CN103808207A - Light high-strength launch barrel - Google Patents
Light high-strength launch barrel Download PDFInfo
- Publication number
- CN103808207A CN103808207A CN201210439257.8A CN201210439257A CN103808207A CN 103808207 A CN103808207 A CN 103808207A CN 201210439257 A CN201210439257 A CN 201210439257A CN 103808207 A CN103808207 A CN 103808207A
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- CN
- China
- Prior art keywords
- launch
- strength
- barrel
- thin skin
- launching tube
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- 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
The invention relates to a launch barrel. In order to reduce occupied space of a launch platform and improve quality, the light high-strength launch barrel is provided. The light high-strength launch barrel comprises a barrel body, a top cover and a base plate. The barrel body comprises a square frame, a plurality of trusses and thin skin, the trusses are fixedly connected to the square frame according to set angles, the square frame is surrounded by the thin skin, and the thin skin is connected with the square frame. Compared with the prior art, the barrel body strength of the launch barrel is strengthened, the weight of the launch barrel is reduced, the occupied space of the launch platform is reduced, the quality is improved, the machine conveying fighting performance of a launch system is improved, and the light high-strength launch barrel is easy to machine, low in cost, high in installation adaptability, safe and reliable.
Description
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Technical field
The present invention relates to launching tube, belong to especially the launching tube of using in carrier rocket, missile release system.
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Background technology
Launching tube is an important component part of emitter, plays the important function of bearing load.The inside and outside core structure of the general employing of traditional method for designing, the launching tube of this structure exists Heavy Weight, flat pad takes up room greatly, increase the burden of flat pad, affect the machine fortune operational performance of emission system, and processed complex, high in cost of production shortcoming, be difficult to meet the requirement of lightweight, high intensity radiation apparatus launching tube.
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Summary of the invention
The defect existing for existing launching tube, the technical problem to be solved in the present invention is to provide a kind of light-high-strength launching tube, guarantees the high-intensity while of launching tube, greatly alleviates emitter weight.
For solving the problems of the technologies described above, a kind of light-high-strength launching tube of the present invention, comprise cylindrical shell, top cover, base plate, cylindrical shell is connected with top cover, base plate, described cylindrical shell comprises square framework, several truss, thin skin, several truss are fixed on square framework by screw by the angle of setting, and thin skin encloses outside square framework and is connected with square framework by screw.
Described square framework comprises four root posts, top frame, on column, have the groove of angle corresponding with truss and number, one end of four root posts is all connected with top frame by screw, and the other end is all connected with base plate by screw, and top frame is connected with top cover by hinge.Form a light-high-strength launching tube.
The present invention adopts truss structure, compared with prior art, when having strengthened the cylinder strength of launching tube, has alleviated the weight of launching tube, is easy to processing, cost is low, suitable dress property is high, safe and reliable.Lightweight cylindrical shell has reduced that flat pad takes up room and quality, has greatly improved the machine fortune operational performance of emission system.
Accompanying drawing explanation
Below with reference to drawings and Examples, the present invention is described in further detail.
Fig. 1 is launching tube structural representation of the present invention.
In figure: base plate 1, framework 2, column 3, truss 4, thin skin 5, top frame 6, top cover 7.
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The specific embodiment
As shown in Figure 1, be launching tube structural representation of the present invention.Launching tube comprises cylindrical shell, top cover 7, base plate 1, and cylindrical shell is connected with top cover 7, base plate 1 by screw.Cylindrical shell comprises square framework 2, truss 4, thin skin 5, on four sides of square framework 2, by screw, three truss 4 are housed, adjacent two truss that connect adjacent two root posts are mutually the angle of a setting, to strengthen the intensity of launching tube cylindrical shell, make launching tube can bear larger power, safe and reliable.Thin skin 5 encloses outside square framework 2 and by screw and square framework 2 fixeds.Square framework 2 comprises four root posts 3, top frame 6, on every root post 3, be processed with several grooves, the angle of its groove and number are corresponding with truss 4, the groove of processing on a face of this routine every root post 3 can fill 4 three of truss, truss 4 and column 3 flush after installing, one end of four root posts 3 by screw all with top frame 6 fixeds, the other end pass through screw all with base plate 1 fixed, top frame 6 is connected with top cover 7 by hinge.Form a light-high-strength launching tube.
