CN204165457U - Rainfall-increasing and anti-hail rocket bullet emitter - Google Patents
Rainfall-increasing and anti-hail rocket bullet emitter Download PDFInfo
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- CN204165457U CN204165457U CN201420602926.3U CN201420602926U CN204165457U CN 204165457 U CN204165457 U CN 204165457U CN 201420602926 U CN201420602926 U CN 201420602926U CN 204165457 U CN204165457 U CN 204165457U
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Abstract
A novel rainfall-increasing and anti-hail rocket bullet emitter, belongs to civilian meteorological control appliance field, and feature includes launching trajectory frame, pitching driving mechanism, rotary motion mechanism, tractor and control device.Floating bearing inner ring and base are fixed together, and are placed on the flat pad of tractor.Launching trajectory frame, pitching driving mechanism and rotary motion mechanism are arranged on floating bearing external toothing.Advantage is the mode adopting vehicular launcher, and conveniently moving is not subject to the restriction of time and region, operation mobility strong; Large-scale adjustment can be done in azimuth, the angle of site, without the need to being equipped with special purpose vehicle; Structure is simple, easy to adjust, can realize manual and automatic adjustment direction angle and the angle of site; Adopt the support floating bearing that engineering truck uses, deflection is easy to adjust, and Stability Analysis of Structures is reliable; Width-adjustable between guide rail, is applicable to dissimilar rainfall-increasing and anti-hail rocket bullet.
Description
Technical field
The utility model belongs to civilian meteorological control appliance field, is specifically related to a kind of rainfall-increasing and anti-hail rocket bullet emitter.
Background technology
At present, precipitation Rain enhancement hail prevention rocket launcher is that rocket projectile is transmitted into cloud layer suitable height according to predeterminated target, implements weather modification.Rainfall-increasing and anti-hail rocket emitter generally adopts the fixed launcher in ground and vehicular launcher two kinds of modes.Fixed launcher position, ground is fixed, and can not move, by the restriction of time and region, cloud layer follow the tracks of and operation mobility poor; Vehicular launcher, gyratory directions angle, orientation adjusting range is little, need be equipped with special purpose vehicle, and when non-operation, automobile inconvenience uses it for anything else.Existing precipitation Rain enhancement hail prevention rocket launcher complex structure, regulates inconvenience, quick adjustment cannot enter emission state to predetermined angular in official hour.Conformability for dissimilar rocket projectile is poor, and finder cannot regulate the width between guide rail.When Launch Operation, can not with extraneous real-time contacts and Long-distance Control, job parameter can not record automatically, without information network.
Summary of the invention
The utility model object is to provide a kind of novel rainfall-increasing and anti-hail rocket bullet emitter, can effectively solve prior art Problems existing.
The utility model realizes like this, and as shown in Figure 1, 2, its architectural feature includes launching trajectory frame 1, pitching driving mechanism 2, rotary motion mechanism 3, tractor 4 and control device 5.As shown in Figure 2, floating bearing inner ring 312 and base 302 are fixed together, and are placed on the flat pad 403 of tractor 4.On floating bearing external toothing 301, left and right is installed with pitching respectively and drives Connection Block 307 and launching trajectory frame Connection Block 309.Revolution drives worm reducer 305 and base 302 to be fixed together.Revolution drive motors 303 drives worm reducer 305 to drive the pinion 306 be meshed with floating bearing external toothing 301 to rotate by revolution.Revolution hand crank 311 drives worm reducer 305 to drive pinion 306 to rotate by the hand decelerator 304 of revolution and revolution.As shown in Figure 3, pitching driving mechanism 2 is driven back shaft 203 by pitching and is fixedly mounted on pitching and drives the pitching on Connection Block 307 to drive supporting seat 308 to be hinged.As shown in Figure 4, the rail bracket supporting seat 108 be fixed together with launching trajectory frame 1 end is hinged by bearing pin 313 and the transmitting supporting seat 310 be fixedly mounted on launcher Connection Block 309.As shown in Fig. 5,6,7, launching trajectory frame 1 is rectangular frame body, its horizontal end face includes the identical rocket bomb transmitting district 109 of n structure, n is whole even number, the end face structure in each rocket bomb transmitting district 109 is connected with the upper/lower guide supporting seat 103 be fixed on launching trajectory frame 1 respectively by adjustment bolt 104 by grooved, the laterally zygomorphic guide rail 102 that shoots, under shoot guide rail 102 rearward end backstop 105 is installed.Rocket projectile 106 is arranged on each rocket launching district 109 central part, shoots between guide rail 102 up and down.The longitudinal direction shooting guide rail 102 is up and down rocket bomb transmitting track, is provided with left and right launching trajectory frame supporting seat 108 in the end bottom of launching trajectory frame 1.Screw 110 is arranged on the middle bottom rail bracket by screw supporting seat 107.As shown in Fig. 2,8, pitching driving mechanism 2 drives back shaft 203 to be arranged on pitching driving supporting seat 308 by pitching, and pitching drives supporting seat 308 to be fixed on pitching and drives on Connection Block 307.Pitching drive motors 205 drives pitching to drive worm reducer 202 and drives leading screw 201 to rotate, and leading screw 201 screws mutually with the screw 110 be arranged on shoe frame 1.Pitching hand crank 206 drives worm reducer 202 to connect by the manual decelerator 204 of pitching with pitching.GPS module, 3G communication module, single-chip microcomputer and automatic recording instrument are installed in control device 5.
