CN103673761A - Underwater missile launching silo - Google Patents
Underwater missile launching silo Download PDFInfo
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- CN103673761A CN103673761A CN201210342093.7A CN201210342093A CN103673761A CN 103673761 A CN103673761 A CN 103673761A CN 201210342093 A CN201210342093 A CN 201210342093A CN 103673761 A CN103673761 A CN 103673761A
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- silo
- missile
- missile launching
- underwater
- launching silo
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Abstract
An underwater missile launching silo is composed of an outer shell, a silo mouth cover and a gravity pressing bearing block, wherein the outer shell is made of double layers of steel. The underwater missile launching silo has the advantages that as the missile launching silo is hidden underwater, the missile launching silo cannot be found when transferred; at ordinary times, the missile launching silo is horizontally hidden under the sea, only the pressing bearing block at the front end of the silo mouth needs to be gotten rid of when a missile is launched, the erection and upward floating actions of the launching silo can be completed only through buoyancy, the structure is simple, and large-scale intercontinental missiles with long missile bodies can be launched.
Description
Technical field
The present invention relates to a kind of submarine-based missile silo.
Background technology
The transmitting of present strategic missile is generally the fixed silo transmitting of continental rise, and missile truck Mobile launch fixedly easily exposes to the open air, expose rear survival ability to the open air very poor, although missile truck formula can be motor-driven, must on highway, travel, so a huge monster, hidden ability extreme difference, although Modern submarine also can be born the task of launching a guided missile, long-range intercontinental missile, because body is longer, cannot be launched with submarine, go deep into enemy coastal waters and be easily found, survival ability is not strong yet.
Summary of the invention
The object of the invention is to solve the problems referred to above of existing existence, provide a kind of coastal waters home of can hiding, the launching silo that can launch a guided missile at any time.
The present invention is such, guided missile is placed in submarine formula steel double Shell, after can being dragged to be launched by boats and ships or submarine, level sinks to seabed, jettisoning silo front end gravity ballast piece when needs are launched, under the buoyancy of buoyant cabin, silo well head is holded up, whole silo well head emerges, open silo well head cover plate, MISSILE LAUNCHING, attacks enemy state native country under the guiding of satellite or under programme-control.
Advantage of the present invention is that between adopting in double Shell, punching has gases at high pressure, can offset the pressure of hydraulic pressure to outer casing, pressure transfer is arrived to internal layer shell, thereby make inside and outside two layers of housing jointly resist the hydraulic pressure of seawater, and make diving depth can reach a times of single hull, increased the buoyancy of silo simultaneously.After silo well head emerges, launch a guided missile, guided missile is in water surface transmitting, and discord contact with sea water does not need the influence of hydraulic pressure of considering that guided missile is launched under water, thereby can reduce guided missile production cost, and MISSILE LAUNCHING operating mode and continental rise transmitting are similar, and the research and development time is short.Silo can drag transfer by submarine, good concealment while shifting under water.Owing to being that silo is holded up rear transmitting, can launch the intercontinental missile that body length is longer, due to intercontinental missile far firing range, only silo need be equipped in to national territorial waters, security is good.Silo is mainly that the action of holding up, float of silo is provided by floating when launching a guided missile, and only has energy consumption seldom, and production cost is low, only needs two layers of shell of a steel, a small amount of control appliance, and production cost is low, can equip our troops in a large number, deterrence enemy.
It in accompanying drawing, is structural representation of the present invention.
In figure, 1 is double Shell, and 2 is armed guided missile, and 3 is buoyant cabin, and 4 is launcher closure, and 5 is gravity ballast piece.
The specific embodiment
The present invention has a double-deck steel shell 1, filling high pressure gas between outer casing and internal layer shell, guided missile 2 to be launched is seated in internal layer shell, and buoyant cabin 3 and double Shell produce silo buoyancy jointly, and launcher closure 4 is closed before transmitting, make inner casing sealing, cut off seawater and enter, gravity ballast piece 5 produces gravity, and the effect of kentledge is to prevent silo floating, now gravity is more bigger than buoyancy, make silo reposefully level sink to seabed.When launching a guided missile, jettisoning gravity ballast piece 5, buoyancy is greater than gravity, and silo uphole end is holded up, and simultaneously whole silo floating, after well head surfaces, opens launcher closure, launches a guided missile, and guided missile is attacked enemy state native country under satellite navigation or under programme-control.
Claims (4)
1. a submarine-based missile silo, comprises double Shell (1), buoyant cabin (3), and launcher closure (4), gravity ballast piece forms (5).
2. submarine-based missile silo according to claim 1, is characterized in that: silo adopts double Shell (1), is filled with gases at high pressure between double Shell.
3. submarine-based missile silo according to claim 1, is characterized in that: outer silo end is provided with buoyant cabin (3).
4. submarine-based missile silo according to claim 1, is characterized in that: outer silo front end is provided with gravity ballast piece (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210342093.7A CN103673761A (en) | 2012-09-17 | 2012-09-17 | Underwater missile launching silo |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210342093.7A CN103673761A (en) | 2012-09-17 | 2012-09-17 | Underwater missile launching silo |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103673761A true CN103673761A (en) | 2014-03-26 |
Family
ID=50312053
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210342093.7A Pending CN103673761A (en) | 2012-09-17 | 2012-09-17 | Underwater missile launching silo |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103673761A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104374235A (en) * | 2014-12-09 | 2015-02-25 | 葛爽 | Submarine-launched missile launcher |
| CN105258572A (en) * | 2015-08-07 | 2016-01-20 | 李黄刚 | Space denial military strategy defense plan system |
| CN110262232A (en) * | 2019-05-30 | 2019-09-20 | 中国矿业大学 | A kind of control method of submarine-based missile launcher closure device for opening high tracking accuracy |
-
2012
- 2012-09-17 CN CN201210342093.7A patent/CN103673761A/en active Pending
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104374235A (en) * | 2014-12-09 | 2015-02-25 | 葛爽 | Submarine-launched missile launcher |
| CN105258572A (en) * | 2015-08-07 | 2016-01-20 | 李黄刚 | Space denial military strategy defense plan system |
| CN110262232A (en) * | 2019-05-30 | 2019-09-20 | 中国矿业大学 | A kind of control method of submarine-based missile launcher closure device for opening high tracking accuracy |
| CN110262232B (en) * | 2019-05-30 | 2021-12-17 | 中国矿业大学 | Control method for high tracking precision of underwater missile launching manhole cover opening device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20140326 |