CN106688744A - Novel artillery rainfall system - Google Patents
Novel artillery rainfall system Download PDFInfo
- Publication number
- CN106688744A CN106688744A CN201611240724.9A CN201611240724A CN106688744A CN 106688744 A CN106688744 A CN 106688744A CN 201611240724 A CN201611240724 A CN 201611240724A CN 106688744 A CN106688744 A CN 106688744A
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- CN
- China
- Prior art keywords
- pedestal
- expansion link
- support
- controller
- antiaircraft gun
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
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Classifications
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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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- Life Sciences & Earth Sciences (AREA)
- Atmospheric Sciences (AREA)
- Environmental Sciences (AREA)
- Spray Control Apparatus (AREA)
Abstract
The invention provides a novel artillery rainfall system. The novel artillery rainfall system comprises a support with an L-shaped structure, wherein the support is arranged on a first substrate; an opening of the support is upward; a first retractable rod is arranged between a long plate of the support and the first substrate; two ends of the first retractable rod are respectively hinged to the first substrate and the long plate; a second retractable rod is arranged between a short plate of the support and the first substrate; two ends of the second retractable rod are respectively hinged to the first substrate and the short plate; the first retractable rod and the second retractable rod are respectively connected with a controller arranged on the first substrate; the controller respectively controls a first driving mechanism and a second driving mechanism of the first retractable rod and the second retractable rod; the outer side of a position where the long plate is connected with the short plate is hinged to the first substrate; and the inner side wall of the long plate of the support is fixedly connected with an artillery transmitting mechanism. The novel artillery rainfall system is simple in structure and convenient to operate; and the transmitting angel of artillery can be adjusted automatically.
Description
Technical field
The invention belongs to rain maker technical field, more particularly, to a kind of new antiaircraft gun rainfall system.
Background technology
In the prior art, can be using rain making, rain making when weather is especially dried or has other demands
It is general use antiaircraft gun emitter to launch can be with the rain making bullet of rain making, the launch angle of rain making bullet is to closing again
Will, launch angle is different, and the region of rain making is just different.
The content of the invention
In view of this, the invention is directed to a kind of new antiaircraft gun rainfall system, to propose that one kind automatically adjusts hair
The antiaircraft gun rainer of firing angle degree.
To reach above-mentioned purpose, what the technical scheme of the invention was realized in：
A kind of new antiaircraft gun rainfall system, including the first pedestal, are provided with the support of L-type structure, support on the first pedestal
It is opening up, the outside of the long slab of support and the junction of short slab is hinged with the first pedestal, solid on the long slab madial wall of support
Antiaircraft gun trigger mechanism is connected to, the first expansion link is provided between long slab and the first pedestal, the two ends of the first expansion link are respectively with
One pedestal and long slab are hinged, and are provided with the second expansion link between short slab and the first pedestal, and the two ends of the second expansion link are respectively with
One pedestal and short slab are hinged, and the first expansion link and the second expansion link are connected with the controller being arranged on the first pedestal respectively, control
Device processed controls first drive mechanism and the second drive mechanism of the first expansion link and the second expansion link respectively.
Further, the lower end of first expansion link and the second expansion link is fixed on one end of support by flange, branch
The other end of frame is hinged with the first pedestal, and loop buffer structure is provided with the middle part of support.
Further, the first pedestal is spindle rotationally arranged on flat car, and the lower end middle part of the first pedestal is connected with rotation
Axle, rotary shaft is connected with flat car by bearing, rotary shaft through being connected with driven gear after flat car thereon, driven gear with
Driving gear is engaged, and driving gear is fixed on the output shaft of motor, and the motor is connected with controller.
Further, it is provided with counter at gun muzzle of the antiaircraft gun trigger mechanism.
Further, also including some precipitation collectors, the precipitation collector is evenly distributed on the artificial drop of needs
In the region of rain, precipitation collector is connected with director server, after director server is processed the signal of precipitation collector
Controller is sent to, signal transmission is given the first drive mechanism and the second drive mechanism by controller again.
Relative to prior art, a kind of new antiaircraft gun rainfall system described in the invention has the advantage that：
(1) the invention simple structure, convenient operation, can automatically adjust the launch angle of antiaircraft gun；
(2) the invention can be according to the number of rain making areal precipitation, the launch angle of adjust automatically antiaircraft gun.
