CN203345188U - Floating-type diving gear capable of automatically emitting torpedo - Google Patents
Floating-type diving gear capable of automatically emitting torpedo Download PDFInfo
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- CN203345188U CN203345188U CN 201220628114 CN201220628114U CN203345188U CN 203345188 U CN203345188 U CN 203345188U CN 201220628114 CN201220628114 CN 201220628114 CN 201220628114 U CN201220628114 U CN 201220628114U CN 203345188 U CN203345188 U CN 203345188U
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- torpedo
- data processing
- floating
- processing system
- launching
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Abstract
A floating-type diving gear capable of automatically emitting a torpedo comprises a satellite terminal float, a dragging antenna cable, an antenna recovering cabin, floating wings, an engine body, a torpedo emitting cabin tube, a torpedo emitting control device, a pusher, a signal collecting system, a data processing system, a hydraulic and pneumatic control system, front and back volume converters, a hiding control system and a battery pack. The floating-type diving gear is characterized in that when the diving gear is placed in a sea area needing to be blockaded, by means of energy supplied by the battery pack, the satellite terminal float emits a signal to get communicated with a land-based station or a surrounding naval vessel through the signal collecting system to identify a target, tracks and approaches the target under water automatically, accurately attacks the target, has signal interrupting, emitting hiding, sinking and floating and driving functions, and can also be used as a persistent seabed detecting station for collecting information; therefore, military spending and consumption of goods and materials are reduced, and the aim of a zero casualty can be achieved.
Description
Technical field
The utility model relates to the diving equipment, particularly floating type diving equipment that the automatic torpedo-launching of military deep water is used.
Background technology
At present aspect the emission of torpedo, the main launch mode that still relies on water surface warship, Submarine, antisubmarine plane, limitation due to the active distance that is subject to torpedo-launching, especially the heat power of torpedo can produce tail clearly, easily expose too early and tackled, and the submarine shooting position also is completely exposed, rely on the launch mode of water surface warship, Submarine, antisubmarine plane, not only can not the approach shot target, the expenditure that also can increase military expenditure and the consumption of goods and materials, equally also can improve belligerent personnel's casualty rate.
Summary of the invention
The purpose of this utility model, in order to make up in the torpedo-launching process, torpedo is subject to the restriction of effective range exactly, is the purpose that closely emission improves hit rate and reaches zero injures and deaths, and the floating type diving equipment of a kind of torpedo-launching automatically proposed.
The purpose of this utility model, be achieved through the following technical solutions, and the utility model comprises: the ICBM SHF satellite terminal buoy, the trailing aerial cable, antenna is recovered cabin, floating wing, the device body, torpedo-launching cabin pipe, propelling unit, signal acquiring system, data processing system, high-pressure gas cylinder, the hydraulic and pneumatic control system, front and back volume conv, the device control system of hiding, battery pack, the torpedo-launching control setup.
Its feature: a, be provided with two floating wings in left and right and propelling unit, ICBM SHF satellite terminal buoy, trailing aerial cable, an antenna at the device body surface and recover cabin and drain gutter group and torpedo-launching cabin pipe everywhere; Wherein ICBM SHF satellite terminal buoy and trailing aerial cable Electricity Federation, trailing aerial cable penetration antenna is recovered the data processing system Electricity Federation arranged in cabin and device body, with the timer body, with two left and right floating wing axles are arranged, connects; Propeller control system and data processing system Electricity Federation, propelling unit connects with device body, propeller control system axle, and propelling unit connects with the device axis; B is provided with data processing system, propeller control system, battery pack, torpedo-launching control setup, signal acquiring system in the device body; Wherein signal acquiring system and data processing system Electricity Federation, data processing system and propeller control system Electricity Federation, data processing system also respectively with hydraulic pressure and air compression system, device hide control system, battery pack, torpedo-launching control setup Electricity Federation.
In addition, also be provided with high-pressure gas cylinder, hydraulic pressure and air compression system, device hide control system, low pressure gaholder, front and back volume conv in body at device; Wherein high-pressure gas cylinder and hydraulic pressure and air compression system gas connect, hydraulic pressure and air compression system and front and back volume conv gas connect, hydraulic pressure is connected with front and back volume conv oil circuit with air compression system, hydraulic pressure and air compression system and wing left and right internal airbag gas connect, solenoid directional control valve and the device control system Electricity Federation of hiding in hydraulic pressure and air compression system.
Data processing system also respectively with hydraulic pressure and air compression system, the device control system Electricity Federation of hiding.
