CN104422341A - Rainfall-enhancement and anti-hail rocket sowing device - Google Patents
Rainfall-enhancement and anti-hail rocket sowing device Download PDFInfo
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- CN104422341A CN104422341A CN201310385661.6A CN201310385661A CN104422341A CN 104422341 A CN104422341 A CN 104422341A CN 201310385661 A CN201310385661 A CN 201310385661A CN 104422341 A CN104422341 A CN 104422341A
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- rainfall
- catalyst
- cover plate
- rocket
- cabin
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Abstract
The invention discloses a rainfall-enhancement and anti-hail rocket sowing device, comprising a catalyst igniter and a catalyst cabin. The catalyst igniter comprises an igniter cover and a shell; an electrical ignition head is arranged in the catalyst igniter; the catalyst cabin comprises a front end cover and a cover plate; the external side of the cover plate is tightly pressed on the front end cover by a spring; and the catalyst igniter is communicated with the catalyst cabin. The rainfall-enhancement and anti-hail rocket sowing device simplifies the structure of the present rainfall-enhancement and anti-hail rocket and has more compact structure; the negative mass is reduced; the firing range is increased correspondingly without changing the full length of the rocket and the problem of the present rainfall-enhancement and anti-hail rocket having shorter firing range is solved.
Description
Technical field
The present invention relates to rainfall-increasing and anti-hail rocket sowing apparatus.
Background technology
Current rainfall-increasing and anti-hail rocket, install additional after all adopting catalyst cabin and sow cabin, sow cabin side direction perforate and sow catalyst, invalid load is large, and structure is more complicated, and cost is higher.
Summary of the invention
For increasing existing rainfall-increasing and anti-hail rocket range, simplifying structure, reducing passive quality, the rainfall-increasing and anti-hail rocket sowing apparatus providing a kind of afterbody to sow catalyst of the present invention, concrete scheme of the present invention is as follows for achieving the above object:
A kind of rainfall-increasing and anti-hail rocket sowing apparatus, comprises catalytic ignition tool, catalyst cabin;
Described catalytic ignition tool comprises tool lid and housing, is provided with electric igniter in described catalytic ignition tool;
Described catalyst cabin comprises drive end bearing bracket and cover plate, presses in drive end bearing bracket outside described cover plate by spring;
Described catalytic ignition tool is communicated with described catalyst cabin.
Preferably, two electric igniters in parallel are provided with in described catalytic ignition tool.
Preferably, described drive end bearing bracket is provided with stepped hole, and described cover plate is embedded in described stepped hole.
Preferably, steel wire rope is connected with between described drive end bearing bracket and described cover plate.
Rainfall-increasing and anti-hail rocket sowing apparatus provided by the invention simplifies the structure of existing rainfall-increasing and anti-hail rocket, make its structure compacter, reduce passive quality, correspondingly when rocket total length is constant increase range, solve the difficult problem that rainfall-increasing and anti-hail rocket range is shorter.
Accompanying drawing explanation
Accompanying drawing described herein is used to provide a further understanding of the present invention, forms a application's part, does not form inappropriate limitation of the present invention, in the accompanying drawings:
Fig. 1 is embodiment of the present invention structural representation.
Detailed description of the invention
Describe the present invention in detail below in conjunction with accompanying drawing and specific embodiment, be used for explaining the present invention in this illustrative examples of the present invention and explanation, but not as a limitation of the invention.
Embodiment
As shown in Figure 1, a kind of rainfall-increasing and anti-hail rocket sowing apparatus, comprises catalytic ignition tool, catalyst cabin; Described catalytic ignition tool comprises tool lid 1 and housing 3, is provided with electric igniter 2, and is filled with bulky grain black powder 4 in described catalytic ignition tool; Described catalyst cabin comprises drive end bearing bracket 5 and cover plate 8, presses in drive end bearing bracket 5 outside described cover plate 8 by spring 9; Described catalytic ignition tool is communicated with described catalyst cabin by screw thread.
As the preferred version of above-described embodiment scheme, in described catalytic ignition tool, be provided with two electric igniters 2 in parallel.
As the improvement of above-described embodiment scheme, described drive end bearing bracket 5 is provided with stepped hole, and described cover plate 8 is embedded in described stepped hole, can also arrange sealing ring 7 between drive end bearing bracket 5 and cover plate 8.
As the improvement of above-described embodiment scheme, between described drive end bearing bracket 5 and described cover plate 8, be connected with steel wire rope 6.
The rainfall-increasing and anti-hail rocket sowing apparatus that above-described embodiment scheme provides, before engine ignition, cover plate 8 is pressed on drive end bearing bracket 5 by spring 9, after engine ignition, motor charge burning produces high temperature and high pressure gas, cover plate 8 is still pressed on drive end bearing bracket 5 by gases at high pressure effect, sow cabin leading portion and keep sealing state, motor charge all burnt, spring 9 unclamps, treat that rainfall-increasing and anti-hail rocket flight is to being applicable to sowing cloud layer, bulky grain black powder 4 lighted by electric igniter 2, catalyst in catalyst cabin lighted by bulky grain black powder 4, the gas that bulky grain black powder 4 and catalyst combustion produce pushes cover plate 8 open, then enter in enging cabin along the passage in drive end bearing bracket 5, finally sprayed by engine jet pipe.