Brief description of the drawings
The accompanying drawing for constituting the part of the invention is used for providing further understanding the invention, present invention wound
The schematic description and description made does not constitute the improper restriction to the invention for explaining the invention.
In accompanying drawing：
Fig. 1 is the structural representation of the invention embodiment；
Fig. 2 is the support and the structural representation of the first expansion link described in the invention embodiment；
Fig. 3 is the control principle drawing of the invention embodiment.
Description of reference numerals：
The pedestals of 1- first；101- rotary shafts；102- driven gears；2- supports；201- long slabs；202- short slabs；3- antiaircraft guns are sent out
Penetrate mechanism；The expansion links of 4- first；The expansion links of 5- second；6- bumper brackets；601- loop buffer structures；7- controllers；8- flat cars；
9- motors；901- driving gears；10- counters.
Specific embodiment
It should be noted that in the case where not conflicting, the feature in embodiment and embodiment in the invention can
To be mutually combined.
In the description of the invention, it is to be understood that term " " center ", " longitudinal direction ", " transverse direction ", " on ", D score,
The orientation or position relationship of the instruction such as "front", "rear", "left", "right", " vertical ", " level ", " top ", " bottom ", " interior ", " outward " are
Based on orientation shown in the drawings or position relationship, it is for only for ease of description the invention and simplifies description, rather than instruction
Or imply that the device or element of meaning with specific orientation, with specific azimuth configuration and operation, therefore must not be understood that
It is the limitation to the invention.Additionally, term " first ", " second " etc. are only used for describing purpose, and it is not intended that indicating
Or imply relative importance or the implicit quantity for indicating indicated technical characteristic.Thus, " first ", " second " etc. are defined
Feature can express or implicitly include one or more this feature.In the description of the invention, unless separately
It is described, " multiple " is meant that two or more.
, it is necessary to explanation, unless otherwise clearly defined and limited, term " is pacified in the description of the invention
Dress ", " connected ", " connection " should be interpreted broadly, for example, it may be fixedly connected, or be detachably connected, or integratedly
Connection；Can mechanically connect, or electrically connect；Can be joined directly together, it is also possible to be indirectly connected to by intermediary,
Can be two connections of element internal.For the ordinary skill in the art, can be by concrete condition understanding
State concrete meaning of the term in the invention.
Describe the invention in detail below with reference to the accompanying drawings and in conjunction with the embodiments.
As shown in Figures 1 to 3, a kind of new antiaircraft gun rainfall system, including the first pedestal 1, L-type is provided with the first pedestal 1
The support 2 of structure, opening up, the outside of the long slab 201 of support 2 and the junction of short slab 202 and first pedestal 1 of support 2
It is hinged.Antiaircraft gun trigger mechanism 3 is connected with the madial wall of long slab 201 of support 2, is provided between the pedestal 1 of long slab 201 and first
One expansion link 4, the two ends of the first expansion link 4 are hinged with the first pedestal 1 and long slab 201 respectively.The pedestal 1 of short slab 202 and first it
Between be provided with the second expansion link 5, the two ends of the second expansion link 5 are hinged with the first pedestal 1 and short slab 202 respectively.First expansion link 4
It is connected with the controller 7 being arranged on the first pedestal 1 respectively with the second expansion link 5, controller 7 controls the first expansion link 4 respectively
With first drive mechanism and the second drive mechanism of the second expansion link 5.As shown in Fig. 2 the first expansion link 4 and the second expansion link 5
Lower end one end of bumper bracket 6 is fixed on by flange, the other end of bumper bracket 6 is hinged with the first pedestal 1, bumper bracket 6
Middle part is provided with loop buffer structure 601.First pedestal 1 is spindle rotationally arranged on flat car 8, in the lower end of the first pedestal 1
Portion is connected with rotary shaft 101, and rotary shaft 101 is connected with flat car 8 by bearing, and rotary shaft 101 is consolidated thereon after passing through flat car 8
Driven gear 102 is connected to, driven gear 102 is engaged with driving gear 901, and driving gear 901 is fixed in the output shaft of motor 9
On, the motor 9 is connected with controller 7.Counter 10 is provided with gun muzzle of antiaircraft gun trigger mechanism 3.New antiaircraft gun rainfall system
System also includes some precipitation collectors, and precipitation collector is evenly distributed in the region for needing rain making, and precipitation is adopted
Storage is connected with director server, and director server is sent to controller 7, controller after the signal of precipitation collector is processed
Signal transmission is given the first drive mechanism and the second drive mechanism by 7 again.
