CN205690994U - Rainfall-increasing and anti-hail rocket bullet integral type igniter - Google Patents
Rainfall-increasing and anti-hail rocket bullet integral type igniter Download PDFInfo
- Publication number
- CN205690994U CN205690994U CN201620545679.7U CN201620545679U CN205690994U CN 205690994 U CN205690994 U CN 205690994U CN 201620545679 U CN201620545679 U CN 201620545679U CN 205690994 U CN205690994 U CN 205690994U
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- CN
- China
- Prior art keywords
- integral type
- igniter
- type intermediate
- sowing apparatus
- chamber
- 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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Abstract
This utility model is specifically related to a kind of rainfall-increasing and anti-hail rocket bullet integral type igniter for hail suppression of increasing rain artificially, it is characterized in that including integral type intermediate, sowing apparatus igniter, integral type intermediate plug, engine ignition tool and retracting device harness, installing and arrange flame agent spray orifice on the integral type intermediate of that one end of sowing apparatus igniter, flame agent spray orifice communicates with conical cavity.The advantage that this utility model has low cost, assembly precision is high, intensity is high.This utility model reduces number of parts, reduces cost, simplifies assembly process, improves assembly precision, strengthens whole bullet intensity, improves product flight stability and reliability.
Description
Technical field
This utility model is specifically related to a kind of rainfall-increasing and anti-hail rocket bullet integral type igniting dress for hail suppression of increasing rain artificially
Put.
Background technology
At present, rainfall-increasing and anti-hail rocket bullet sowing apparatus igniter and engine ignition tool be separately mounted to flame bilge seat and in
Between on the end, flame bilge seat and the middle end, are threaded connection, and material is phenol aldehyde laminated cloth rod, has been added by machine.Pass through Theoretical Calculation
And practical flight, the weak link of whole bullet is in flame bilge seat and threaded connection place, the middle end, and existing structure is by two part spiral shells
Stricture of vagina connects, and this structure exists and connects error, reduces whole bullet assembly precision, affects rocket flight stability；Two parts be by
Phenol aldehyde laminated cloth rod material machine has added, and design of part complexity not only adds processing cost, and concordance is poor, is unfavorable for that batch is raw
Produce；Two parts are connection to be carried out in connection procedure, increases assembly difficulty, and assembly technology is poor；The phenol aldehyde laminated cloth rod that machine adds
Material Burning corrosion resistance is poor, intensity is unreliable, and rocket easily snaps off appearance in flight and dropping process and disintegrates, and reduces rocket
Safety, reliability.
Utility model content
The purpose of this utility model is that the igniter solving prior art rainfall-increasing and anti-hail rocket bullet is separately mounted to flame cabin
Base with at middle the end, and both are threaded connection, and there is connection error, and assembly difficulty is big, causes whole bullet low precision, legibility
Body, poor stability, the defect of poor reliability, it is provided that a kind of rainfall-increasing and anti-hail rocket bullet integral type igniter, its purpose is as follows:
(1) flame bilge seat and the middle end are united two into one, be designed to a part, i.e. integral type intermediate, reduce part
Quantity, reduces processing and material cost, reduces rigging error, improves efficiency of assembling；
(2) on integral type intermediate, design sowing apparatus igniter and engine ignition has two assembling structures, adjust
Connection position, improves assembly reliability, optimizes assembly technology；
(3) the integral type intermediate after adjusting uses once molding formed, and material is phenolic fiberglass reinforced plastics plastics, both enhances
The intensity of part, Burning corrosion resistance, also improve part processing precision and concordance.