Solenoid directional control valve a, solenoid directional control valve b, oil pump, air pump and the device control system Electricity Federation of hiding.
The utility model is owing to having adopted technique scheme, be provided with two floating wings in left and right and a propelling unit on the device body, the ICBM SHF satellite terminal buoy, the trailing aerial cable, antenna is recovered cabin, and be provided with tool signal acquiring system and data processing system at the device internal body, hydraulic pressure and air compression system, the device control system of hiding, front and back volume conv, the device control system of hiding, battery pack, the torpedo-launching control setup, thereby realize the lifting of ICBM SHF satellite terminal buoy, the hiding function such as signal interruption and emission, and make this device sink-float and drive, utilize the ICBM SHF satellite terminal buoy to transmit and obtain communication contact with continental rise station or near naval vessels, man machine communication or automatic tracing approach target, torpedo-launching and reach approach shot enemy warship ship, the purpose of Submarine target, when this device being rendered to the marine site of required blockade, the energy that relies on battery pack to offer, also can be used as lasting seabed detecting station collection information uses.
The accompanying drawing explanation
Fig. 1 is this utility model axle side schematic diagram
Fig. 2 is the vertical full sectional view of this utility model
Fig. 3 is this utility model left and right wing part sectional view
Fig. 4 is the principle cross-sectional schematic of former and later two volume convs
Fig. 5 is air pressure and the underground principle schematic of former and later two volume convs
Which :1 - propulsion 2 - satellite terminal buoy 3 - Drag antenna cable 4 - Antenna recover cabin 5 - before the drainage holes set 6 - Floating left wing 7 - Left drain hole group of 8 - devices body 9 - Right drain hole group of 10 - Right wing float 11 - after the drainage holes group of 12 - torpedo compartment tube 13 - data processing system 14 - high pressure cylinder 15 - 16 before the volume converter - hydraulic and compressed air system 17 - device latency control system 18 - low pressure gas cylinders 19 - the volume converter 20 - thruster control system 21 - battery Pack 22 - torpedo launch control device 23 - signal acquisition system 24 - Built- left wing balloon 25 - Right wing built- balloon 26 - the volume of air cabin Interface converter 27 - before the cabin air volume converter interface 28 - before the water tank volume converters Interface 29 - before the rod chamber volume converter oil line interface 30 - before the rod chamber volume converter oil line interface 31 - hydraulic cylinder piston 32 - hydraulic cylinder piston rod 33 - pneumatic cylinder piston 34 - cylinder 35 - the volume of seawater tanks converter interface 36 - the volume of the oil rod cavity converter interface 37 - the volume of the oil chamber rodless converter interface 38 - solenoid valve a39 - pump 40 - tank 41 - relief 42 - solenoid valve b43 - pump 44 - a one-way valve
The specific embodiment
Below in conjunction with accompanying drawing, the utility model will be further described:
The utility model is mainly the inside and outside set ICBM SHF satellite terminal buoy of use device body, the trailing aerial cable, data processing system, signal acquiring system, the torpedo-launching control setup, realize the hiding functions such as signal interruption and emission, this device is provided with two floating wings in left and right and a propelling unit simultaneously, front and back volume conv, make this device sink-float and drive under device is hidden control system control, so, this device utilizes the ICBM SHF satellite terminal buoy to transmit and obtains communication contact with continental rise station or near naval vessels, realize that man machine communication or automatic tracing approach the target torpedo-launching, and reach approach shot enemy warship ship, the purpose of Submarine target, when this device being rendered to the marine site of required blockade, the energy that relies on battery pack to offer, also can be used as lasting seabed detecting station collection information uses.
As shown in Figure 1: above the utility model device body (8), respectively be provided with left and right two floating wings (6), (10), with a propelling unit (1), ICBM SHF satellite terminal buoy (2), trailing aerial cable (3), antenna is recovered cabin (4) and drain gutter group (5) everywhere, (7), (9), (11), left and right two floating wings (6), (10) and propelling unit (1) with device body (8) axle, connect, the axle of the propeller control system (20) that propelling unit (1) is inner with being arranged on device body (8) connects, propeller control system (20) and data processing system (13) Electricity Federation, the purpose of implement device body (8) advance and retreat, ICBM SHF satellite terminal buoy (2) and trailing aerial cable (3) Electricity Federation, trailing aerial cable (3) passes through recovers cabin (4) and data processing system (13) Electricity Federation, recovers cabin (4) and makes trailing aerial cable (3) folding and unfolding reach the purpose that ICBM SHF satellite terminal buoy (2) carries out lifting according to the instruction of data processing system (13).
As shown in Fig. 3, Fig. 5: the left inside right inside solenoid directional control valve a(42 put in air bag (25) and hydraulic pressure and air compression system (16) of air bag (24), wing that puts of the inner wing arranged in left and right two floating wings (6), (10) wherein), check valve (44), air pump (43) gas even.
As shown in Fig. 2, Fig. 5: be provided with hydraulic pressure and air compression system (16), device hide control system (17), data processing system (13) in device body (8), wherein data processing system (13) and device control system (17) Electricity Federation of hiding.
As shown in Figure 5: solenoid directional control valve b(42) with low pressure gaholder (18), check valve (44) gas, connect, air pump (43) connects with check valve (44), wing left and right internal airbag (24), (25) gas.
As shown in Figure 4: the hydraulic cylinder piston (31) in cylinder body (34), pneumatic cylinder piston (33) connect with hydraulic cylinder piston rod (32) axle.
In device body (8), be provided with signal acquiring system (23) and with data processing system (13) Electricity Federation, accept instruction or automatically by data processing system (13), carry out the control setup control system (17) of hiding through signal acquiring system (23) and ICBM SHF satellite terminal buoy (2) and continental rise station or near naval vessels control station communication contact, control hydraulic pressure and the middle solenoid directional control valve a (38) of air compression system (16) by the device control system (17) of hiding again, oil pump (39), solenoid directional control valve b(42) with low pressure gaholder (18), air pump (43) makes air bag (24), and front and back volume convs (15) (25), (19) volume changes, seawater can be from drain gutter group (5) everywhere, (7), (9), (11) turnover, reaching facing upward of device body (8) bows, left right balanced purpose.
As shown in Figure 2: the lower end of the utility model device body (8) be provided with torpedo-launching cabin pipe (12) and with torpedo-launching control setup (22) Electricity Federation, the inside of device body (8) is provided with data processing system (13) and propeller control system (20), torpedo-launching control setup (22) Electricity Federation, battery pack (21) and data processing system (13) Electricity Federation, data processing system (13) and signal acquiring system (23) Electricity Federation, when receiving signal acquiring system (23) data, data processing system (13) arrives continental rise station or near naval vessels command signal through information processing or terminal buoy (2) transmitting-receiving via satellite, can control torpedo-launching control setup (22) drives propelling unit (1) to realize automatic tracing with propeller control system (20), approach, the purpose struck target.
In addition, signal acquiring system (23) is mainly to utilize magnetic field, pressure sensor, the underwater acoustic technology automatic search, pass through again data processing system (13) and control the purpose that propeller control system (20) reaches the diving tracking of swimming, once find that not clear naval vessels or submarine are close, accept tracking with continental rise station or near naval vessels control station exchange message immediately, attack, sink-float, and next communication time instruction, then, recover ICBM SHF satellite terminal buoy (2) interruption and continental rise station or near naval vessels control station communication contact and reach hidden purpose, and torpedo-launching control setup (22) is sent to instruction reach target of attack.
Claims (8)
1. the floating type diving equipment of torpedo-launching automatically comprises:
The ICBM SHF satellite terminal buoy, the trailing aerial cable, antenna is recovered cabin, floating wing, the device body, torpedo-launching cabin pipe, propelling unit, its feature:
A, be provided with two left floating wings (6), right floating wing (10) on device body (8) surface, and (12) are managed in a propelling unit (1), ICBM SHF satellite terminal buoy (2), trailing aerial cable (3), antenna recovery cabin (4) and front drain gutter group (5), left bank water hole group (7), right drain gutter group (9), rear drain gutter group (11), torpedo-launching cabin; Wherein ICBM SHF satellite terminal buoy (2), with trailing aerial cable (3) Electricity Federation, pass through again in antenna recovery cabin (4) and device body (8) and be provided with data processing system (13) Electricity Federation, with timer body (8) with left floating wing (6), right floating wing (10) arranged, axle connects; Propeller control system (20) and data processing system (13) Electricity Federation, propelling unit (1) connects with device body (8), propeller control system (20) axle, and front drain gutter group (5), rear drain gutter group (11) communicate with front volume conv sea water tank interface (28), rear volume conv sea water tank interface (35) respectively;
B is provided with data processing system (13), propeller control system (20), battery pack (21), torpedo-launching control setup (22), signal acquiring system (23) in device body (8); Wherein signal acquiring system (23) and data processing system (13) Electricity Federation, data processing system (13) and propeller control system (20) Electricity Federation, data processing system (13) also respectively with hydraulic pressure and air compression system (16), device hide control system (17), battery pack (21), torpedo-launching control setup (22) Electricity Federation.
2. the floating type diving equipment of a kind of torpedo-launching automatically as claimed in claim 1, is characterized in that: in device body (8), be outside equipped with ICBM SHF satellite terminal buoy (2), signal acquiring system (23) data processing system (13); Wherein signal acquiring system (23) and data processing system (13) Electricity Federation, data processing system (13) and ICBM SHF satellite terminal buoy (2) Electricity Federation.
3. the floating type diving equipment of a kind of torpedo-launching automatically as claimed in claim 1 or 2, it is characterized in that: data processing system (13) and propeller control system (20), torpedo-launching control setup (22) Electricity Federation, battery pack (21) and data processing system (13) Electricity Federation.
4. the floating type diving equipment of a kind of torpedo-launching automatically as claimed in claim 1 is characterized in that: left floating wing (6), the inner wing arranged of right floating wing (10) be left inside puts the right inside solenoid directional control valve a(42 put in air bag (25) and hydraulic pressure and air compression system (16) of air bag (24), wing), check valve (44), air pump (43) gas company.
5. the floating type diving equipment of a kind of torpedo-launching automatically as claimed in claim 1 is characterized in that: data processing system (13) also respectively with hydraulic pressure and air compression system (16), device control system (17) Electricity Federation of hiding.
6. the floating type diving equipment of a kind of torpedo-launching automatically as claimed in claim 1 is characterized in that: also be provided with high-pressure gas cylinder (14), hydraulic pressure and air compression system (16), device hide control system (17), low pressure gaholder (18), front volume conv (15), rear volume conv (19) in device body (8), wherein high-pressure gas cylinder (14) connects with hydraulic pressure and air compression system (16) gas, hydraulic pressure and air compression system (16) and front volume conv (15), front volume conv air tank interface (27) in rear volume conv (19), rear volume conv air tank interface (26) gas connects, hydraulic pressure and air compression system (16) and front volume conv (15), front volume conv rod chamber oil circuit interface (29) in rear volume conv (19), rear volume conv rod chamber oil circuit interface (36), front volume conv rodless cavity oil circuit interface (30), rear volume conv rodless cavity oil circuit interface (37) oil circuit connects, hydraulic pressure and air compression system (16) and the left inside air bag (24) of putting of wing, right inside air bag (25) gas of putting of wing connects, solenoid directional control valve a(38 in hydraulic pressure and air compression system (16)), solenoid directional control valve b(42) with the device control system (17) of hiding, be electrically connected.
7. the floating type diving equipment of a kind of torpedo-launching automatically as claimed in claim 6, it is characterized in that: in front volume conv (15), rear volume conv (19), cylinder body (34) connects with hydraulic cylinder piston rod (32) bar, and hydraulic cylinder piston (31), pneumatic cylinder piston (33) connect with hydraulic cylinder piston rod (32) axle.
8. the floating type diving equipment of a kind of torpedo-launching automatically as claimed in claim 1 is characterized in that: solenoid directional control valve a(38), solenoid directional control valve b(42), oil pump (39), air pump (43) and device control system (17) Electricity Federation of hiding.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220628114 CN203345188U (en) | 2012-11-26 | 2012-11-26 | Floating-type diving gear capable of automatically emitting torpedo |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220628114 CN203345188U (en) | 2012-11-26 | 2012-11-26 | Floating-type diving gear capable of automatically emitting torpedo |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203345188U true CN203345188U (en) | 2013-12-18 |
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ID=49745114
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220628114 Expired - Fee Related CN203345188U (en) | 2012-11-26 | 2012-11-26 | Floating-type diving gear capable of automatically emitting torpedo |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203345188U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112882038A (en) * | 2021-01-11 | 2021-06-01 | 太原理工大学 | Horizontal salt cavern form detector, remote monitoring detection system and remote detection method |
| CN114148490A (en) * | 2021-11-29 | 2022-03-08 | 海鹰企业集团有限责任公司 | Flexible wing towed body with foldable function |
-
2012
- 2012-11-26 CN CN 201220628114 patent/CN203345188U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN112882038A (en) * | 2021-01-11 | 2021-06-01 | 太原理工大学 | Horizontal salt cavern form detector, remote monitoring detection system and remote detection method |
| CN114148490A (en) * | 2021-11-29 | 2022-03-08 | 海鹰企业集团有限责任公司 | Flexible wing towed body with foldable function |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20131218 Termination date: 20141126 |
|
| EXPY | Termination of patent right or utility model |