The operation principle of the invention：
Controller 7 controls the first drive mechanism and the second drive mechanism, so as to control the first expansion link 4 and the second expansion link
5 stretch, then realizes the launch angle of adjustment antiaircraft gun trigger mechanism 3.The precipitation information that precipitation collector will be collected
Director server is sent to, after director server is by the signal transacting of precipitation collector, controller 7 is sent to, controller 7 is according to drop
The precipitation information of water flux gather device, the launch angle of adjustment antiaircraft gun trigger mechanism 3, so as to adjust the scope of rain making.Control
The startup of the controlled motor 9 of device processed 7, so as to realize that controller 7 controls the rotation of the first pedestal 1.
The preferred embodiment of the invention is the foregoing is only, creation is not intended to limit the invention, it is all at this
Within the spirit and principle of innovation and creation, any modification, equivalent substitution and improvements made etc. should be included in the invention
Protection domain within.
Claims (5)
1. a kind of new antiaircraft gun rainfall system, it is characterised in that：Including the first pedestal (1), the first pedestal is provided with L-type on (1)
The support (2) of structure, support (2) it is opening up, the outside of the long slab (201) of support (2) and the junction of short slab (202) with
First pedestal (1) is hinged, and is connected with antiaircraft gun trigger mechanism (3) on long slab (201) madial wall of support (2), long slab (201) and the
(1) is provided with the first expansion link (4) between one pedestal, the two ends of the first expansion link (4) respectively with the first pedestal (1) and long slab
(201) it is hinged, the second expansion link (5), the two ends point of the second expansion link (5) is provided between short slab (202) and the first pedestal (1)
Be not hinged with the first pedestal (1) and short slab (202), the first expansion link (4) and the second expansion link (5) respectively be arranged on the first base
Controller (7) connection on seat (1), controller (7) controls the first drive of the first expansion link (4) and the second expansion link (5) respectively
Motivation structure and the second drive mechanism.
2. new antiaircraft gun rainfall system according to claim 1, it is characterised in that：First expansion link (4) and second
The lower end of expansion link (5) is fixed on one end of bumper bracket (6), other end and first pedestal (1) of bumper bracket (6) by flange
It is hinged, loop buffer structure (601) is provided with the middle part of bumper bracket (6).
3. new antiaircraft gun rainfall system according to claim 1, it is characterised in that：First pedestal (1) is rotatably set
On flat car (8), the lower end middle part of the first pedestal (1) is connected with rotary shaft (101), and rotary shaft (101) is led to flat car (8)
Cross bearing connection, rotary shaft (101) through being connected with driven gear (102) after flat car (8) thereon, driven gear (102) with
Driving gear (901) is engaged, and driving gear (901) is fixed on the output shaft of motor (9), the motor (9) and controller (7)
Connection.
4. new antiaircraft gun rainfall system according to claim 1, it is characterised in that：The big gun of the antiaircraft gun trigger mechanism (3)
Counter (10) is provided with mouthful.
