CN201096482Y - Deep sea submarine missile launcher - Google Patents
Deep sea submarine missile launcher Download PDFInfo
- Publication number
- CN201096482Y CN201096482Y CNU2007200156265U CN200720015626U CN201096482Y CN 201096482 Y CN201096482 Y CN 201096482Y CN U2007200156265 U CNU2007200156265 U CN U2007200156265U CN 200720015626 U CN200720015626 U CN 200720015626U CN 201096482 Y CN201096482 Y CN 201096482Y
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- CN
- China
- Prior art keywords
- missile
- motor
- fuel cell
- deep sea
- output shaft
- 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
- 239000000446 fuel Substances 0.000 claims abstract description 17
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract description 4
- 230000002411 adverse Effects 0.000 abstract 1
- 238000004880 explosion Methods 0.000 abstract 1
- 239000002360 explosive Substances 0.000 description 3
- 238000000034 method Methods 0.000 description 2
- 238000005422 blasting Methods 0.000 description 1
- 238000007600 charging Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000012530 fluid Substances 0.000 description 1
- 238000010338 mechanical breakdown Methods 0.000 description 1
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Abstract
Disclosed is a deep sea submarine missile launcher, which has a missile body, the tail part of the missile body is provided with a motor, the output shaft of the motor is led out from the tail end of the missile main body, an impeller is arranged on the output shaft of the motor, a fuel cell and a high energy battery are disposed in the missile body, and the fuel cell and the high energy battery are respectively connected with the power supply end of the motor by a switching controller. The missile launcher has advantages that: the explosion phenomenon will not happen even if the missile can not be launched caused by the failure of the port relying on the fuel cell to provide power to the missile, thereby ensuring the safety of personnel on the submarine; and because the fire propulsion is changed into the electric propulsion, the noise is low and the concealment is strong during launching, and the missile will not be detected easily under water, the ahead speed will not be affected, therefore, the threat to the sea-going target of the adverse party is big.
Description
Technical field:
The utility model is particularly related to a kind of deep sea submarine missile launcher.
Background technology:
Missile launcher is the explosive ejector emission by its afterbody and advances to target of attack under the guiding of satellite navigation system on the submarine.At first to open the hatch door of guided missile load compartment during MISSILE LAUNCHING, in case because of mechanical breakdown or fault, when hatch door can't be opened, because explosive ejector is lighted, guided missile be will cause in the load compartment implode, personnel death and the heavy extra large major accident of submarine in the submarine caused.In addition, the noise of explosive ejector own is big, disguised poor, is easily found by enemy's shipboard sonar in water, and can't hit the mark.
Summary of the invention:
The purpose of this utility model is to solve the problems referred to above that prior art exists, provide a kind of and can when submarine is launched, guarantee personal security on the submarine, noise is little, disguised strong in the emission process, in water, be difficult for being taken place by the enemy, fltting speed is unaffected, and enemy's naval target is threatened big deep sea submarine missile launcher.
The utility model is achieved in that it has a Missile Body, be provided with motor at the Missile Body afterbody, the output shaft of motor is drawn by guided missile main body tail end, on the output shaft of motor, impeller is installed, in Missile Body, be provided with fuel cell and high-energy battery, be provided with remote-controlled valve on fuel cell, described fuel cell is connected with the power end of motor by switching controller respectively with high-energy battery.
Above-mentioned deep sea submarine missile launcher, described high-energy battery is a high-energy rechargeable battery, is provided with TRT on impeller, described TRT is connected with high-energy rechargeable battery by lead.
The utility model has the advantages that: provide power by fuel cell to guided missile, both made, guarantee personal security on the submarine in the hatch door phenomenon of also can not blasting when guided missile can't be launched that breaks down; Be electric propulsion owing to change the firepower propelling, noise is little, disguised strong in the emission process, is difficult for being taken place in water, and fltting speed is unaffected, and is big to the threat of enemy's naval target.
Description of drawings:
Fig. 1 is a structural representation of the present utility model.
Among the figure: Missile Body 1, motor 2, impeller 3, TRT 4, high-energy charged pond 5, fuel cell 6, remote-controlled valve 7, switching controller 8.
The specific embodiment
The utility model has a Missile Body 1, be provided with motor 2 at Missile Body 1 afterbody, the output shaft of motor 2 is drawn by guided missile main body 1 tail end, impeller 3 is installed on the output shaft of motor 2, in Missile Body 1, be provided with fuel cell 6 and high-energy rechargeable battery 5, described fuel cell is the oxyhydrogen combustion battery, is provided with remote-controlled valve 7 on fuel cell 6, and described fuel cell 6 is connected by the power end of switching controller 8 with motor 2 respectively with high-energy rechargeable battery 5.Be provided with TRT 4 on impeller 3, described TRT 4 is connected with high-energy rechargeable battery 5 by lead.
During work, by remote-controlled valve 7 starting fluid batteries 6, fuel cell 6 provides electric energy for motor 2, makes impeller 3 rotation at a high speed, advances to target of attack under the guiding of satellite navigation and location system.When if fuel cell 6 electric energy are not enough, insert high-energy rechargeable battery 5 by switching controller 8 and power is provided for motor 2, in impeller 3 rotary courses, TRT 4 generatings give high-energy rechargeable battery 5 chargings, guarantee high-energy rechargeable battery 5 electric energy abundances.
Claims (2)
1, a kind of deep sea submarine missile launcher, comprise Missile Body, it is characterized in that: be provided with motor at the Missile Body afterbody, the output shaft of motor is drawn by the Missile Body tail end, on the output shaft of motor, impeller is installed, be provided with fuel cell and high-energy battery in Missile Body, be provided with remote-controlled valve on fuel cell, described fuel cell is connected with the power end of motor by switching controller respectively with high-energy battery.
2, deep sea submarine missile launcher according to claim 1, it is characterized in that: described high-energy battery is a high-energy rechargeable battery, is provided with TRT on impeller, described TRT is connected with high-energy rechargeable battery by lead.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200156265U CN201096482Y (en) | 2007-10-30 | 2007-10-30 | Deep sea submarine missile launcher |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2007200156265U CN201096482Y (en) | 2007-10-30 | 2007-10-30 | Deep sea submarine missile launcher |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201096482Y true CN201096482Y (en) | 2008-08-06 |
Family
ID=39923535
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2007200156265U Expired - Fee Related CN201096482Y (en) | 2007-10-30 | 2007-10-30 | Deep sea submarine missile launcher |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201096482Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102923281A (en) * | 2012-04-05 | 2013-02-13 | 周松林 | Submarine type missile launching platform |
| 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 |
| CN103808206A (en) * | 2012-11-05 | 2014-05-21 | 杭州航海仪器有限公司 | A modular co-frame vertical launching device |
-
2007
- 2007-10-30 CN CNU2007200156265U patent/CN201096482Y/en not_active Expired - Fee Related
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102923281A (en) * | 2012-04-05 | 2013-02-13 | 周松林 | Submarine type missile launching platform |
| CN103808206A (en) * | 2012-11-05 | 2014-05-21 | 杭州航海仪器有限公司 | A modular co-frame vertical launching device |
| CN103808206B (en) * | 2012-11-05 | 2015-09-02 | 杭州航海仪器有限公司 | A modular co-frame vertical launching device |
| 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 |
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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: 20080806 Termination date: 20101030 |