CN201284005Y - Deep sea submarine missile transmitting propulsion unit - Google Patents
Deep sea submarine missile transmitting propulsion unit Download PDFInfo
- Publication number
- CN201284005Y CN201284005Y CNU2008202184565U CN200820218456U CN201284005Y CN 201284005 Y CN201284005 Y CN 201284005Y CN U2008202184565 U CNU2008202184565 U CN U2008202184565U CN 200820218456 U CN200820218456 U CN 200820218456U CN 201284005 Y CN201284005 Y CN 201284005Y
- Authority
- CN
- China
- Prior art keywords
- canister
- cylinder body
- missile
- launching tube
- propelling unit
- 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
A deep-sea submarine missile emission propulsion unit, includes a boat body, a missile launching tube provided in the boat body, and missiles provided in the missile launching tube, which is characterized in that a launching tube support compartment is provided in the corresponding missile launching tube in the boat, a launching tube propulsion unit is provided at the bottom inside the launching tube support compartment, the missile launching tube is located in the supporting compartment and the lower end of which is connected to the propulsion unit; the launching tube propulsion unit is composed of a multi-stage oil cylinder and a hydraulic control system connected to the multi-stage oil cylinder. The utility model has advantages of reasonable structure, safe operation, and capability of using the launching tube propulsion unit to push the missile launching tube and the missile in the missile launching tube out from the boat body and then igniting to emit the missile, so that the missile will not explode in the boat body even if the missile launcher has a failure, to effectively protect the personal safety of the submarine personnel.
Description
Technical field
The utility model is particularly related to a kind of deep sea submarine MISSILE LAUNCHING propelling unit.
Background technology
At present, it is to light a fire in the hull of submarine that military deep-sea operational submarine is launched a guided missile, and by feedway guided missile is penetrated then, in case its feedway breaks down, guided missile just might misfire, and causes guided missile in the submarine implode, causes ship to ruin the serious consequence that the people dies.
Summary of the invention
The purpose of this utility model is to solve the problems referred to above that prior art exists, and provides a kind of avoiding to cause the hull implode because of feedway breaks down, and guarantees the deep sea submarine MISSILE LAUNCHING propelling unit of submarine personal security.
The utility model is achieved in that it comprises hull, is located at the launch canister in the hull and is located at the interior guided missile of launch canister, its special character is: corresponding launch canister place is provided with canister launcher and supports the cabin in hull, support the cabin inner bottom part at canister launcher and be provided with the canister launcher propelling unit, described launch canister is positioned at canister launcher support cabin and the lower end is connected with the canister launcher propelling unit; Described canister launcher propelling unit is to be made of with the hydraulic control system that links to each other with multi-stage oil cylinder a multi-stage oil cylinder.
Above-mentioned deep sea submarine MISSILE LAUNCHING propelling unit, described multi-stage oil cylinder is a two-level oil cylinder, is to be made of an outer cylinder body and the inner piston rod that is located at the inner cylinder body in the outer cylinder body and be located in the inner cylinder body, described inner piston rod upper end is affixed with launch canister.
Above-mentioned deep sea submarine MISSILE LAUNCHING propelling unit, described hydraulic control system comprises fuel tank and the oil pump that is connected fuel tank, oil pump is communicated with outer cylinder body and inner cylinder body by oil circuit respectively, is respectively equipped with solenoid directional control valve and flow velocity control cock on oil pump and outer cylinder body and inner cylinder body bonded assembly oil circuit.
The utility model has the advantages that: rational in infrastructure, safety of operation; can launch canister and the guided missile that is positioned at launch canister be released behind the hull igniting again by the canister launcher propelling unit launches a guided missile; even the guided missile launcher guided missile that breaks down can effectively not protected submarine personnel's personal safety in the hull implode yet like this.
Description of drawings
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is the structural representation of the utility model canister launcher propelling unit.
Among the figure: hull 1, loam cake 2, guided missile 3, launch canister 4, canister launcher supports cabin 5, multi-stage oil cylinder 6, outer cylinder body 601, piston 602, cylinder body 603, inner piston rod 604, hydraulic control system 7, fuel tank 701, oil pump 702, solenoid directional control valve 703, flow velocity control cock 704, solenoid directional control valve 705, watertight barrier film 8.
The specific embodiment
As shown in the figure, the utility model comprises hull 1, be located at the launch canister 4 in the hull 1 and be located at guided missile 3 in the launch canister 4, corresponding launch canister 4 places are provided with loam cake 2 on hull 1, corresponding launch canister 4 places are provided with canister launcher and support cabin 5 in hull 1, support cabin 5 inner bottom parts at canister launcher and be provided with the canister launcher propelling unit, described launch canister 4 is positioned at that canister launcher supports cabin 5 and the lower end is connected with the canister launcher propelling unit, in the upper port of launch canister 4 one deck watertight barrier film 8 is installed.Described canister launcher propelling unit is to be made of with the hydraulic control system 7 that links to each other with multi-stage oil cylinder 6 multi-stage oil cylinder 6.Described multi-stage oil cylinder 6 is a two-level oil cylinder, this two-level oil cylinder is by an outer cylinder body 601, the inner piston rod 604 that is located at the inner cylinder body 603 in the outer cylinder body 601 and is located in the inner cylinder body 603 constitutes, be provided with inner cylinder body 603 in inner cylinder body 603 lower ends and be the piston 602 of one, described inner piston rod 604 upper ends and launch canister 4 are affixed.Described hydraulic control system 7 comprises fuel tank 701 and the oil pump 702 that is connected fuel tank 701, oil pump 702 is communicated with outer cylinder body 601 and inner cylinder body 603 by oil circuit respectively, is respectively equipped with solenoid directional control valve 703,705 and flow velocity control cock 704 on oil pump 702 and outer cylinder body 601 and inner cylinder body 603 bonded assembly oil circuits.
When launching a guided missile, at first launch canister 4 is carried out supercharging in the tube, simultaneously between watertight barrier film 8 and loam cake 2, inject seawater, make that the sea pressure in the space all equates with hull 1 sea pressure outward between air pressure in the launch canister 4 and watertight barrier film 8 and the loam cake 2.Can open loam cake 2 by the maneuvering system of submarine then, starting hydraulic control system 7 control multi-stage oil cylinders 6 launches successively, launch canister 4 base portions are released hull 1, can light gas generator and launch a guided missile 3, guided missile 3 can break through watertight barrier film 8 and penetrate.After the emission, seawater can be poured into launch canister 4 immediately and replenish the weight that hull 1 is launched a guided missile and lost after 3, drives launch canisters 4 by hydraulic control system 7 control multi-stage oil cylinders 6 and resets.
Claims (3)
1, a kind of deep sea submarine MISSILE LAUNCHING propelling unit, comprise hull, be located at the launch canister in the hull and be located at the interior guided missile of launch canister, it is characterized in that: corresponding launch canister place is provided with canister launcher and supports the cabin in hull, support the cabin inner bottom part at canister launcher and be provided with the canister launcher propelling unit, described launch canister is positioned at canister launcher support cabin and the lower end is connected with the canister launcher propelling unit; Described canister launcher propelling unit is to be made of with the hydraulic control system that links to each other with multi-stage oil cylinder a multi-stage oil cylinder.
2, deep sea submarine MISSILE LAUNCHING propelling unit according to claim 1, it is characterized in that: described multi-stage oil cylinder is a two-level oil cylinder, be to be made of an outer cylinder body and the inner piston rod that is located at the inner cylinder body in the outer cylinder body and be located in the inner cylinder body, described inner piston rod upper end is affixed with launch canister.
3, deep sea submarine MISSILE LAUNCHING propelling unit according to claim 1 and 2, it is characterized in that: described hydraulic control system comprises fuel tank and the oil pump that is connected fuel tank, oil pump is communicated with outer cylinder body and inner cylinder body by oil circuit respectively, is respectively equipped with solenoid directional control valve and flow velocity control cock on oil pump and outer cylinder body and inner cylinder body bonded assembly oil circuit.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008202184565U CN201284005Y (en) | 2008-10-13 | 2008-10-13 | Deep sea submarine missile transmitting propulsion unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008202184565U CN201284005Y (en) | 2008-10-13 | 2008-10-13 | Deep sea submarine missile transmitting propulsion unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201284005Y true CN201284005Y (en) | 2009-08-05 |
Family
ID=40948989
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008202184565U Expired - Fee Related CN201284005Y (en) | 2008-10-13 | 2008-10-13 | Deep sea submarine missile transmitting propulsion unit |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201284005Y (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102285437A (en) * | 2011-05-17 | 2011-12-21 | 哈尔滨工程大学 | Hydraulic system of pneumatic miniature sightseeing submarine |
| WO2013000133A1 (en) * | 2011-06-29 | 2013-01-03 | 北京机械设备研究所 | Pollution-free liquid balancing device |
| CN104176218A (en) * | 2014-09-01 | 2014-12-03 | 董兰田 | Vertical launch submarine with tilted missile launching silo |
| CN110775232A (en) * | 2019-10-08 | 2020-02-11 | 中国矿业大学 | Underwater missile launching shaft cover opening and closing device system |
| CN110906790A (en) * | 2019-12-31 | 2020-03-24 | 哈尔滨工业大学 | Repeatedly-loading underwater simultaneous shooting device capable of adjusting boat speed and launching relative position |
-
2008
- 2008-10-13 CN CNU2008202184565U patent/CN201284005Y/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102285437A (en) * | 2011-05-17 | 2011-12-21 | 哈尔滨工程大学 | Hydraulic system of pneumatic miniature sightseeing submarine |
| CN102285437B (en) * | 2011-05-17 | 2013-10-30 | 哈尔滨工程大学 | Hydraulic system of pneumatic miniature sightseeing submarine |
| WO2013000133A1 (en) * | 2011-06-29 | 2013-01-03 | 北京机械设备研究所 | Pollution-free liquid balancing device |
| US8707847B2 (en) | 2011-06-29 | 2014-04-29 | Beijing Mechanical Equipment Institute | Pollution-free liquid balancing device |
| CN104176218A (en) * | 2014-09-01 | 2014-12-03 | 董兰田 | Vertical launch submarine with tilted missile launching silo |
| CN110775232A (en) * | 2019-10-08 | 2020-02-11 | 中国矿业大学 | Underwater missile launching shaft cover opening and closing device system |
| CN110906790A (en) * | 2019-12-31 | 2020-03-24 | 哈尔滨工业大学 | Repeatedly-loading underwater simultaneous shooting device capable of adjusting boat speed and launching relative position |
| CN110906790B (en) * | 2019-12-31 | 2021-11-19 | 哈尔滨工业大学 | Repeatedly-loading underwater simultaneous shooting device capable of adjusting boat speed and launching relative position |
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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: 20090805 Termination date: 20101013 |