5. new antiaircraft gun rainfall system according to claim 1, it is characterised in that：Also include some precipitation collectors,
The precipitation collector is evenly distributed in the region for needing rain making, and precipitation collector is connected with director server, always
Server is sent to controller (7) after the signal of precipitation collector is processed, controller (7) is again by signal transmission to the
One drive mechanism and the second drive mechanism.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611240724.9A CN106688744A (en) | 2016-12-29 | 2016-12-29 | Novel artillery rainfall system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611240724.9A CN106688744A (en) | 2016-12-29 | 2016-12-29 | Novel artillery rainfall system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106688744A true CN106688744A (en) | 2017-05-24 |
Family
ID=58895643
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611240724.9A Pending CN106688744A (en) | 2016-12-29 | 2016-12-29 | Novel artillery rainfall system |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106688744A (en) |
Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2316624Y (en) * | 1998-03-11 | 1999-04-28 | 中国航天工业总公司第四研究院第四十一研究所 | Raining hail-suppression rocket launching device |
| WO2005029942A1 (en) * | 2003-09-26 | 2005-04-07 | Jury Grigorievich Ishkov | Rain initiating method, in particular in summer time |
| CN101112163A (en) * | 2007-08-30 | 2008-01-30 | 济南卓信智能科技有限公司 | Weather modification communicating and directing device |
| CN201016649Y (en) * | 2006-10-23 | 2008-02-06 | 新疆维吾尔自治区人工影响天气办公室 | Multifunctional artificial hail-proof rain-increasing rocket pod and emission controller thereof |
| CN201028961Y (en) * | 2007-02-26 | 2008-02-27 | 江西钢丝厂 | Remote control emitting device for hail-suppression and rain-adding rocket projectile |
| CN103884236A (en) * | 2014-03-03 | 2014-06-25 | 浙江海洋学院 | Movable precipitation cannonball firing frame |
| CN204165457U (en) * | 2014-10-17 | 2015-02-18 | 太原融盛科技有限公司 | Rainfall-increasing and anti-hail rocket bullet emitter |
| CN104412879A (en) * | 2013-09-10 | 2015-03-18 | 中国兵器科学研究院 | Novel artificial influenced weather system designed by ordnance science institute of china |
| CN104412877A (en) * | 2013-09-10 | 2015-03-18 | 中国兵器科学研究院 | Full-automatic rocket system integrated with radar detection and integrated seeding |
| CN204831015U (en) * | 2015-06-26 | 2015-12-02 | 罗俊颉 | Precipitation of hail of rockets emitter operation information acquisition device and system |
| US20160165813A1 (en) * | 2014-12-10 | 2016-06-16 | The Boeing Company | Systems and methods of inducing rainfall |
| CN206481726U (en) * | 2016-12-29 | 2017-09-12 | 雷神科技（天津）有限公司 | One kind automatically adjusts antiaircraft gun rainer |
-
2016
- 2016-12-29 CN CN201611240724.9A patent/CN106688744A/en active Pending
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2316624Y (en) * | 1998-03-11 | 1999-04-28 | 中国航天工业总公司第四研究院第四十一研究所 | Raining hail-suppression rocket launching device |
| WO2005029942A1 (en) * | 2003-09-26 | 2005-04-07 | Jury Grigorievich Ishkov | Rain initiating method, in particular in summer time |
| CN201016649Y (en) * | 2006-10-23 | 2008-02-06 | 新疆维吾尔自治区人工影响天气办公室 | Multifunctional artificial hail-proof rain-increasing rocket pod and emission controller thereof |
| CN201028961Y (en) * | 2007-02-26 | 2008-02-27 | 江西钢丝厂 | Remote control emitting device for hail-suppression and rain-adding rocket projectile |
| CN101112163A (en) * | 2007-08-30 | 2008-01-30 | 济南卓信智能科技有限公司 | Weather modification communicating and directing device |
| CN104412879A (en) * | 2013-09-10 | 2015-03-18 | 中国兵器科学研究院 | Novel artificial influenced weather system designed by ordnance science institute of china |
| CN104412877A (en) * | 2013-09-10 | 2015-03-18 | 中国兵器科学研究院 | Full-automatic rocket system integrated with radar detection and integrated seeding |
| CN103884236A (en) * | 2014-03-03 | 2014-06-25 | 浙江海洋学院 | Movable precipitation cannonball firing frame |
| CN204165457U (en) * | 2014-10-17 | 2015-02-18 | 太原融盛科技有限公司 | Rainfall-increasing and anti-hail rocket bullet emitter |
| US20160165813A1 (en) * | 2014-12-10 | 2016-06-16 | The Boeing Company | Systems and methods of inducing rainfall |
| CN204831015U (en) * | 2015-06-26 | 2015-12-02 | 罗俊颉 | Precipitation of hail of rockets emitter operation information acquisition device and system |
| CN206481726U (en) * | 2016-12-29 | 2017-09-12 | 雷神科技（天津）有限公司 | One kind automatically adjusts antiaircraft gun rainer |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20170524 |