Claims (2)
1. a light-high-strength launching tube, comprise cylindrical shell, top cover, base plate, cylindrical shell is connected with top cover, base plate, it is characterized in that: described cylindrical shell comprises square framework, several truss, thin skin, several truss are fixed on square framework by the angle of setting, and thin skin encloses outside square framework and square framework Joint.
2. light-high-strength launching tube according to claim 1, it is characterized in that: described square framework comprises four root posts, top frame, column is provided with the groove of angle and the number corresponding with truss, one end of four root posts is all connected with top frame by screw, the other end is all connected with base plate by screw, and top frame is connected with top cover by hinge.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210439257.8A CN103808207A (en) | 2012-11-07 | 2012-11-07 | Light high-strength launch barrel |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210439257.8A CN103808207A (en) | 2012-11-07 | 2012-11-07 | Light high-strength launch barrel |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103808207A true CN103808207A (en) | 2014-05-21 |
Family
ID=50705331
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210439257.8A Pending CN103808207A (en) | 2012-11-07 | 2012-11-07 | Light high-strength launch barrel |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103808207A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104075622A (en) * | 2014-06-19 | 2014-10-01 | 北京航天发射技术研究所 | Launch barrel device with inner surface resisting gas flushing |
| CN106288952A (en) * | 2016-08-18 | 2017-01-04 | 成都航天万欣科技有限公司 | Launching tube W shape arc and moulding process thereof |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5115711A (en) * | 1991-03-25 | 1992-05-26 | Fmc Corporation | Missile canister and method of fabrication |
| US5327809A (en) * | 1993-03-24 | 1994-07-12 | Fmc Corporation | Dual pack canister |
| US7040212B1 (en) * | 1996-08-09 | 2006-05-09 | Mbda Uk Limited | Launching missiles |
| JP4039480B2 (en) * | 1999-04-23 | 2008-01-30 | 横浜ゴム株式会社 | Lid for projectile launcher |
| RU2348888C2 (en) * | 2006-12-11 | 2009-03-10 | Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения | Missile launching container |
-
2012
- 2012-11-07 CN CN201210439257.8A patent/CN103808207A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5115711A (en) * | 1991-03-25 | 1992-05-26 | Fmc Corporation | Missile canister and method of fabrication |
| US5327809A (en) * | 1993-03-24 | 1994-07-12 | Fmc Corporation | Dual pack canister |
| US7040212B1 (en) * | 1996-08-09 | 2006-05-09 | Mbda Uk Limited | Launching missiles |
| JP4039480B2 (en) * | 1999-04-23 | 2008-01-30 | 横浜ゴム株式会社 | Lid for projectile launcher |
| RU2348888C2 (en) * | 2006-12-11 | 2009-03-10 | Открытое акционерное общество Центральный научно-исследовательский институт специального машиностроения | Missile launching container |
Non-Patent Citations (1)
| Title |
|---|
| 吴媛: "贮运发射箱结构设计及有限元分析", 《中国优秀硕士学位论文全文数据库 工程科技Ⅱ辑》, 15 November 2009 (2009-11-15), pages 13 - 14 * |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104075622A (en) * | 2014-06-19 | 2014-10-01 | 北京航天发射技术研究所 | Launch barrel device with inner surface resisting gas flushing |
| CN106288952A (en) * | 2016-08-18 | 2017-01-04 | 成都航天万欣科技有限公司 | Launching tube W shape arc and moulding process thereof |
| CN106288952B (en) * | 2016-08-18 | 2017-11-10 | 成都航天万欣科技有限公司 | Launching tube W shapes arc and its moulding process |
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Legal Events
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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: 20140521 |