Cabin is sowed in the sowing apparatus cancellation of the present embodiment, simplifies and entirely plays structure, reduce passive quality; Decrease processing and installation step, improve the manufacturability of processing and assembling, reduce production cost; At the cover plate of the similar one-way valve structures of sowing apparatus indoor design, be against the spring compression of motor charge end face by one end, while the sealing of maintenance catalyst cabin, ensure motor charge not play in enging cabin, improve enging cabin security; Cancel and sow cabin, when full bullet long constant, correspondingly add motor length, increase range; Catalyst is sowed from afterbody, effectively can reduce at the bottom of bullet and hinder, increase range.
Above the technical scheme that the embodiment of the present invention provides is described in detail, apply specific case herein to set forth the principle of the embodiment of the present invention and embodiment, the explanation of above embodiment is only applicable to the principle helping to understand the embodiment of the present invention; Meanwhile, for one of ordinary skill in the art, according to the embodiment of the present invention, detailed description of the invention and range of application all will change, and in sum, this description should not be construed as limitation of the present invention.
Claims (4)
1. a rainfall-increasing and anti-hail rocket sowing apparatus, is characterized in that:
Comprise catalytic ignition tool, catalyst cabin;
Described catalytic ignition tool comprises tool lid and housing, is provided with electric igniter in described catalytic ignition tool;
Described catalyst cabin comprises drive end bearing bracket and cover plate, presses in drive end bearing bracket outside described cover plate by spring;
Described catalytic ignition tool is communicated with described catalyst cabin.
2. rainfall-increasing and anti-hail rocket sowing apparatus as claimed in claim 1, is characterized in that:
Two electric igniters in parallel are provided with in described catalytic ignition tool.
3. rainfall-increasing and anti-hail rocket sowing apparatus as claimed in claim 1, is characterized in that:
Described drive end bearing bracket is provided with stepped hole, and described cover plate is embedded in described stepped hole.
4. rainfall-increasing and anti-hail rocket sowing apparatus as claimed in claim 1, is characterized in that:
Steel wire rope is connected with between described drive end bearing bracket and described cover plate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310385661.6A CN104422341A (en) | 2013-08-23 | 2013-08-23 | Rainfall-enhancement and anti-hail rocket sowing device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310385661.6A CN104422341A (en) | 2013-08-23 | 2013-08-23 | Rainfall-enhancement and anti-hail rocket sowing device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104422341A true CN104422341A (en) | 2015-03-18 |
Family
ID=52972026
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310385661.6A Pending CN104422341A (en) | 2013-08-23 | 2013-08-23 | Rainfall-enhancement and anti-hail rocket sowing device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104422341A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105557409A (en) * | 2015-12-18 | 2016-05-11 | 重庆长安工业(集团)有限责任公司 | Artificial rainfall rocket projectile catalyst scattering device based on molten metal |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1058341A (en) * | 1964-03-26 | 1967-02-08 | Diehl Karl | Percussion fuze for a projectile or missile |
| RU2060002C1 (en) * | 1992-01-30 | 1996-05-20 | Борис Иванович Гончаренко | Antihail rocket |
| CN2497060Y (en) * | 2001-06-18 | 2002-06-26 | 内蒙古北方保安民爆器材有限公司 | Assembled rain-increasing anti-hail rocket engine |
| CN202024689U (en) * | 2011-05-05 | 2011-11-02 | 吉林保利科技中试有限公司 | Rainmaking rocket in which catalyst of 82mm and rocket engine shares spray pipe |
| CN202890102U (en) * | 2012-11-13 | 2013-04-24 | 晋西工业集团有限责任公司 | Civil hail preventing rain increasing rocket catalyst diffusing device |
-
2013
- 2013-08-23 CN CN201310385661.6A patent/CN104422341A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB1058341A (en) * | 1964-03-26 | 1967-02-08 | Diehl Karl | Percussion fuze for a projectile or missile |
| RU2060002C1 (en) * | 1992-01-30 | 1996-05-20 | Борис Иванович Гончаренко | Antihail rocket |
| CN2497060Y (en) * | 2001-06-18 | 2002-06-26 | 内蒙古北方保安民爆器材有限公司 | Assembled rain-increasing anti-hail rocket engine |
| CN202024689U (en) * | 2011-05-05 | 2011-11-02 | 吉林保利科技中试有限公司 | Rainmaking rocket in which catalyst of 82mm and rocket engine shares spray pipe |
| CN202890102U (en) * | 2012-11-13 | 2013-04-24 | 晋西工业集团有限责任公司 | Civil hail preventing rain increasing rocket catalyst diffusing device |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105557409A (en) * | 2015-12-18 | 2016-05-11 | 重庆长安工业(集团)有限责任公司 | Artificial rainfall rocket projectile catalyst scattering device based on molten metal |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20150318 |