CN2316624Y - Raining hail-suppression rocket launching device - Google Patents
Raining hail-suppression rocket launching device Download PDFInfo
- Publication number
- CN2316624Y CN2316624Y CN 98201698 CN98201698U CN2316624Y CN 2316624 Y CN2316624 Y CN 2316624Y CN 98201698 CN98201698 CN 98201698 CN 98201698 U CN98201698 U CN 98201698U CN 2316624 Y CN2316624 Y CN 2316624Y
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- Prior art keywords
- rocket
- guide rail
- finder
- launching
- launcher
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- Expired - Lifetime
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- 230000005540 biological transmission Effects 0.000 claims abstract description 8
- 230000000694 effects Effects 0.000 claims description 3
- 238000001514 detection method Methods 0.000 abstract description 4
- 230000000903 blocking effect Effects 0.000 abstract 3
- 230000002349 favourable effect Effects 0.000 abstract 1
- 238000012360 testing method Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 4
- 238000003754 machining Methods 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000004020 conductor Substances 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000002411 adverse Effects 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000011161 development Methods 0.000 description 1
- 238000010304 firing Methods 0.000 description 1
- 239000003999 initiator Substances 0.000 description 1
- 238000007689 inspection Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 238000003466 welding Methods 0.000 description 1
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Abstract
A rain-increasing hail-suppression rocket launching device comprises a launching frame, a controller, a magnetic seat goniometer and the like, wherein the launching frame comprises one or more launching channels, each launching channel comprises a guide rail, a connecting frame, an ignition contact and an elastic blocking device, the two launching channels are connected together through a fastener, the ignition contact is located in the middle of the guide rail, the elastic blocking device is located at the tail of the guide rail, and the distance between the ignition contact and the elastic blocking device corresponds to the position of a rocket projectile-related ignition contact piece. The magnetic seat goniometer is used for accurately measuring the transmitting elevation angle, and the controller has the function of line safety detection besides the boosting transmitting function. The utility model discloses the transmission precision is high, and the operation is safe convenient, is favorable to catching the operation opportunity.
Description
The utility model belongs to the rocket above-ground launcher, is specifically related to a kind of rainfall-increasing and anti-hail rocket emitter.
The rainfall-increasing and anti-hail rocket emitter provides ignition energy by the basic demand of the supporting rocket of institute, and guarantees the directed safe emission of rocket.The JFJ type emitter that present domestic rainfall-increasing and anti-hail rocket emitter mainly contains the development of Yunnan 866 factories and produces, it structurally comprises launcher, exploder and other accessory, wherein launcher comprises finder, support body, parts such as angle indicating device.It has following deficiency:
1. the pointer of angle indicating device and finder are fastened together, dial and support body are fixed together, and will launch comparatively accurately like this, must carry out horizontal adjusting to launcher, otherwise the elevation angle of dial indication is false, and this will directly influence fire accuracy;
2. finder is by round steel or steel pipe aligning back welding fabrication, and machining accuracy is relatively poor, and the fit clearance of rocket projectile and launcher etc. be cannot say for sure to demonstrate,prove, and this also directly influences launch accuracy;
3. this emitter ignition circuit is a bundle conductor, bundle conductor one end is connected with junction box with exploder, and the other end is fixed on a certain position of launcher support body, after rocket loads, each ignitor electrode of rocket igniter needs the interim connection one by one respectively of operating personnel, and is dangerous;
4. the exploder of this emitter is the common quick-fried standard product of the people, only have and boost and emission function, when carrying out many pieces of rocket launching, every piece of rocket must once boost and firing operation, complicated operation, if indivedual mistakes that occur connect or connect not firm when circuit connects, be difficult in advance find, during emission not too safety also affect operation opportunity easily adversely.
The purpose of this utility model is to provide a kind of launch accuracy height, handling safety, reliable rainfall-increasing and anti-hail rocket emitter easily.
The utility model reaches by following measure: a kind of rainfall-increasing and anti-hail rocket emitter, comprise launcher, launcher comprises the support body of finder and supporting finder, it is characterized in that finder contains one or more transmission channels, each transmission channel comprises guide rail, guide rail is worked the connecting frame that connects positioning action, igniting contact and bomb retaining device etc., all link together between them by securing member, igniting contact is positioned at the middle part of guide rail, bomb retaining device is positioned at the afterbody of guide rail, the relevant igniting with rocket projectile of distance between the two contact position is corresponding, and bomb retaining device is in order to limiting the tram of rocket projectile in guide rail, and plays the effect of supporting rocket airframe, when rocket load put in place after, the igniting contact of rocket and the automatic conducting of igniting contact.
