CN203489792U - Rain-increasing/hail-suppressing rocket-powered missile accurate in timing and reliable in running - Google Patents
Rain-increasing/hail-suppressing rocket-powered missile accurate in timing and reliable in running Download PDFInfo
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- CN203489792U CN203489792U CN201320653769.4U CN201320653769U CN203489792U CN 203489792 U CN203489792 U CN 203489792U CN 201320653769 U CN201320653769 U CN 201320653769U CN 203489792 U CN203489792 U CN 203489792U
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- 230000006698 induction Effects 0.000 claims abstract description 15
- 239000000779 smoke Substances 0.000 abstract 2
- 230000007812 deficiency Effects 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
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Abstract
The utility model provides a rain-increasing/hail-suppressing rocket-powered missile accurate in timing and reliable in running, which comprises a ballistic cap, a parachute, a spreader, a smoke bin and a rocket part; and the rocket-powered missile is characterized by also comprising an active electronic delay chip, a battery, an umbrella bin door and an induction umbrella, wherein the umbrella bin door is arranged on the side wall of the ballistic cap, the induction umbrella is connected with the umbrella bin door, the parachute and the spreader are arranged in the ballistic cap, the induction umbrella is connected with the parachute, the front end of the spreader is dead against the umbrella bin door, the active electronic delay chip and the battery are arranged between the spreader and the smoke bin, the active electronic delay chip is electrically connected with the battery, and the rocket part is located at the rear end part of the rocket-powered missile. The rocket-powered missile has the effects that 1, faults such as umbrella chasing and umbrella twisting and the like at a rear body of an existing rocket-powered missile do not occur, therefore, the normal opening and running of the parachute are ensured; and 2, the rocket-powered missile is accurate in delay time and reliable in running.
Description
Technical field: the utility model relates to accurately reliable rainfall-increasing and anti-hail rocket bullet of a kind of rainfall-increasing and anti-hail rocket bullet of Weather modification operation, particularly a kind of timing.
Technical background: as shown in Figure 1, it is mainly comprised of blast cap 1, parachute 2, umbrella hook 3, ejector 4, firer's Delay Tube 5, tabacco barn 6, rocket portion 7 existing rainfall-increasing and anti-hail rocket bullet.Parachute 2 is located in the blast cap 1 of rocket projectile front portion, and it is released and flick forward together with blast cap 1 by the thrust of ejector 4.The deficiency that this kind of rocket projectile in use exists is: after 1, easily producing, body chases after umbrella, turns round the faults such as umbrella, have a strong impact on the operation of rocket projectile, because parachute 2 is to open in running forward under the effect of impulse force, in some cases, body below can catch up with the parachute 1 opening, and parachute 1 can not normally be opened and cause fault; 2, defer time forbidden, moved unreliable, because the arming delay device in rocket projectile is firer's Delay Tube 5, and firer's Delay Tube 5 in whole production process because of the impact of the aspects such as raw material, processing technology, assemble flow, its extension is difficult to accurately, it is unreliable to make to move.
Summary of the invention: the purpose of this utility model is, for body after the easy generation in use existing before the existing hail-suppression rocket bullet of increasing rain artificially chase after umbrella, turn round umbrella, defer time is forbidden, move insecure deficiency, and proposes accurately reliable rainfall-increasing and anti-hail rocket bullet of a kind of timing.
By following technical proposals, can realize the purpose of this utility model, a kind of timing is reliable rainfall-increasing and anti-hail rocket bullet accurately, comprise blast cap, parachute, ejector, tabacco barn, rocket portion, it is characterized in that, also comprise active electronic delay chip, battery, umbrella door, induction umbrella, umbrella door is located at the sidewall of blast cap, induction umbrella is connected with umbrella door, parachute and ejector are located in blast cap, induction umbrella is connected with parachute, ejector front end is over against umbrella door, active electronic extension chip and battery are located between ejector and tabacco barn, active electronic extension chip and battery are electrically connected to, rocket portion is positioned at the rearward end of rocket projectile.
For ease of umbrella door, open, umbrella door is that buckle is connected with the sidewall of blast cap.
Effect of the present utility model is: 1, there will not be the rear body of existing rocket projectile to chase after umbrella, turn round the faults such as umbrella, can guarantee that parachute normally opens and move, this is that this device is provided with umbrella door and induction umbrella in the sidewall of blast cap, umbrella door is opened and moves and involve induction umbrella to vertical rocket projectile traffic direction under the effect of ejector, induction umbrella is taken parachute again out of, because parachute is vertical rocket projectile traffic direction operation, so, there will not be rear body to chase after umbrella, turn round the faults such as umbrella; 2, defer time is accurate, reliable, because this rocket projectile adopts active electronic extension chip and thermal cell to delay, the degree of accuracy of electronic product in time operation is high more than firer's Delay Tube, because its affected factor is few, so it can make rocket projectile defer time accurate, reliable.