The utility model advantage and good effect are:
adopt the mode of vehicular launcher, conveniently moving, be not subject to the restriction of time and region, operation mobility strong;
large-scale adjustment can be done in azimuth, the angle of site, without the need to being equipped with special purpose vehicle;
structure is simple, easy to adjust, can realize manual and automatic adjustment direction angle and the angle of site;
adopt the support floating bearing that engineering truck uses, deflection is easy to adjust, and Stability Analysis of Structures is reliable;
width-adjustable between guide rail, is applicable to dissimilar rainfall-increasing and anti-hail rocket bullet;
adopt digitlization, informationization technology, the functions such as firepower control, emission control, information management, location are organically blended.When after the instruction of operator receiving command centre, determine the job parameters such as launcher azimuth, the angle of site.Automatic adjustment launcher, to shooting position and firing point, automatically detects launcher state, long-rangely realizes rocket projectile state-detection, realizes the task of single-shot or running fire rainfall-increasing and anti-hail rocket bullet;
be provided with GPS module in this device, the automatic recording parameters instrument of 3G communication module, single-chip microcomputer, rocket operation, it can realize data upload, and inquiry, makes its level of informatization greatly improve, and facilitate foundation and the management of user profile network.
accompanying drawing illustrates:
Fig. 1 is the utility model structural representation;
Fig. 2 is rotary motion mechanism schematic diagram;
Fig. 3 is F enlarged drawing in Fig. 1;
Fig. 4 is H enlarged drawing in Fig. 1;
Fig. 5 is launching trajectory shelf structure schematic diagram;
Fig. 6 is the A direction view in Fig. 1, i.e. the transverse end surface view of launching trajectory frame;
Fig. 7 is I portion enlarged drawing in Fig. 6;
Fig. 8 is pitching driving mechanism schematic diagram;
Fig. 9 is tractor structural representation;
Figure 10 is that motor drives and driven by shaking principle schematic.
In figure: 1-launching trajectory frame, 2-pitching driving mechanism, 3-rotary motion mechanism, 4-tractor, 5-control device, 102-shoot guide rail, 103-guide supporting seat, 104-adjustment bolt, 105-backstop, 106-rocket projectile, 107-screw supporting seat, 108-rail bracket supporting seat, 109-rocket bomb transmitting district, 110-screw, 201-leading screw, 202-pitching drives worm reducer, 203-pitching drives back shaft, the manual decelerator of 204-pitching, 205-pitching drive motors, 206-pitching hand crank, 301-floating bearing external toothing, 302-base, 303-revolution drive motors, 304-turn round hand decelerator, 305-revolution drives worm reducer, 306-pinion, 307-pitching drives Connection Block, 308-pitching drives supporting seat, 309-launcher Connection Block, 310-launcher supporting seat, 311-revolution hand crank, 312-floating bearing inner ring, 313-bearing pin, 401-wheel, 402-ground supports leg, 403-flat pad, 404-vehicle frame, 405-hook, 406-bracing frame, A-drive motors, B-turbine and worm decelerator, C-hand crank, D-decelerator.
detailed description of the invention:
As shown in Figure 1, when needs carry out artificial rain operation, the place set is hauled by increasing rain mill hail rocket bomb transmitting device, by the ground supports leg 402 on adjustment tractor 4 by tractor 4 and ground fixation, manipulating pitching by pitching drive motors 205 and pitching hand crank 206 drives worm reducer 202 to drive leading screw 201 to rotate, realize regulating launching trajectory frame 1 namely to shoot the elevation angle of guide rail 102, manipulating revolution by manipulation revolution drive motors 303 and revolution hand crank 311 again drives worm reducer 305 to drive floating bearing external toothing 301 to rotate, realize regulating launching trajectory frame 1 namely to shoot the adjustment of guide rail 102 anglec of rotation, location is reached up and down after angle adjustment, rainfall-increasing and anti-hail rocket bullet 106 is loaded in the middle of rocket launching district 109, shoot between guide rail 102 up and down, manipulated by control device 5 and launch.
