with the large track group (1) in a sliding mode, and the sliding track is parallel to the axis of the large track group (1); the moving assembly (4) is connected with the small track group (3) in a sliding mode, an included angle is formed between the sliding track and the axis of the small track group (3), the small track group (3) is located between the limiting mechanisms, and the limiting mechanisms are used for limiting the small track group (3) not to displace in the moving direction of the moving assembly (4); so that the small track group (3) moves longitudinally in the sliding track with the included angle when the moving component (4) translates on the large track group (1).
3. The adaptive artificial precipitation hail suppression rocket launcher according to claim 2, wherein: the moving assembly (4) comprises a lower moving piece (401) and an upper moving piece (402); the lower moving piece (401) is installed at the bottom of the first rail (101) through a plurality of lower installation parts (5), and the upper moving piece (402) is installed at the top of the second rail (102) through a plurality of upper installation parts (6) which are in mirror symmetry with the lower installation parts (5).
4. The adaptive artificial precipitation hail suppression rocket launcher according to claim 3, wherein: the lower mounting part (5) comprises a moving member first mounting plate (501), a moving member second mounting plate (502) and a moving member connecting bulge; the moving member first mounting plate (501) and the moving member second mounting plate (502) are arranged on two sides of the bottom of the first rail (101) in parallel and symmetrically; a first sliding rail (5011) is arranged on the first mounting plate (501) of the moving part; a second sliding rail (5021) is arranged on the second mounting plate (502) of the moving part; the first sliding rail (5011) and the second sliding rail (5021) are parallel to the axis of the first rail (101);
the bottom of the first rail (101) is provided with a first limiting hole; a moving member connecting bulge (503) is arranged at the bottom of the third rail (301); the moving piece connecting bulge (503) is positioned in the first limiting hole; the moving member connecting projection (503) is provided with a third sliding rail (5031); the third sliding rail (5031) and the axis of the third rail (301) form an included angle, the lower moving part (401) comprises a lower moving part A (4011) and a lower moving part B (4012), a pushing shaft (10) is fixedly arranged between the lower moving part A (4011) and the lower moving part B (4012), and the pushing shaft (10) penetrates through the first sliding rail (5011), the third sliding rail (5031) and the second sliding rail (5021).
5. The adaptive artificial precipitation hail suppression rocket launcher according to claim 2, wherein: the driving device is an electric push rod (7), the electric push rod (7) is fixed on the frame (2), and the end part of a movable push rod of the electric push rod (7) is fixedly connected with the moving assembly (4).
6. The adaptive artificial precipitation hail suppression rocket launcher according to claim 5, wherein: the electric push rod (7) is connected with the moving assembly (4) through a connecting frame (8) and a plurality of pushing shaft connecting rods (9); the connecting frame (8) is connected with the end part of a movable push rod of the electric push rod (7), and at least two pushing shaft connecting rods (9) which are respectively positioned at the top and the bottom of the large track group (1) are fixedly connected with the moving assembly (4) and the connecting frame (8) at the same time; each pushing shaft connecting rod (9) is connected with the moving component (4).
7. The adaptive artificial precipitation hail suppression rocket launcher according to claim 5, wherein: the electric push rod (7) is a three-way 1200 micro push rod.
8. The control system of the adaptive artificial precipitation and hail suppression rocket launcher according to any one of claims 1 to 7 is characterized in that: the rainfall bullet type number scanning device comprises a code scanning terminal used for reading rainfall bullet type number information and an electric push rod control unit in signal connection with the code scanning terminal.
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| CN202010163762.9A CN111220023B (en) | 2020-03-10 | 2020-03-10 | Self-adaptive artificial precipitation hail-suppression rocket launching frame and control system |
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| CN202010163762.9A CN111220023B (en) | 2020-03-10 | 2020-03-10 | Self-adaptive artificial precipitation hail-suppression rocket launching frame and control system |
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| CN111220023B CN111220023B (en) | 2024-05-03 |
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| CN111220023B (en) | 2024-05-03 |
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