The utility model compared with prior art has following advantage:
1. launch accuracy height, the launcher finder all takes machining process to finish, and can guarantee necessary machining accuracy; Launching elevation adopts the magnetic support angular instrument to measure, can directly record finder angle with respect to the horizontal plane, thereby unnecessary launching site ground is carried out specially treated or launcher itself is carried out horizontal adjusting, can save the plenty of time, help catching operation opportunity.
2. easy-to-operate is saved manpower, and after rocket loaded and puts in place, the ignition circuit of rocket and emitter ignition circuit were connected automatically, need not to carry out the wiring operation, can avoid artificial wiring error; Whole device operation at most only needs 2 people to finish.
3. controller has the safety detection function, can find line fault early, and in time gets rid of, and helps catching operation opportunity.
Below in conjunction with drawings and Examples the utility model is further described.
Fig. 1 is that utility model is vertical or the structural representation of ground during surface launching;
Fig. 2 is that the utility model is horizontal or vehicle-mounted launcher structural representation;
Fig. 3 is a finder profile of the present utility model;
Fig. 4 is the testing circuit theory diagram of the utility model controller;
Fig. 5 is the testing circuit schematic diagram of the utility model controller.
Referring to accompanying drawing 1,2,3, launcher comprises the support body 6 of finder 5 and supporting finder, support body 6 among Fig. 2 is a car launcher, finder 5 contains one or more transmission channels, each transmission channel comprises guide rail 7, to 7 connecting frames 8 that connect positioning action of guide rail, igniting contact 9 and bomb retaining device 10, all link together between them by securing member, igniting contact 9 is positioned at the middle part of guide rail 7, bomb retaining device 10 is positioned at the afterbody of guide rail 7, the relevant ignition location with rocket projectile of distance between the two is corresponding, and bomb retaining device 10 is in order to limiting the tram of rocket projectile in guide rail 7, and plays the effect of supporting rocket airframe, when rocket load put in place after, the igniting contact of rocket and igniting contact 9 automatic conductings.
Referring to accompanying drawing 1,4; controller 2 joins by cable 3 and launcher; controller 2 is except that having the emission function of boosting; also has the function that line security detects; promptly before and after loading, rocket all can check device connection line state; so that discovery early and get rid of the fault or the problem of ignition circuit device, guarantee that rocket projectile launches under normal condition.Controller 2 comprises constant-current source 11 that joins with the emission circuit and the voltmeter 12 that joins with the constant-current source output, its will guarantee that on the one hand testing process works under little current status, to guarantee the security (can not mistakenly launch) of testing process because of detection makes rocket, detect electric current and can surpass 10mA in no instance, detect open-circuit voltage less than 1V (meeting national Initiator Safety examination criteria); Will guarantee detection line resistance accurately on the other hand, detected line resistance is converted into voltage signal by the 1mA constant-current source, and the input digit voltmeter shows that numerical value is the test line resistance value.
Referring to accompanying drawing 5, because of c, d both end voltage known and stable, therefore IR is stable, Iw is the quiescent current of voltage-stablizer 7805, is stationary value, so Ib is stable, hence one can see that, and I is a constant current, when emission circuit resistance variations, voltage-stablizer 7805 is kept constant current by the potential difference that changes a, c two ends, to guarantee the safety of testing process.
The utility model also comprises the magnetic support angular instrument 4 that can be adsorbed on the finder guide level at any time, be used to measure the finder elevation angle with respect to the horizontal plane.Magnetic support angular instrument 4 is the standard product, in the time of need carrying out the adjustment at the rocket launching elevation angle, the magnetic support angular instrument is adsorbed on the plane parallel of finder with transmit direction, because the pointer of magnetic support angular instrument is according to the design of weight principle, so total indicator reading indicates finder angle with respect to the horizontal plane all the time.
Operating process of the present utility model is, by designing requirement with the rocket projectile launcher of packing into, require to determine launching elevation according to meteorological condition, carry out the device wireline inspection, after circuit is normal, open the controller boosted switch, after voltage reaches the design launch requirements, by the emission knob, rocket just can normal transmission be gone out.
Claims (3)
1. a rainfall-increasing and anti-hail rocket emitter comprises launcher, launcher comprises the support body of finder and supporting finder, it is characterized in that: finder contains one or more transmission channels, each transmission channel comprises guide rail, guide rail is worked connecting frame, the igniting contact that connects positioning action and plays the bomb retaining device that supports the rocket airframe effect, all link together between them by securing member, igniting contact is positioned at the middle part of guide rail, bomb retaining device is positioned at the afterbody of guide rail, and the relevant igniting with rocket projectile of the distance between the two contact position is corresponding.
2. rainfall-increasing and anti-hail rocket emitter according to claim 1 is characterized in that: also comprise the controller that joins by cable 3 and launcher, this controller comprises and launches constant-current source that circuit joins and the voltmeter that joins with the constant-current source output.