Below in conjunction with accompanying drawing, the utility model is further set forth.
Accompanying drawing explanation:
Accompanying drawing 1 is the structural representation (broken section) of existing rainfall-increasing and anti-hail rocket bullet.
Accompanying drawing 2 is structural representation of the present utility model (broken section).
Referring to accompanying drawing 2, a kind of timing is reliable rainfall-increasing and anti-hail rocket bullet accurately, and it is comprised of blast cap 1, parachute 2, umbrella door 3, induction umbrella (not shown), ejector 4, active electronic extension chip 5, battery 6, tabacco barn 7, rocket portion 8.Parachute 2 and ejector 4 are located in blast cap 1.Umbrella door 3 is located at the sidewall of blast cap 1, and induction umbrella is connected with umbrella door 3, and induction umbrella is connected with parachute 2.Ejector 4 front ends are over against umbrella door 3.Active electronic extension chip 5 and battery 6 are located between ejector 4 and tabacco barn 7, and active electronic extension chip 5 and battery 6 are electrically connected to.Rocket portion 8 is positioned at the rearward end of rocket projectile.For ease of umbrella door 3, open, umbrella door 3 is that buckle is connected with the sidewall of blast cap 1.
Claims (2)
1. the accurate reliable rainfall-increasing and anti-hail rocket bullet of a timing, comprise blast cap, parachute, ejector, tabacco barn, rocket portion, it is characterized in that, also comprise active electronic delay chip, battery, umbrella door, induction umbrella, umbrella door is located at the sidewall of blast cap, induction umbrella is connected with umbrella door, parachute and ejector are located in blast cap, induction umbrella is connected with parachute, ejector front end is over against umbrella door, active electronic extension chip and battery are located between ejector and tabacco barn, and active electronic extension chip and battery are electrically connected to, and rocket portion is positioned at the rearward end of rocket projectile.
2. by the accurate reliable rainfall-increasing and anti-hail rocket bullet of timing claimed in claim 1, it is characterized in that, umbrella door is that buckle is connected with the sidewall of blast cap.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320653769.4U CN203489792U (en) | 2013-10-12 | 2013-10-12 | Rain-increasing/hail-suppressing rocket-powered missile accurate in timing and reliable in running |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320653769.4U CN203489792U (en) | 2013-10-12 | 2013-10-12 | Rain-increasing/hail-suppressing rocket-powered missile accurate in timing and reliable in running |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203489792U true CN203489792U (en) | 2014-03-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320653769.4U Expired - Lifetime CN203489792U (en) | 2013-10-12 | 2013-10-12 | Rain-increasing/hail-suppressing rocket-powered missile accurate in timing and reliable in running |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203489792U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109253666A (en) * | 2018-09-07 | 2019-01-22 | 陕西中天火箭技术股份有限公司 | A kind of low cost simulated training rocket |
| CN112444166A (en) * | 2020-12-07 | 2021-03-05 | 云南锐达民爆有限责任公司 | Timing accurate safe and reliable passive digital rain-increasing hail-suppression rocket |
| CN112540562A (en) * | 2020-12-21 | 2021-03-23 | 云南锐达民爆有限责任公司 | Shadow rocket launching safety locking device based on MCU microprocessor control |
-
2013
- 2013-10-12 CN CN201320653769.4U patent/CN203489792U/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109253666A (en) * | 2018-09-07 | 2019-01-22 | 陕西中天火箭技术股份有限公司 | A kind of low cost simulated training rocket |
| CN109253666B (en) * | 2018-09-07 | 2020-10-09 | 陕西中天火箭技术股份有限公司 | Low-cost simulation training rocket |
| CN112444166A (en) * | 2020-12-07 | 2021-03-05 | 云南锐达民爆有限责任公司 | Timing accurate safe and reliable passive digital rain-increasing hail-suppression rocket |
| CN112540562A (en) * | 2020-12-21 | 2021-03-23 | 云南锐达民爆有限责任公司 | Shadow rocket launching safety locking device based on MCU microprocessor control |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| C56 | Change in the name or address of the patentee | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 609 mailbox 338000, Jiangxi City, Xinyu Province Patentee after: JIANGXI XINYU GUOKE TECHNOLOGY CO.,LTD. Address before: 609 mailbox 338000, Jiangxi City, Xinyu Province Patentee before: JIANGXI XINYU GUOKE TECHNOLOGY CO.,LTD. |
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| CX01 | Expiry of patent term | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140319 |