CN202938700U - Seaborne intelligent full-automatic intercontinental missile launching silo - Google Patents
Seaborne intelligent full-automatic intercontinental missile launching silo Download PDFInfo
- Publication number
- CN202938700U CN202938700U CN 201220524997 CN201220524997U CN202938700U CN 202938700 U CN202938700 U CN 202938700U CN 201220524997 CN201220524997 CN 201220524997 CN 201220524997 U CN201220524997 U CN 201220524997U CN 202938700 U CN202938700 U CN 202938700U
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- CN
- China
- Prior art keywords
- missile
- silo
- missile launching
- buoyancy
- intercontinental
- 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.)
- Expired - Fee Related
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Abstract
The utility model relates to a seaborne intelligent full-automatic intercontinental missile launching silo. The seaborne intelligent full-automatic intercontinental missile launching silo comprises a circular arc shaped semi-round barrel. A buoyancy flat-round barrel layer is arranged right under the circular arc shaped semi-round barrel. A missile launching vertical silo is arranged at the position of the central portion of the circular arc shaped semi-round barrel and are formed by an inner layer carbon fiber protective casing and an outer layer carbon fiber protective casing, and an intercontinental missile is arranged in the missile launching vertical silo. Two sides of the lower portion of the buoyancy flat-round barrel layer are respectively provided with stored program control propellers. Two sides of the missile launching vertical silo are provided with multiple stored program control propeller thrusters parallel to the stored program control propellers on two sides of the buoyancy flat-round barrel layer. A submarine torpedo sensing instrument is further arranged at the bottom of the missile launching vertical silo. The seaborne intelligent full-automatic intercontinental missile launching silo has the advantages of having invisibility and defense penetration capability compared with land launching, and giving deadly attack to enemies.
Description
Technical field
The utility model relates to a kind of launching silo, relates in particular to the frame for movement of this launching silo.
Background technology
The launching silo of prior art is generally on land, and how realizing settling launching silo at sea is that the technical staff will consider.
Summary of the invention
The utility model technical issues that need to address have been to provide a kind of marine intelligent full-automatic intercontinental missile silo, are intended to solve the above problems.
In order to solve the problems of the technologies described above, the utility model is achieved through the following technical solutions:
The utility model comprises: circular arc half drum; It is buoyancy flat barrel layer below being close to circular arc half drum; Centre at described circular arc half drum is equipped with missile cell; Described missile cell is made by inside and outside two layers of carbon fiber containment vessel, built-in intercontinental missile in missile cell; Be equipped with respectively program control propeller in described buoyancy flat barrel layer bottom two sides; Be equipped with many program control propeller propellers in the both sides of missile cell, and parallel with the program control propeller of buoyancy flat barrel layer two side; Also settled the submarine mine inductance gauge bottom described missile cell.
Compared with prior art, the beneficial effects of the utility model are: have more crypticity than land emission, have more penetration ability, give the enemy with havoc.
Description of drawings
Fig. 1 is structural representation of the present utility model.
The specific embodiment
Below in conjunction with accompanying drawing and the specific embodiment, the utility model is described in further detail:
As seen from Figure 1: the utility model comprises: circular arc half drum 1; Buoyancy flat barrel layer 2 below being close to circular arc half drum 1; Centre at described circular arc half drum 1 is equipped with missile cell 3; Described missile cell 3 is made by inside and outside two layers of carbon fiber containment vessel 4, at the built-in intercontinental missile 5 of missile cell 3; Be equipped with respectively program control propeller 6 in described buoyancy flat barrel layer 2 bottom two side; Be equipped with many program control propeller propellers 7 in the both sides of missile cell 3, and parallel with the program control propeller 6 of buoyancy flat barrel layer 2 two side; Also settled submarine mine inductance gauge 8 in described missile cell 3 bottoms.
The top of marine intelligent full-automatic intercontinental missile silo of the present utility model is circular arc half drum, and being close to below half drum is buoyancy flat barrel layer.Post solar panel above circular arc half drum, be equipped with GPS and aerial target inductor waterborne on a side of circular arc.The centre of circular arc half drum is equipped with carbon fiber guided missile vertical firing shaft, and vertical firing shaft is made by inside and outside two layers of carbon fiber containment vessel, the built-in intercontinental missile of drum.The top of vertical shaft is put plastic closure and is covered slim carbon fiber protective layer outward.During MISSILE LAUNCHING, guided missile breaks through the capping on top, target easily.Capping is protecting vertical shaft to make it not take even a drop of water at ordinary times closely.
Arc half drum is built-in with the instruments such as computer program controlled facility electrical storage device.Computer program controlled facility is according to the situation of satellite instruction and inductor reflection, and the activities of marine intelligent full-automatic intercontinental missile silo is being controlled in intellectuality.
Be equipped with respectively program control propeller in buoyancy flat barrel layer bottom two sides, be equipped with many program control propeller propellers on the vertical firing shaft of buoyancy flat barrel bottom, and parallel with keg float two side propeller.Program control propeller can intelligently make launching silo shift at sea.
Be equipped with many pieces of air-sea light guided missiles at the edge of buoyancy half drum, the situation that light guided missile is sought and visited according to inductance gauge and the instruction issue of GPS are with the safety of protection intercontinental missile.
The bottom of guided missile vertical shaft is equipped with the submarine mine inductance gauge, and is equipped with many pieces of carbon fiber skin plastic packaging Deep Underwater Missiles.Inductance gauge is sought and visited enemy's submarine or submarine mine, and computer chip just starts Deep Underwater Missile and destroys at one stroke the enemy, the safety of protection intercontinental missile.
Marine intelligent full-automatic intercontinental missile silo has greatly improved the viability and prominent anti-power of our intercontinental missile, in wartime to the beyond thought surprise attack of enemy.
Claims (1)
1. a marine intelligent full-automatic intercontinental missile silo, is characterized in that comprising: circular arc half drum; It is buoyancy flat barrel layer below being close to circular arc half drum; Centre at described circular arc half drum is equipped with missile cell; Described missile cell is made by inside and outside two layers of carbon fiber containment vessel, built-in intercontinental missile in missile cell; Be equipped with respectively program control propeller in described buoyancy flat barrel layer bottom two sides; Be equipped with many program control propeller propellers in the both sides of missile cell, and parallel with the program control propeller of buoyancy flat barrel layer two side; Also settled the submarine mine inductance gauge bottom described missile cell.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220524997 CN202938700U (en) | 2012-10-12 | 2012-10-12 | Seaborne intelligent full-automatic intercontinental missile launching silo |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220524997 CN202938700U (en) | 2012-10-12 | 2012-10-12 | Seaborne intelligent full-automatic intercontinental missile launching silo |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202938700U true CN202938700U (en) | 2013-05-15 |
Family
ID=48322934
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220524997 Expired - Fee Related CN202938700U (en) | 2012-10-12 | 2012-10-12 | Seaborne intelligent full-automatic intercontinental missile launching silo |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202938700U (en) |
-
2012
- 2012-10-12 CN CN 201220524997 patent/CN202938700U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20130515 Termination date: 20131012 |