3. rainfall-increasing and anti-hail rocket emitter according to claim 1 and 2 is characterized in that: also comprise being adsorbed on the finder guide level, being used to measure the finder magnetic support angular instrument at the elevation angle with respect to the horizontal plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 98201698 CN2316624Y (en) | 1998-03-11 | 1998-03-11 | Raining hail-suppression rocket launching device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 98201698 CN2316624Y (en) | 1998-03-11 | 1998-03-11 | Raining hail-suppression rocket launching device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2316624Y true CN2316624Y (en) | 1999-04-28 |
Family
ID=33958908
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 98201698 Expired - Lifetime CN2316624Y (en) | 1998-03-11 | 1998-03-11 | Raining hail-suppression rocket launching device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2316624Y (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104236389A (en) * | 2014-08-08 | 2014-12-24 | 西安航天化学动力厂 | Rain increasing and hail suppressing rocket launcher |
| CN106688744A (en) * | 2016-12-29 | 2017-05-24 | 雷神科技（天津）有限公司 | Novel artillery rainfall system |
| CN107907015A (en) * | 2017-11-07 | 2018-04-13 | 重庆长安工业(集团)有限责任公司 | People's rain rocket projectile contact copper sheet layout method |
| CN108151584A (en) * | 2018-01-08 | 2018-06-12 | 广州鼎飞科技有限公司 | Integral type rocket bomb transmitting cylinder and emitter |
| CN108414255A (en) * | 2017-12-07 | 2018-08-17 | 上海航天精密机械研究所 | A kind of push type firing mount separation simulation device |
| CN110887405A (en) * | 2019-11-27 | 2020-03-17 | 贵州航天特种车有限责任公司 | Rocket projectile vehicle-mounted and ground integrated launching vehicle |
| CN111055984A (en) * | 2020-01-09 | 2020-04-24 | 新余国科特种装备有限公司 | Rocket launcher for ships |
| CN111197946A (en) * | 2020-03-10 | 2020-05-26 | 成都润联科技开发有限公司 | Raining hail-suppression rocket launching device |
| CN111547266A (en) * | 2020-05-13 | 2020-08-18 | 陕西中天火箭技术股份有限公司 | Multi-channel foldable box-type low-altitude sounding rocket launching device |
-
1998
- 1998-03-11 CN CN 98201698 patent/CN2316624Y/en not_active Expired - Lifetime
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104236389A (en) * | 2014-08-08 | 2014-12-24 | 西安航天化学动力厂 | Rain increasing and hail suppressing rocket launcher |
| CN104236389B (en) * | 2014-08-08 | 2015-09-30 | 西安航天化学动力厂 | A kind of precipitation Rain enhancement hail prevention rocket launcher |
| CN106688744A (en) * | 2016-12-29 | 2017-05-24 | 雷神科技（天津）有限公司 | Novel artillery rainfall system |
| CN107907015A (en) * | 2017-11-07 | 2018-04-13 | 重庆长安工业(集团)有限责任公司 | People's rain rocket projectile contact copper sheet layout method |
| CN108414255A (en) * | 2017-12-07 | 2018-08-17 | 上海航天精密机械研究所 | A kind of push type firing mount separation simulation device |
| CN108151584A (en) * | 2018-01-08 | 2018-06-12 | 广州鼎飞科技有限公司 | Integral type rocket bomb transmitting cylinder and emitter |
| CN110887405A (en) * | 2019-11-27 | 2020-03-17 | 贵州航天特种车有限责任公司 | Rocket projectile vehicle-mounted and ground integrated launching vehicle |
| CN111055984A (en) * | 2020-01-09 | 2020-04-24 | 新余国科特种装备有限公司 | Rocket launcher for ships |
| CN111197946A (en) * | 2020-03-10 | 2020-05-26 | 成都润联科技开发有限公司 | Raining hail-suppression rocket launching device |
| CN111547266A (en) * | 2020-05-13 | 2020-08-18 | 陕西中天火箭技术股份有限公司 | Multi-channel foldable box-type low-altitude sounding rocket launching device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee |
Owner name: SHAANXI ZHONGTIAN ROCKET TECHNOLOGY CO., LTD. Free format text: FORMER NAME OR ADDRESS: NO.41 INST., NO.4 ACADEMY, CHINA AEROSPACE INDUSTRY CORP. |
|
| CP01 | Change in the name or title of a patent holder |
Patentee after: Shaanxi Zhongjian Rocket Technology Co., Ltd. Patentee before: No.41 Inst., No.4 Academy, China Aerospace Industry Corp. |
|
| C17 | Cessation of patent right | ||
| CX01 | Expiry of patent term |