CN104374235A - Submarine-launched missile launcher - Google Patents
Submarine-launched missile launcher Download PDFInfo
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- CN104374235A CN104374235A CN201410745055.5A CN201410745055A CN104374235A CN 104374235 A CN104374235 A CN 104374235A CN 201410745055 A CN201410745055 A CN 201410745055A CN 104374235 A CN104374235 A CN 104374235A
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- missile
- submarine
- air bag
- liquid chamber
- launched
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Abstract
The invention discloses a submarine-launched missile launcher. The submarine-launched missile launcher is characterized by comprising a missile protecting barrel capable of vertically storing missiles and an airbag, the airbag coats around the upper end of the missile protecting barrel annularly, a liquid chamber for storing liquefied gas is arranged at the bottom of the missile protecting barrel, an air pipe or an air way are arranged inside the missile protecting barrel, one end of the air pipe or the air way is communicated with the liquid chamber while the other end of the same is communicated with the airbag, and a control valve controlling the air pipe or the air way to be open and closed is arranged on the air pipe or the air way. When the submarine-launched missile launcher sinks into the sea for launching a missile, the control valve is opened, the liquefied gas in the liquid chamber enters the airbag through the air pipe or the air way, and the airbag is inflated to gradually float out the sea to vertically launch the missile. The submarine-launched missile launcher can ascend from the sea to the water surface by inflating the airbag, and a temporary launching silo can be built in the sea for vertical launching, so that application range of the submarine-launched missile launcher can be widened greatly, invisibility of the submarine-launched missile launcher is improved greatly, and the submarine-launched missile launcher is enabled to be difficult to track and prevent, thereby being higher in safety and practicability.
Description
[technical field]
The present invention relates to missile launcher, particularly a kind ofly rely on airbag aeration and transmitter can be made to sink to marine and float on the submarine launched missile transmitter that MISSILE LAUNCHING is carried out on sea.
[background technology]
Submarine launched missile refers to by certain class submarine-launched missile, and its method of launching mainly contains two kinds, and one is the unpowered transmitting of dry type, and another kind is the dynamic transmitting of dry type.The maximum difference of these two kinds of radiation patterns is exactly the design difference of its underwater research vehicle.After the vehicle of transmitting that dry type is unpowered is launched out torpedo tube (launch canister), the buoyancy utilizing launch power and vehicle (i.e. missile launcher) itself to have navigates by water and floats in water, when casing is raised to the water surface at a certain angle, the protecgulum of automatic jettisoning vehicle, simultaneously, missile booster is lighted a fire guided missile release in vehicle, and guided missile proceeds to airflight state immediately.Compared with no-power way, the vehicle afterbody of dynamic transmitting is equipped with rocket engine, underwater control rudder and related control device.After being launched by torpedo tube, first unpowered control section is entered, after vehicle leaves 10 meters, submarine, the rocket motor ignition of vehicle afterbody, vehicle is accelerated to the speed of 20 meter per seconds, after 10-15 second, vehicle and sea level are miter angle water outlet and leap to aerial, and its freeboard can reach more than 20 meters.Now by the thrust of the gas generator in vehicle, ejected by guided missile by a piston from vehicle, anti-warship guided missle boost motor is lighted a fire, and guided missile enters airflight state.This two kinds of each have their own design difficulties of radiation pattern and operational superiority.When adopting unpowered vehicle radiation pattern, for reducing the underwater speed loss of vehicle, ensure that it goes out the requirement of water speed, submarine can only adopt periscope depth to launch, disguise will almost, adopt Powered carrier radiation pattern then to there is not this shortcoming, therefore can carry out MISSILE LAUNCHING in the full operation degree of depth of submarine, disguise is higher, but it need arrange complicated power set.Generally speaking, existing submarine launched missile transmitter or complex structure, cost is comparatively large, or the scope of application is narrow, is difficult to the user demand meeting various occasion, disguised poor.
[summary of the invention]
The present invention is intended to solve the problem, and provides the submarine launched missile transmitter that a kind of structure is simpler, disguised more by force, security is higher, the scope of application is wider.
For achieving the above object, the invention provides a kind of submarine launched missile transmitter, it is characterized in that, it comprises can the guided missile casing of vertical storage guided missile and air bag, described air pocket rings is coated on the upper end surrounding of guided missile casing ringwise, the liquid chamber of storing liquefied gas is provided with in the bottom of described guided missile casing, tracheae or air flue is provided with in the inside of described guided missile casing, one end of described tracheae or air flue is communicated with described liquid chamber, the other end is communicated with described air bag, described tracheae or air flue are provided with the control valve controlling its break-make, when missile launcher sink to marine need launch a guided missile time, described control valve is opened, liquid gas in liquid chamber enters air bag by described tracheae or air flue, make airbag aeration and gradually emersion sea with Vertical-launched Missile.
When missile launcher need drop into marine, described control valve is opened, and described liquid gas enters that air bag makes airbag aeration and controlled missile launcher processed sinks to marine gently.
Described air bag is provided with pressure-reducing valve.
Be provided with the increasing apparatus that the liquid gas in described liquid chamber can be made to boost in the bottom of described guided missile casing, described increasing apparatus makes gasifying liquefied gas enter air bag to inflate by making liquid chamber boost.
Described liquid gas is the mixed liquefied gas being mixed with combustible gas.
Described increasing apparatus is heater, and it makes airbag aeration by heating boosting.
Described increasing apparatus is igniter, and it makes liquid chamber boost by controlled burning, and the gases at high pressure of the generation made enter air bag and inflate.
Favorable attributes of the present invention is, it efficiently solves the problems referred to above.The present invention, by arranging the air bag of annular in the upper end of guided missile casing, utilizes airbag aeration and makes missile launcher can rise to the water surface from water, setting up a temporal emission well, to carry out Vertical Launch marine.The present invention is relative to existing submarine launched missile transmitter, and tool of the present invention has the following advantages:
1, structure of the present invention is simple, small volume, and it projects by various conventional means of transport, and as naval vessel, submarine, nuclear submarine, freighter, fishing boat etc., it can improve the scope of application greatly, and strengthens its disguise.
2, submarine launched missile transmitter of the present invention uses flexibly, has stronger disguise, higher security, is more difficult to be followed the trail of strick precaution by enemy, and therefore, its scope of application is wider, has higher practicality.
3, the marine site that submarine launched missile transmitter of the present invention can drop into any degree of depth uses, and its deep degree of diving substantially exceeds the latent depth sounding degree of existing nuclear submarine.
Though 4, the present invention belongs to latent emitter, it can use roadbed, ship-based missile, and it is more cost-saving up to 20% than traditional submarine launched missile transmitter.
[accompanying drawing explanation]
Fig. 1 is planar structure schematic diagram of the present invention.
[detailed description of the invention]
The following example is to further explanation of the present invention and supplements, and does not constitute any limitation the present invention.
As shown in Figure 1, submarine launched missile transmitter of the present invention mainly comprises guided missile casing 1 and air bag 2.
Described guided missile casing 1 is for vertical storage guided missile 7 and carry out guided missile 7 and launch.In addition, guided missile casing 1 of the present invention, also for the protection of guided missile 7, helps guided missile 7 to resist the pressure of seawater.Therefore, described guided missile casing 1 should be made up of corrosion-resistant, that intensity is high material.In the present embodiment, described guided missile casing 1 is in column type, and it meets the basic demand of existing launch canister: provide mechanical protection as it can be guided missile 7, make guided missile 7 from mechanical damage; Can be guided missile 7 and temperature protection is provided, make guided missile 7 from the impact of the adverse circumstances such as high temperature, severe cold, sleet; Can be guided missile 7 and dry gas or inert gas shielding are provided, make guided missile 7 from corrosion that is warm, smog.Meanwhile, described guided missile casing 1 should have certain intensity, rigidity, meets the effect of various load under transport and emission state; In addition, be provided with various instrument and meter in described guided missile casing 1, it can be used for controlling and ensure that guided missile 7 leaves the right or normal track smoothly and launches.Primary object of the present invention is, is equipped with inflatable air bag 2 in the top surrounding of described guided missile casing 1, is provided with the liquid chamber 3 of storing liquefied gas in the bottom of described guided missile casing 1, is provided with tracheae or air flue 4 in described guided missile casing 1.One end and the air bag 2 of described tracheae or air flue 4 are through, the other end and liquid chamber 3 through.Described tracheae or air flue 4 are provided with control valve 5, and it is for controlling the break-make of tracheae or air flue 4, to realize the control of inflating air bag 2.Described control valve 5 can adopt known electronic control valve 5, also can adopt air valve.In the present embodiment, described control valve 5 is air valve.
Because in deep-sea, ocean temperature is lower, enter in air bag 2 for making the liquid gas in liquid chamber 3 and air bag 2 is inflated, increasing apparatus 6 can be set in the bottom of described guided missile casing 1.Described increasing apparatus 6 heats up for making liquid chamber 3, makes gasifying liquefied gas become gas, and the gases at high pressure providing enough pressure to make gasification can enter air bag 2 and air bag 2 is inflated.Described increasing apparatus 6 can be heater, and its mode by heat temperature raising makes liquid chamber 3 temperature improve, and pressure improves and makes gasifying liquefied gas and enter air bag 2 to inflate.In addition, described increasing apparatus also can be igniter, and it makes dry gas fuel by lighting a fire, and produces higher pressure and makes airbag aeration.When producing HTHP for needing controlled burning, described liquid gas can select the hydraulic hybrid gas being mixed with combustible gas, and described increasing apparatus 6 can adopt electric plug device.It should be noted that, according to submarine launched missile transmitter the marine site degree of depth that is suitable for different, those skilled in the art can adopt diverse ways to utilize the liquid gas in liquid chamber to inflate air bag 2, to realize object of the present invention, heating boosting described in the present embodiment, igniting boosting are only wherein one of mode, and it is not limited to this.Such as, when this submarine launched missile transmitter applies to neritic area, not needing, increasing apparatus 6 is set and just can easily utilize the liquid gas of liquid chamber 3 to inflate air bag 2; And for example, when this submarine launched missile transmitter apply to a little depths time, described hydraulic pressure gas can adopt hydraulic pressure nitrogen etc., arrange simultaneously increasing apparatus carry out heating boosting.And for marine site, deep-sea, because seawater pressure is comparatively large, being now suitable for the mode of ignition boosting, described liquid gas can select the mixed liquefied gas being mixed with combustible gas, is produced required pressure to airbag aeration by controlled burning.The mode strutted owing to making it to expand to air bag 2 inflation is a lot, and the present embodiment cannot enumerate, and therefore, under the condition not departing from the present invention's design, those skilled in the art's similar structures used all should fall within the scope of protection of the present invention.
Described control valve 5 and increasing apparatus 6 are connected with long-range control end by wireless signal, and like this, just remote controlled end controls the inflation of air bag 2.In addition, because deep sea pressure is comparatively large, for ensureing air bag 2 performance, described air bag 2 is also provided with pressure-reducing valve 8.By this, submarine launched missile transmitter of the present invention is just defined.During air bag 2 unaerated, it is empty flat is convenient to transport.During use, described submarine launched missile transmitter is by naval vessel, submarine, nuclear submarine, freighter, and even fishing boat is thrown in, and is dropped in water.In the process of this submarine launched missile 7 submerged, control control valve 5 by remote control terminal and open, the liquid gas in liquid chamber 3 is entered in air bag 2 by tracheae or air flue 4, air bag 2 is inflated.By controlling the aeration quantity of air bag 2, and ensure the mild submerged of submarine launched missile 7.When needs launch a guided missile 7 time, air bag 2 is inflated, to ensure that the buoyancy suffered by submarine launched missile transmitter is greater than seawater pressure and self gravitation thereof, thus can rise gently under air bag 2 acts on and float up to sea, air bag 2 is made to float on sea, under the guided missile casing 1 be positioned at below air bag 2 is then positioned at horizontal plane, thus be equivalent to establish a temporal emission well at sea.Because air bag 2 is in the ring-like surrounding being coated on guided missile casing 1, its profile is similar to mushroom, and therefore it can make the basic and horizontal plane of guided missile 7, thus can be beneficial to guided missile 7 Vertical Launch.
Submarine launched missile transmitter of the present invention is not only applicable to the guided missile 7 of Vertical Launch, and being also applicable to other can the rocket projectile etc. of Vertical Launch.Submarine launched missile transmitter of the present invention is applied widely, and it is not limited to launch environment, can project in any waters, and due to its small volume, is difficult to tracked, can substantially increases disguise and security after in input water.In addition, submarine launched missile transmitter of the present invention loads convenient transportation, and not only special naval vessel, submarine, nuclear submarine can carry, and common fishing boat, freighter also can carry, even can also air transport drop, thus it is more flexible that it is used, and is difficult to be followed the trail of strick precaution by enemy.
Although by above embodiment to invention has been announcement, scope of the present invention is not limited thereto, and under the condition not departing from the present invention's design, above each component can be replaced with the similar or equivalent element that art personnel understand.
Claims (7)
1. a submarine launched missile transmitter, it is characterized in that, it comprises can the guided missile casing (1) of vertical storage guided missile (7) and air bag (2), described air bag (2) ring is coated on the upper end surrounding of guided missile casing (1) ringwise, the liquid chamber (3) of storing liquefied gas is provided with in the bottom of described guided missile casing (1), tracheae or air flue (4) is provided with in the inside of described guided missile casing (1), one end of described tracheae or air flue (4) is communicated with described liquid chamber (3), the other end is communicated with described air bag (2), described tracheae or air flue (4) are provided with the control valve (5) controlling its break-make, when missile launcher sink to marine need launch a guided missile (7) time, described control valve (5) is opened, liquid gas in liquid chamber (3) enters air bag (2) by described tracheae or air flue (4), make air bag (2) inflate and gradually emersion sea with Vertical-launched Missile (7).
2. submarine launched missile transmitter as claimed in claim 1, it is characterized in that, when missile launcher need drop into marine, described control valve (5) is opened, described liquid gas enter air bag (2) make air bag (2) inflate and controlled missile launcher processed sinks to marine gently.
3. submarine launched missile transmitter as claimed in claim 2, is characterized in that, described air bag (2) is provided with pressure-reducing valve (8).
4. submarine launched missile transmitter as claimed in claim 3, it is characterized in that, be provided with the increasing apparatus (6) that the liquid gas in described liquid chamber (3) can be made to boost in the bottom of described guided missile casing (1), described increasing apparatus (6) makes gasifying liquefied gas enter air bag (2) to inflate by making liquid chamber (3) boost.
5. submarine launched missile transmitter as claimed in claim 4, it is characterized in that, described liquid gas is the mixed liquefied gas being mixed with combustible gas.
6. submarine launched missile transmitter as claimed in claim 5, it is characterized in that, described increasing apparatus is heater, and it makes air bag (2) inflate by heating boosting.
7. submarine launched missile transmitter as claimed in claim 5, it is characterized in that, described increasing apparatus is igniter, and it makes liquid chamber boost by controlled burning, and the gases at high pressure of the generation made enter air bag (2) and inflate.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410745055.5A CN104374235A (en) | 2014-12-09 | 2014-12-09 | Submarine-launched missile launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410745055.5A CN104374235A (en) | 2014-12-09 | 2014-12-09 | Submarine-launched missile launcher |
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| Publication Number | Publication Date |
|---|---|
| CN104374235A true CN104374235A (en) | 2015-02-25 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410745055.5A Pending CN104374235A (en) | 2014-12-09 | 2014-12-09 | Submarine-launched missile launcher |
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| CN (1) | CN104374235A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109204753A (en) * | 2018-07-27 | 2019-01-15 | 南京航空航天大学 | The launch vehicle and the means of delivery of submarine multitask unmanned plane |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201449211U (en) * | 2009-08-14 | 2010-05-05 | 姜春 | Equal-pressure launching device for deep-sea submarine ballistic missile |
| CN102923281A (en) * | 2012-04-05 | 2013-02-13 | 周松林 | Submarine type missile launching platform |
| CN202793178U (en) * | 2012-08-02 | 2013-03-13 | 河南科技大学 | Submarine-launched missile launcher capable of track preventing |
| CN103673761A (en) * | 2012-09-17 | 2014-03-26 | 陆小敏 | Underwater missile launching silo |
| CN204359204U (en) * | 2014-12-09 | 2015-05-27 | 葛爽 | Submarine launched missile transmitter |
-
2014
- 2014-12-09 CN CN201410745055.5A patent/CN104374235A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201449211U (en) * | 2009-08-14 | 2010-05-05 | 姜春 | Equal-pressure launching device for deep-sea submarine ballistic missile |
| CN102923281A (en) * | 2012-04-05 | 2013-02-13 | 周松林 | Submarine type missile launching platform |
| CN202793178U (en) * | 2012-08-02 | 2013-03-13 | 河南科技大学 | Submarine-launched missile launcher capable of track preventing |
| CN103673761A (en) * | 2012-09-17 | 2014-03-26 | 陆小敏 | Underwater missile launching silo |
| CN204359204U (en) * | 2014-12-09 | 2015-05-27 | 葛爽 | Submarine launched missile transmitter |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109204753A (en) * | 2018-07-27 | 2019-01-15 | 南京航空航天大学 | The launch vehicle and the means of delivery of submarine multitask unmanned plane |
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Application publication date: 20150225 |