Claims (1)
1. a rainfall-increasing and anti-hail rocket bullet emitter, its architectural feature includes launching trajectory frame (1), pitching driving mechanism (2), rotary motion mechanism (3), tractor (4) and control device (5); Floating bearing inner ring (312) and base (302) are fixed together, and are placed on the flat pad (403) of tractor (4); On floating bearing external toothing (301), left and right is installed with pitching respectively and drives Connection Block (307) and launching trajectory frame Connection Block (309); Revolution drives worm reducer (305) and base (302) to be fixed together, revolution drive motors (303) drives worm reducer (305) to drive the pinion (306) be meshed with floating bearing external toothing (301) to rotate by revolution, and revolution hand crank (311) drives worm reducer (305) to drive pinion (306) to rotate by the hand decelerator of revolution (304) and revolution; Pitching driving mechanism (2) is driven back shaft (203) by pitching and is fixedly mounted on pitching and drives the pitching on Connection Block (307) to drive supporting seat (308) to be hinged; The rail bracket supporting seat (108) be fixed together with launching trajectory frame (1) end is hinged by bearing pin (313) and the transmitting supporting seat (310) be fixedly mounted on launcher Connection Block (309); Launching trajectory frame (1) is rectangular frame body, its horizontal end face includes the identical rocket bomb transmitting district (109) of n structure, n is whole even number, the end face structure of each rocket bomb transmitting district (109) is connected with the upper/lower guide supporting seat (103) be fixed on launching trajectory frame (1) respectively by adjustment bolt (104) by grooved, the laterally zygomorphic guide rail (102) that shoots, under shoot guide rail (102) rearward end backstop (105) is installed; Rocket projectile (106) is arranged on each rocket launching district (109) central part, shoots between guide rail (102) up and down; The longitudinal direction shooting guide rail (102) is up and down rocket bomb transmitting track; In the end bottom of launching trajectory frame (1), left and right launching trajectory frame supporting seat (108) is installed; Screw (110) is arranged on the middle bottom rail bracket by screw supporting seat (107); Pitching driving mechanism (2) drives back shaft (203) to be arranged in pitching driving supporting seat (308) by pitching, and pitching drives supporting seat (308) to be fixed in pitching driving Connection Block (307); Pitching drive motors (205) drives pitching to drive worm reducer (202) and drives leading screw (201) to rotate, and leading screw (201) screws mutually with the screw (110) be arranged on shoe frame (1); Pitching hand crank (206) drives worm reducer (202) to connect by the manual decelerator of pitching (204) and pitching.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420602926.3U CN204165457U (en) | 2014-10-17 | 2014-10-17 | Rainfall-increasing and anti-hail rocket bullet emitter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420602926.3U CN204165457U (en) | 2014-10-17 | 2014-10-17 | Rainfall-increasing and anti-hail rocket bullet emitter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204165457U true CN204165457U (en) | 2015-02-18 |
Family
ID=52539138
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420602926.3U Withdrawn - After Issue CN204165457U (en) | 2014-10-17 | 2014-10-17 | Rainfall-increasing and anti-hail rocket bullet emitter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204165457U (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104315921A (en) * | 2014-10-17 | 2015-01-28 | 太原融盛科技有限公司 | Rain-increasing antihail rocket projectile launching device |
| CN105486172A (en) * | 2016-01-12 | 2016-04-13 | 中国人民解放军总参谋部工程兵科研三所 | Large-caliber supersonic-speed target missile launcher |
| CN106688744A (en) * | 2016-12-29 | 2017-05-24 | 雷神科技（天津）有限公司 | Novel artillery rainfall system |
| CN110530203A (en) * | 2019-08-08 | 2019-12-03 | 贵州航天特种车有限责任公司 | A kind of integrated emission system of self-propelled transmitting filling |
-
2014
- 2014-10-17 CN CN201420602926.3U patent/CN204165457U/en not_active Withdrawn - After Issue
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104315921A (en) * | 2014-10-17 | 2015-01-28 | 太原融盛科技有限公司 | Rain-increasing antihail rocket projectile launching device |
| CN104315921B (en) * | 2014-10-17 | 2015-10-28 | 太原融盛科技有限公司 | Rainfall-increasing and anti-hail rocket bullet emitter |
| CN105486172A (en) * | 2016-01-12 | 2016-04-13 | 中国人民解放军总参谋部工程兵科研三所 | Large-caliber supersonic-speed target missile launcher |
| CN106688744A (en) * | 2016-12-29 | 2017-05-24 | 雷神科技（天津）有限公司 | Novel artillery rainfall system |
| CN110530203A (en) * | 2019-08-08 | 2019-12-03 | 贵州航天特种车有限责任公司 | A kind of integrated emission system of self-propelled transmitting filling |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20150218 Effective date of abandoning: 20151028 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |