CN108891565A - It is a kind of can air-sea switching submarine - Google Patents
It is a kind of can air-sea switching submarine Download PDFInfo
- Publication number
- CN108891565A CN108891565A CN201810940642.8A CN201810940642A CN108891565A CN 108891565 A CN108891565 A CN 108891565A CN 201810940642 A CN201810940642 A CN 201810940642A CN 108891565 A CN108891565 A CN 108891565A
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- Prior art keywords
- fuselage
- submarine
- air
- motor
- output shaft
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60F—VEHICLES FOR USE BOTH ON RAIL AND ON ROAD; AMPHIBIOUS OR LIKE VEHICLES; CONVERTIBLE VEHICLES
- B60F5/00—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media
- B60F5/02—Other convertible vehicles, i.e. vehicles capable of travelling in or on different media convertible into aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
- B63G8/08—Propulsion
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63G—OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
- B63G8/00—Underwater vessels, e.g. submarines; Equipment specially adapted therefor
- B63G8/001—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations
- B63G2008/002—Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations unmanned
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Toys (AREA)
Abstract
The invention discloses it is a kind of can air-sea switching submarine,Including fuselage and single-chip microcontroller,The fuselage side is provided with starboard wing,The starboard wing bottom is provided with right aircraft engine,The fuselage other side is provided with port wing,The port wing bottom is provided with left aircraft engine,The fuselage two sides are provided with floating plate,Air bag is provided on the floating plate,The fuselage roof is provided with ventilation head,Headlamp is provided on the fuselage,The headlamp bottom is provided with camera,Motor one is provided in the fuselage,Output shaft one is provided on the motor one,Propeller one is provided on the output shaft one,One side of motor is provided with motor two,Output shaft two is provided on the motor two,Propeller two is provided on the output shaft two,This can air-sea switching Submarine Structure design it is reasonable,It can carry out the work of the underwater and water surface,It is practical.
Description
Technical field
The present invention be it is a kind of can air-sea switching submarine, belong to unmanned plane Submarine Equipment technical field.
Background technique
Underwater UAV is to utilize radio robot and the presetting apparatus provided for oneself referred to as " unmanned plane "
The not manned undersea search machine of manipulation, main function is that explorations is monitored to the external world, and midget submarine is mainly work under water
Make, to carrying out exploration use under water, for present unmanned plane is with midget submarine, typically respectively carries out using can not
Meet coefficient effect, level of application is caused to be subject to certain restrictions, it is not very practical, for unmanned plane and midget submarine
For, underwater operation on the one hand can only be carried out, can not be worked in the water surface, not very practical, exploration range is smaller, Er Qiegong
Make inefficient, on the other hand cannot be combined use, need to be used separately, cause manufacturing cost excessively high, and operates tired
Difficulty cannot change position well, cause when being worked, the not high problem of working efficiency.
It would therefore be desirable to it is a kind of can the submarine of air-sea switching bring help to solve the above problems.
Summary of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide it is a kind of can air-sea switching submarine, on solving
The problem of proposing in background technique is stated, the present invention is novel in design, and underwater unmanned plane and submarine mixing arrangement, practicability is high, work
Effect is good.
To achieve the above object, the present invention provides the following technical solutions：It is a kind of can air-sea switching submarine, including fuselage and
Single-chip microcontroller, the fuselage are equipped with flying power mechanism and submarine power mechanism, and it is flying power mechanism that the fuselage, which is equipped with,
With the battery of submarine power mechanism power supply.