This utility model is achieved by the following technical solution:
I.e. a kind of rainfall-increasing and anti-hail rocket bullet integral type igniter, it is characterised in that include integral type intermediate, sow
Device igniter, integral type intermediate plug, engine ignition tool and retracting device harness, described integral type intermediate is two
The hollow tube-shape body that end is open, its one end arranges conical cavity, and the other end arranges cylindrical cavity, is provided with and broadcasts bottom conical cavity
Spreading device igniter and install chamber, sowing apparatus igniter is installed chamber side and is provided with retracting device harness hole, reclaims dress
Putting one end, harness hole to communicate with conical cavity, the other end communicates with cylindrical cavity, and retracting device harness is arranged on
In retracting device fire hole, its front end extends to outside integral type intermediate by conical cavity, and sowing apparatus igniter is installed
Chamber communicates with cylindrical cavity, and cylindrical cavity internally installed engine ignition tool and integral type intermediate plug, in integral type
The outer end of mesosome plug is provided with groove, and engine ignition tool is installed in a groove, is provided with through hole in the middle part of integral type intermediate plug, reclaims
The rear end of device harness is connected through the through hole of integral type intermediate plug with engine ignition tool, installs sowing apparatus igniting
Having on the integral type intermediate of that one end and arrange flame agent spray orifice, flame agent spray orifice communicates with conical cavity.
As preferred version of the present utility model: flame agent spray orifice of the present utility model is obliquely installed.
As preferred version of the present utility model: sowing apparatus igniter is installed and is provided with between chamber and cylindrical cavity point
Separate space room, the internal diameter of described separation chamber installs the internal diameter of chamber more than sowing apparatus igniter, less than in cylindrical cavity
Footpath.
It is to facilitate retracting device harness cabling that this utility model separates the effect of chamber.
Principle of the present utility model is as follows:
This utility model uses phenolic fiberglass reinforced plastics integral type intermediate, is passed in the middle of integral type by retracting device harness
Body is fixed, then is arranged on integral type intermediate by sowing apparatus igniter, then integral type intermediate plug is assembled, and uses ring
Oxygen glue is fixed, and is finally fixed in the groove of intermediate plug by engine ignition tool, forms integral type intermediate igniter.Work
When making, retracting device igniter, sowing apparatus igniter, engine ignition tool are lighted a fire simultaneously, and electromotor first works, sowing apparatus,
The time that retracting device is set by extension rope works successively.
The advantage that this utility model has low cost, assembly precision is high, intensity is high.This utility model minimizing number of parts,
Reduce cost, simplify assembly process, improve assembly precision, strengthen whole bullet intensity, improve product flight stability and reliability.
Accompanying drawing explanation
Fig. 1 is structural representation of the present utility model；
Fig. 2 is face of partly the deciding what is right and what is wrong structural representation of this utility model stereoscopic-state；
Fig. 3 is the structural representation of this utility model integral type intermediate；
Fig. 4 is the perspective view of this utility model integral type intermediate；
Fig. 5 is the structural representation of this utility model sowing apparatus igniter；
Fig. 6 is the structural representation of this utility model integral type intermediate plug；
Fig. 7 is the structural representation of this utility model engine ignition tool.
As shown in FIG.: 1. integral type intermediate；2. flame agent spray orifice；3. sowing apparatus igniter；4. integral type intermediate
Plug；5. engine ignition tool；6. igniter medicine box；7. packing ring；8. ignition charge；9. igniter head；10. retracting device harness；
11. taper chambers；Chamber installed by 12. sowing apparatus igniters；13. cylindrical chamber；14. through holes；15. grooves；16. reclaim dress
Put harness hole；17. separate chamber.
Detailed description of the invention
As shown in Fig. 1-Fig. 7: integral type intermediate 1 is the hollow tube-shape body of both ends open, and its one end arranges conical cavity
11, the other end arranges separation chamber 17, cylindrical cavity 13, and the internal diameter separating chamber 17 is slightly less than the interior of cylindrical cavity 13
Footpath, is provided with sowing apparatus igniter and installs chamber 12 bottom conical cavity 11, sowing apparatus igniter is installed chamber 12 side and set
Retracting device harness hole 16, one end, retracting device harness hole 16 is had to communicate with conical cavity 11, the other end and separation
Chamber 17, cylindrical cavity 13 communicate, and retracting device harness 10 is arranged in retracting device harness hole 16, its front end
Extending to integral type intermediate 1 by conical cavity 11 outside, sowing apparatus igniter 3 is arranged on sowing apparatus igniter and installs
In chamber 12, it is indoor that integral type intermediate plug 4 is arranged on cylindrical cavity, and it arranges through hole 14 and groove 15, engine ignition tool 5
Being arranged in recessed 15, the rear end of retracting device harness 10 passes through hole 14 and the engine ignition of integral type intermediate plug 4
Tool 5 connection, installs and is provided with multiple flame agent being obliquely installed spray on the integral type intermediate 1 of that one end of sowing apparatus igniter 3
Hole 2, flame agent spray orifice 2 communicates with conical cavity 11.
When this utility model assembles, first by retracting device harness 10 through the retracting device on integral type intermediate 1
Harness hole 16 is fixed；Then sowing apparatus igniter 3 is assembled to the sowing apparatus igniter installation of integral type intermediate 1
On chamber 12；Again that integral type intermediate plug 4 is indoor at the cylindrical cavity of integral type intermediate 1 with Wear Characteristics of Epoxy Adhesive；Finally will send out
Motivation igniter 5 is assemblied on the groove 15 of integral type intermediate plug 4, and fixes with epoxy glue.
When this utility model uses, retracting device igniter, sowing apparatus igniter 3, engine ignition have 5 same time points
Fire, electromotor first works, and the time that sowing apparatus, retracting device are set by extension rope works successively.
Claims (3)
1. a rainfall-increasing and anti-hail rocket bullet integral type igniter, it is characterised in that include integral type intermediate, sowing apparatus
Igniter, integral type intermediate plug, engine ignition tool and retracting device harness, described integral type intermediate is that two ends are opened
The hollow tube-shape body put, its one end arranges conical cavity, and the other end arranges cylindrical cavity, is provided with and sows dress bottom conical cavity
Putting igniter and install chamber, sowing apparatus igniter is installed chamber side and is provided with retracting device harness hole, retracting device point
Fire wire guide one end communicates with conical cavity, and the other end communicates with cylindrical cavity, and retracting device harness is arranged on recovery
In mounted point fire hole, its front end extends to outside integral type intermediate by conical cavity, and chamber installed by sowing apparatus igniter
Communicate with cylindrical cavity, cylindrical cavity internally installed engine ignition tool and integral type intermediate plug, integral type intermediate
The outer end of plug is provided with groove, and engine ignition tool is installed in a groove, is provided with through hole, retracting device in the middle part of integral type intermediate plug
The rear end of harness is connected through through hole and the engine ignition tool of integral type intermediate plug, installation sowing apparatus igniter that
Arranging flame agent spray orifice on the integral type intermediate of one end, flame agent spray orifice communicates with conical cavity.
Rainfall-increasing and anti-hail rocket bullet integral type igniter the most according to claim 1, it is characterised in that flame agent spray orifice inclines
Tiltedly arrange.
Rainfall-increasing and anti-hail rocket bullet integral type igniter the most according to claim 1, it is characterised in that sowing apparatus point
Fire tool is installed and is provided with separation chamber between chamber and cylindrical cavity, and the internal diameter of described separation chamber is more than sowing apparatus igniter
The internal diameter of chamber is installed, less than the internal diameter of cylindrical cavity.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620545679.7U CN205690994U (en) | 2016-06-07 | 2016-06-07 | Rainfall-increasing and anti-hail rocket bullet integral type igniter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620545679.7U CN205690994U (en) | 2016-06-07 | 2016-06-07 | Rainfall-increasing and anti-hail rocket bullet integral type igniter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205690994U true CN205690994U (en) | 2016-11-16 |
Family
ID=57261409
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620545679.7U Expired - Fee Related CN205690994U (en) | 2016-06-07 | 2016-06-07 | Rainfall-increasing and anti-hail rocket bullet integral type igniter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205690994U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023108567A1 (en) * | 2021-12-16 | 2023-06-22 | 陕西中天火箭技术股份有限公司 | Catalyst sowing device and high-temperature-resistant precipitation-increasing rocket having same |
-
2016
- 2016-06-07 CN CN201620545679.7U patent/CN205690994U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2023108567A1 (en) * | 2021-12-16 | 2023-06-22 | 陕西中天火箭技术股份有限公司 | Catalyst sowing device and high-temperature-resistant precipitation-increasing rocket having same |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161116 Termination date: 20210607 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |