CN202041121U - Cruise type cruise missile emitter - Google Patents
Cruise type cruise missile emitter Download PDFInfo
- Publication number
- CN202041121U CN202041121U CN2011200151018U CN201120015101U CN202041121U CN 202041121 U CN202041121 U CN 202041121U CN 2011200151018 U CN2011200151018 U CN 2011200151018U CN 201120015101 U CN201120015101 U CN 201120015101U CN 202041121 U CN202041121 U CN 202041121U
- Authority
- CN
- China
- Prior art keywords
- charging device
- solar
- solar charging
- main body
- solar energy
- 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
Links
Images
Abstract
The utility model discloses a cruise type cruise missile emitter. The two edges of a solar fixed receiving surface are movably connected to a solar receiving surface which is fixedly connected to a telescoping rod, and the telescoping rod is movably connected to a solar charging device main body; the solar fixed receiving surface is fixedly connected to the solar charging device main body; the front end of the middle part of the solar fixed receiving surface is provided with a satellite antenna, the rear end of the middle part of the solar fixed receiving surface is provided with a shooting lens, the satellite antenna and the shooting lens are fixedly connected; the solar charging device main body is fixedly connected to a missile casing shield via a plurality of solar charging device fixed points; the two ends of the solar charging device are provided with auxiliary turbine paddles; the lower bottom of the missile casing shield is provided with a sonar detector cable, and the rear end of the missile casing shield is provided with a plurality of turbine propellers. The emitter in the utility model has the advantages of simple structure, convenient, practical and durable use, low cost, safety, reliability, and easy installation.
Description
Technical field
The utility model relates to a kind of guided missile launcher, especially a kind of formula cruise missile emitter that cruises.
Background technology
At present, the southern China sea in China through after 5 years relatively stable, existed the southern China sea tense situation of controversial issue with sovereign right to emerge once more in 2007.Day by day nervous situation has almost been lighted in resource, the competition that comprises oil, gas storage and fishery resources, but other factors, as nationalism, also playing a role, in addition, more powerful regional military presence can make China carry out strength projection, blockade and reconnaissance activities, and to influence the crucial sea route in this district, these traffic lines are passages of global 50% commerce and trade.The combination of these interests encourages China external military assets is carried out daily operational sensitiveness at China's territory restriction external water area.
If China carries out the strategy patrol to southern China sea waters; this will make the Chinese government that more powerful conventional military presence is provided; guarantee protection to its sea-based deterrent; the increase of garrisoning comprises the water surface, and airborne platform under water; but; China does not build one or many aircraft carriers so far as yet, so PLA need strengthen the delivery capabilities of sea power scope, to change zone equilibrium.
The utility model content
The purpose of this utility model provides a kind of simple in structure, convenient and practical, the formula of cruising cruise missile emitter that cost is lower, and is not only durable in use, safe and reliable, and installs easily.
For solving the problems of the technologies described above, the technical solution of the utility model is:
This formula cruise missile emitter that cruises comprises: antenna, turbine slurry, the solar energy fixedly both sides and the solar energy of receiving plane are accepted the face flexible connection, and solar energy is accepted face and fixedlyed connected with expansion link, and expansion link is connected with the solar charging device subject activity; Solar energy fixedly receiving plane is fixedlyed connected with the solar charging device main body; The solar energy fixedly front end at receiving plane middle part is provided with satellite antenna, and the solar energy fixedly rear end at receiving plane middle part is provided with pick-up lens, and satellite antenna is fixedlyed connected with pick-up lens; The solar charging device main body is fixedlyed connected with the tub guard shield by a plurality of solar charging device fixing points; The two ends of solar charging device main body are provided with auxiliary turbine slurry; Be provided with depth charge in the tub guard shield, the front end of tub guard shield is provided with the openable seal cover, and going to the bottom of tub guard shield is provided with the sonoprobe hawser, and the rear end of tub guard shield is provided with a plurality of turbine propulsion devices.
The inside and outside of openable seal cover all can be opened, in open time the inside machine spring when being collided, can open engaging device; But outside manual unlocking.
Being provided with power circuit in the solar charging device fixing point imports and exports.
The beneficial effects of the utility model:
This utility model is a kind of simple in structure, convenient and practical, the formula of cruising cruise missile emitter that cost is lower, and is not only durable in use, safe and reliable, and installs easily.
Submerge formula cruise missile emitter is as the double action of strategy, tactics; Strategic design: the default self-destruction program of this device, go deep into the deep-sea after the MISSILE LAUNCHING and demolish disappearance automatically, thereby keep its mysteriousness, allow the enemy can not touch the limit, it is produced various imaginations, reach the threat effect that the enemy is taken the photograph in shake; In order to reach fascination enemy's purpose, specify a launch site earlier in the abysmal area, presumptive area is arrived in this device dense ground float, be hidden in the underwater float, issue bulletin novel submarines will be carried out the MISSILE LAUNCHING test again, its place is near more from the enemy army base, and the shake property taken the photograph is big more, and purpose is to hit its self-confidence for missile defense systems.
If the enemy army obtains message, be certain to flight path with a large amount of vessel detection China submarines, we have arrived the appointed place to the emitter submerge already and have hidden in fact.Flight path when countries in the world with the advanced unlikely submarine of sonar detection, and China is after launching cruise missile suddenly under their eyelid, this device sinks to the deep-sea self-destruction and disappears, and its shake is taken the photograph effect and is well imagined.
As tactical effect mainly is confidentiality and the shock action that shows it, also has its precision strike effect.When the guided missile of precise guidance behind the ground of appointment point source explosion, the enemy can later think deeply the safety problem of metropolitan territory.
If up to a hundred carry the emitter of warship guided missile hidden ambush suddenly in the only way which must be passed of enemy aircraft-carrier battle group, may cause the elimination of whole aircraft-carrier battle group.For emergent approach shot, the scene that enemy warship only can occur being at one's wit's end, China to the warship guided missile just as a pack of wolves, enemy warship then is that lamb is the same.
Description of drawings
Below in conjunction with the drawings and specific embodiments the utility model is further described.
Fig. 1 is a combining structure schematic diagram of the present utility model.
Fig. 2 is a backsight structural representation of the present utility model
Fig. 3 is a side-looking structural representation of the present utility model.
The specific embodiment
According to Fig. 1-shown in Figure 3, the utility model mainly comprises: solar energy is accepted face 1, expansion link 2, solar charging device main body 3, solar energy fixedly receiving plane 4, solar charging device fixing point 5, tub guard shield 6, openable seal cover 7, turbine propulsion device 8, sonoprobe hawser 9, satellite antenna 10, depth charge 11, auxiliary turbine slurry 12, pick-up lens 13.
The solar energy fixedly both sides of receiving plane 4 and solar energy is accepted face 1 and is flexibly connected, and solar energy is accepted face 1 and fixedlyed connected expansion link 2 and 3 flexible connections of solar charging device main body with expansion link 2; Solar energy fixedly receiving plane 4 is fixedlyed connected with solar charging device main body 3; The solar energy fixedly front end at receiving plane 4 middle parts is provided with satellite antenna 10, and the solar energy fixedly rear end at receiving plane 4 middle parts is provided with pick-up lens 13, and satellite antenna 10 is fixedlyed connected with pick-up lens 13; Solar charging device main body 3 is fixedlyed connected with tub guard shield 6 by a plurality of solar charging device fixing points 5; The two ends of solar charging device main body 3 are provided with auxiliary turbine slurry 12; Be provided with depth charge 11 in the tub guard shield 6, the front end of tub guard shield 6 is provided with openable seal cover 7, and going to the bottom of tub guard shield 6 is provided with sonoprobe hawser 9, and the rear end of tub guard shield 6 is provided with a plurality of turbine propulsion devices 8.
The inside and outside of openable seal cover 7 all can be opened, in open time the inside machine spring when being collided, can open engaging device; But outside manual unlocking.
Being provided with power circuit in the solar charging device fixing point 5 imports and exports.
Operation principle:
The early warning of cruise missile emitter collection, cruise, attack in one, need not manually-operated and drive, identical with the function of scounting aeroplane, different is that it only is suitable for marine early warning, can to around the marine site sky cruise early warning, attack.Its advantage is disguised strong, replenishes power source (solar recharging) automatically, swims since die in boundless and indistinct big sea, only need expose a slight signal transmitting antenna, and command post keeps in touch with the base.
This guided missile launcher can be in base straighforward operation on the bank, receive the early warning information of being passed back around it, its navigation circuit of satellite fix guidance is equipped with retractable aerial above it, surface several meters high, camera is housed all around, directly several kilometers Surface Picture is passed the base back on every side, and its shell mechanism is identical with submarine, light-duty alloy steel products manufacturing, skin can conceal the section bar material, the satellite reconaissance of prevention sky.
Submerge formula cruise missile emitter integral color is identical with seawater, provides power by battery, solar recharging, when found around enemy helicopter, but the free shrink solar charging device is dived in the underwater, and close all power sources, prevent the detection of sonar device.If in the state of war, its direct current generator drives the noise that is produced and equals zero under the covering of great waves sound.As long as avoid the eyes search of helicopter pilot, any surface ship all can't be guarded against its attack.
If under the state of war, submarine formula cruise missile is near enemy native country or military base, and its entrained ground can carry out destructive strike to the enemy to guided missile.If what carry is nuclear bomb, in the native country when under attack, the riposte of making reprisals property.
Because of its disguise is strong, voyage is unlimited, under satellite fix, can in high sea, cruise arbitrarily, because distance is near, and the time weak point.The anti-preheater system of any guided missile all is invalid to its defence.
Solar energy is accepted face 1: navy blue is identical with the color of seawater.
Expansion link 2: be used for shrinking solar energy equipment.
Solar charging device main body 3: be connected and fixed with guided missile outer shield E portion.
Solar energy is receiving plane 4 fixedly: not collapsible.Can regulate guided missile single unit system balance.
Solar charging device fixing point 5: power circuit is imported and exported.
Tub guard shield 6.
Openable seal cover 7: inside and outsidely all can open, but in just open engaging device outside manual unlocking when the machine semi-annular jade pendant of the inside is collided when opening.
Turbine propulsion device 8: there are two, a job, one is standby.
Sonoprobe hawser 9: scalable.
Satellite antenna 10: scalable.
Side is hung depth charge 11: to the special use of enemy's submarine.
Auxiliary turbine slurry 12: but the direction of rapid adjustment navigation.
Pick-up lens 13: following connection retractable aerial, it is flexible that the base is adjustable.
Chip is equipped with in submerge formula cruise missile emitter inside, the intelligence software timer, and satellite guidance after MISSILE LAUNCHING, start the self-destruction program, and the blast back disappears.
Found by enemy's small-size water surface naval vessels in non-war or under the fortuitous event and near the time, but active attack and enemy perish together, can accomplish secret effect like this.
Can carry additionally depth charge, when find the invasion of enemy's submarine produce and moved under water near the time, can attack in advance, sink by bombing enemy's submarine.
Claims (3)
1. formula cruise missile emitter that cruises, comprise: antenna, turbine slurry, it is characterized in that: the solar energy fixedly both sides and the solar energy of receiving plane (4) is accepted face (1) flexible connection, solar energy is accepted face (1) and is fixedlyed connected with expansion link (2), and expansion link (2) flexibly connects with solar charging device main body (3); Solar energy fixedly receiving plane (4) is fixedlyed connected with solar charging device main body (3); The solar energy fixedly front end at receiving plane (4) middle part is provided with satellite antenna (10), and the solar energy fixedly rear end at receiving plane (4) middle part is provided with pick-up lens (13), and satellite antenna (10) is fixedlyed connected with pick-up lens (13); Solar charging device main body (3) is fixedlyed connected with tub guard shield (6) by a plurality of solar charging device fixing points (5); The two ends of solar charging device main body (3) are provided with auxiliary turbine slurry (12); Be provided with depth charge (11) in the tub guard shield (6), the front end of tub guard shield (6) is provided with openable seal cover (7), going to the bottom of tub guard shield (6) is provided with sonoprobe hawser (9), and the rear end of tub guard shield (6) is provided with a plurality of turbine propulsion devices (8).
2. the formula cruise missile emitter that cruises according to claim 1, it is characterized in that: the inside and outside of described openable seal cover (7) all can be opened, in open time the inside machine spring when being collided, can open engaging device; But outside manual unlocking.
3. the formula cruise missile emitter that cruises according to claim 1 is characterized in that: be provided with power circuit in the described solar charging device fixing point (5) and import and export.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200151018U CN202041121U (en) | 2011-01-18 | 2011-01-18 | Cruise type cruise missile emitter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2011200151018U CN202041121U (en) | 2011-01-18 | 2011-01-18 | Cruise type cruise missile emitter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN202041121U true CN202041121U (en) | 2011-11-16 |
Family
ID=44968560
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2011200151018U Expired - Fee Related CN202041121U (en) | 2011-01-18 | 2011-01-18 | Cruise type cruise missile emitter |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN202041121U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103425913A (en) * | 2013-08-06 | 2013-12-04 | 中国航天科工集团第三研究院第八三五七研究所 | Safely and credibly launching control method for missile |
| CN107102297A (en) * | 2017-03-15 | 2017-08-29 | 上海大学 | A kind of wireless ocean acoustic field monitors positioner |
-
2011
- 2011-01-18 CN CN2011200151018U patent/CN202041121U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103425913A (en) * | 2013-08-06 | 2013-12-04 | 中国航天科工集团第三研究院第八三五七研究所 | Safely and credibly launching control method for missile |
| CN103425913B (en) * | 2013-08-06 | 2017-03-29 | 中国航天科工集团第三研究院第八三五七研究所 | A kind of guided missile safety is credible emission control method |
| CN107102297A (en) * | 2017-03-15 | 2017-08-29 | 上海大学 | A kind of wireless ocean acoustic field monitors positioner |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| Bagnasco | Submarines of World War Two: Design, Development & Operations | |
| RU2554640C2 (en) | Method of detecting sea targets | |
| CN102269552A (en) | Missile with submarine canister | |
| Erickson et al. | Chinese Mine Warfare: A PLA Navy'Assassin's Mace'Capability | |
| Erickson et al. | China Near Seas Combat Capabilities | |
| CN202041121U (en) | Cruise type cruise missile emitter | |
| Wang et al. | Development plan of unmanned system and development status of uuv technology in foreign countries | |
| Ragheb | Nuclear marine propulsion | |
| CN102582808A (en) | Unmanned submarine | |
| CN103673760A (en) | Diving/buoyancy power/gliding (missile/torpedo) system | |
| CN102963513B (en) | Foley submarine | |
| CN108847113A (en) | A kind of dedicated emulated crab locator of teenager's research in defense-related science and technology | |
| RU2576221C1 (en) | Submarine | |
| CN204606178U (en) | A kind of stealthy Submarine | |
| Owen | Anti-submarine warfare: An illustrated history | |
| CN202609063U (en) | Unmanned submarine | |
| CN202743469U (en) | Voice simulation submarine | |
| Winklareth | The Battle of the Denmark Strait: A Critical Analysis of the Bismarck's Singular Triumph | |
| CN107067931A (en) | A kind of special transport aircraft carrier of teenager's research in defense-related science and technology | |
| Jordan | Future Trends in Soviet Submarine Development | |
| Hampshire | Soviet Cruise Missile Submarines of the Cold War | |
| CN109398654A (en) | A kind of ship is downloaded from the attack antisubmarine plane weapon system of transmitting | |
| OHara et al. | Fighting in the Dark: Naval Combat at Night, 1904-1944 | |
| CN102466434A (en) | Intelligent seabed static guided missile | |
| CN203116621U (en) | Detachable anti-intercept and anti-laser-attack flyer capable of releasing bait object |
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: 20111116 Termination date: 20120118 |