The fuselage is equipped with collecting mechanism, and collecting mechanism includes the lifting chamber on fuselage, and the lifting is intracavitary to be set
It is equipped with elevating lever, collection head is provided on the elevating lever, the lifting chamber side is provided with water pump, setting at the top of the water pump
Have drinking-water pipe, be provided with solenoid valve one on the drinking-water pipe, the water pump bottom is provided with water inlet pipe, the lifting chamber by into
Water pipe is connect with water pump；
The fuselage is equipped with the inflatable structure matched with air bag, and inflatable structure includes air pump, and the air pump side is provided with
Air inlet pipe, the air bag are connect by air inlet pipe with air pump, and the air pump other side is provided with exhaust tube, and the ventilation head passes through
Exhaust tube is connect with air pump, and solenoid valve two is provided on the exhaust tube；
The single-chip microcontroller includes monitoring device, control device and data transmission device, the monitoring device include hydraulic pressure sensor,
Water depth sensor, infrared sensor and luminosity sensor, the hydraulic pressure sensor setting is in fuselage bottom, the depth of water sensing
Device is arranged at the top of floating plate, and the infrared sensor is arranged at the top of headlamp, and the luminosity sensor setting is imaging
Head bottom, the control device include solenoid valve one, solenoid valve two, solenoid valve three, solenoid valve four, solenoid valve five, power supply valve one,
Power supply valve two, power supply valve three and power supply valve four, the solenoid valve three are arranged on submarine engine, and the setting of solenoid valve four exists
On left aircraft engine, the solenoid valve five is arranged on right aircraft engine, and the power supply valve one is arranged on motor one,
The power supply valve two is arranged on motor two, and the power supply valve three is arranged on motor three, and the setting of power supply valve four exists
On headlamp, the data transmission device includes operating terminal.
As a kind of preferred embodiment of the invention, active carbon layer, flying power mechanism are provided on the battery
Starboard wing including being located at fuselage side, the starboard wing bottom are provided with right aircraft engine, the fuselage other side setting
There is port wing, the port wing bottom is provided with left aircraft engine, and the fuselage two sides are provided with floating plate, the floating plate
On be provided with air bag.
As a kind of preferred embodiment of the invention, in the output shaft one, output shaft two, output shaft three and rotation axis
It is arranged with collision mat, submarine power mechanism includes the motor one on fuselage, is provided with output on the motor one
Axis one is provided with propeller one on the output shaft one, and one side of motor is provided with motor two, the motor two
On be provided with output shaft two, propeller two is provided on the output shaft two, the submarine power mechanism further includes motor three,
It is provided with output shaft three on the motor three, propeller three is provided on the output shaft three, three side of motor is set
It is equipped with submarine engine, rotation axis is provided on the submarine engine, is provided with power blade in the rotation axis.
As a kind of preferred embodiment of the invention, the fuselage roof is provided with ventilation head, and the fuselage head is set
It is equipped with headlamp, the headlamp bottom is provided with camera, is provided with transparent panel on headlamp.
As a kind of preferred embodiment of the invention, rubber ring is arranged on the elevating lever.
As a kind of preferred embodiment of the invention, the left aircraft engine, right aircraft engine, floating plate are gentle
The quantity of capsule is 2.
As a kind of preferred embodiment of the invention, the battery passes through electric wire and motor one, motor two, electricity
Motivation three, water pump, air pump are connected with headlamp.
Beneficial effects of the present invention：
1. this can the submarine of air-sea switching mixed structure design is carried out using underwater unmanned plane and midget submarine, can be effectively combined
The function of underwater unmanned plane and midget submarine works, and practical, work efficiency is high.
2. this can the submarine of air-sea switching worked with submarine engine using aircraft engine, make device in operation
More convenient, multiple propellers are capable of the position of effective ensuring equipment movement, easy to use efficient.
3. this can air-sea switching Submarine Design it is novel, practicability is high, has good development prospect.
Detailed description of the invention
Fig. 1 be one kind of the present invention can air-sea switching submarine structural schematic diagram；
Fig. 2 be one kind of the present invention can air-sea switching submarine cross-sectional view；
Fig. 3 be one kind of the present invention can air-sea switching submarine system block diagram；
In figure：1- fuselage, 2- starboard wing, 3- port wing, the right aircraft engine of 4-, the left aircraft engine of 5-, 6- floating plate, 7- are logical
Gas head, 8- headlamp, 9- camera, 10- motor one, 11- output shaft one, 12- propeller one, 13- motor two, 14- are defeated
Shaft two, 15- propeller two, 16- lifting chamber, 17- elevating lever, 18- water pump, 19- water inlet pipe, 20- drinking-water pipe, 21- battery,
22- air pump, 23- air inlet pipe, 24- exhaust tube, 25- motor three, 26- output shaft three, 27- propeller three, 28- submarine start
Machine, 29- rotation axis, 30- power blade, 31- collect head, 32- hydraulic pressure sensor, 33- water depth sensor, 34- infrared ray sensing
Device, 35- luminosity sensor, 36- monitoring device, 37- single-chip microcontroller, 38- control device, 39- data transmission device, 40- operation are eventually
End, 41- solenoid valve one, 42- solenoid valve two, 43- solenoid valve three, 44- solenoid valve four, 45- solenoid valve five, 46- power supply valve one,
47- power supply valve two, 48- power supply valve three, 49- power supply valve four.
Specific embodiment
Following will be combined with the drawings in the embodiments of the present invention, and technical solution in the embodiment of the present invention carries out clear, complete
Site preparation description, it is clear that described embodiments are only a part of the embodiments of the present invention, instead of all the embodiments.It is based on
Embodiment in the present invention, it is obtained by those of ordinary skill in the art without making creative efforts every other
Embodiment shall fall within the protection scope of the present invention.
Embodiment 1
Fig. 1-3 is please referred to, the present invention provides a kind of technical solution：It is a kind of can air-sea switching submarine, including fuselage 1 and single-chip microcontroller
37, the fuselage 1 is equipped with flying power mechanism and submarine power mechanism, and the fuselage 1 is equipped with battery 21；
Flying power mechanism includes the starboard wing 2 positioned at 1 side of fuselage, and 2 bottom of starboard wing is provided with right aircraft engine
4,1 other side of fuselage is provided with port wing 3, and 3 bottom of port wing is provided with left aircraft engine 5,1 liang of the fuselage
Side is provided with floating plate 6, is provided with air bag on the floating plate 6；
Ventilation head 7 is provided at the top of the fuselage 1,1 head of fuselage is provided with headlamp 8,8 bottom of the headlamp setting
There is camera 9, the fuselage 1 is equipped with；
Submarine power mechanism includes the motor 1 on fuselage 1, is provided with output shaft 1 on the motor 1,
Propeller 1 is provided on the output shaft 1, one 10 side of motor is provided with motor 2 13, described electronic
It is provided with output shaft 2 14 on machine 2 13, propeller 2 15 is provided on the output shaft 2 14, the submarine power mechanism is also
Including motor 3 25, it is provided with output shaft 3 26 on the motor 3 25, is provided with propeller on the output shaft 3 26
3 27,3 25 side of motor is provided with submarine engine 28, and rotation axis 29, institute are provided on the submarine engine 28
It states and is provided with power blade 30 in rotation axis 29；
The fuselage 1 is equipped with collecting mechanism, and collecting mechanism includes the lifting chamber 16 on the fuselage 1, in the lifting chamber 16
It is provided with elevating lever 17, is provided on the elevating lever 17 and collects head 31,16 side of lifting chamber is provided with water pump 18, described
It is provided with drinking-water pipe 20 at the top of water pump 18, solenoid valve 1 is provided on the drinking-water pipe 20,18 bottom of water pump is provided with
Water inlet pipe 19, the lifting chamber 16 are connect by water inlet pipe 19 with water pump 18；
The fuselage 1 is equipped with the inflatable structure matched with air bag, and inflatable structure includes air pump 22, and 22 side of air pump is set
It is equipped with air inlet pipe 23, the air bag is connect by air inlet pipe 23 with air pump 22, and 22 other side of air pump is provided with exhaust tube 24,
The ventilation head 7 is connect by exhaust tube 24 with air pump 22, is provided with solenoid valve 2 42 on the exhaust tube 24；
The single-chip microcontroller 37 includes monitoring device 36, control device 38 and data transmission device 39, and the monitoring device 36 includes
Hydraulic pressure sensor 32, water depth sensor 33, infrared sensor 34 and luminosity sensor 35, the setting of hydraulic pressure sensor 32 exist
1 bottom of fuselage, the setting of water depth sensor 33 are pushed up in 6 top of floating plate, the setting of infrared sensor 34 in headlamp 8
Portion, the luminosity sensor 35 setting in 9 bottom of camera, the control device 38 include solenoid valve 1, solenoid valve 2 42,
Solenoid valve 3 43, solenoid valve 4 44, solenoid valve 5 45, power supply valve 1, power supply valve 2 47, power supply valve 3 48 and power supply valve four
49, the solenoid valve 3 43 is arranged on submarine engine 28, and the solenoid valve 4 44 is arranged on left aircraft engine 5, institute
It states solenoid valve 5 45 to be arranged on right aircraft engine 4, the power supply valve 1 is arranged on motor 1, the power supply valve
2 47 are arranged on motor 2 13, and the power supply valve 3 48 is arranged on motor 3 25, and the setting of power supply valve 4 49 exists
On headlamp 8, the data transmission device 39 includes operating terminal 40.
As a kind of preferred embodiment of the invention, active carbon layer is provided on the battery 21.
As a kind of preferred embodiment of the invention, the output shaft 1, output shaft 2 14, output shaft 3 26 and turn
Collision mat is arranged on moving axis 29.
As a kind of preferred embodiment of the invention, transparent panel is provided on the headlamp 8.
As a kind of preferred embodiment of the invention, rubber ring is arranged on the elevating lever 17.
As a kind of preferred embodiment of the invention, the left aircraft engine 5, right aircraft engine 4, floating plate 6
Quantity with air bag is 2.
As a kind of preferred embodiment of the invention, the battery 21 passes through electric wire and motor 1, motor
2 13, motor 3 35, water pump 18, air pump 22 and headlamp 8 connect.
Working principle：Using this can air-sea switching submarine when, battery 21 provides required electric energy for the present apparatus first,
When mixing arrangement ontology works under water, solenoid valve 3 43 is opened, and submarine engine 28 works, and drives 29 turns of rotation axis
Dynamic, rotation axis 29 drives power blade 30 to be rotated, and the rotation of power blade 30 is that fuselage 1 provides forward power, the depth of water
Sensor 33 can monitor the depth of mixing arrangement ontology, then be transferred to operating terminal 40 by data transmission device 39, when mixed
It when conjunction device noumenon needs to rise, is operated by operating terminal 40, power supply valve 2 47 is opened, and motor 2 13 starts work
Make, motor 2 13 drives output shaft 2 14 to rotate, and output shaft 2 14 drives propeller 2 15 to start turning, and propeller 2 15 is
1 head of fuselage provides upward power, is moved up, while the opening of valve 3 48 of powering, motor 3 25 are started to work, electricity
Motivation 3 25 drives output shaft 3 26 to start turning, and output shaft 3 26 drives propeller 3 27 to start turning, and propeller 3 27 is
1 tail portion of fuselage provides upward power, increase fuselage 1, when depth transducer 33 monitors that fuselage 1 reaches designated depth,
The revolving speed that motor 2 13 and motor 3 25 are controlled by operating terminal 40, makes fuselage 1 reach balance in the depth, works as depth
When sensor 33 monitors that fuselage 1 needs to decline, power supply valve 1 is opened, and motor 1 is started to work, one 10 band of motor
Dynamic output shaft 1 starts turning, and output shaft 1 drives propeller 1 to start turning, and propeller 1 is that 1 head of fuselage mentions
For power, move down fuselage 1, when depth transducer 33 monitors that depth is suitable, power supply valve 1 is closed, motor one
10 stop working, and it is headlamp that when luminosity sensor 35 monitors that light is poor, power supply valve 4 49, which is opened, and headlamp 8 lights
The camera 9 of 8 bottoms provides illumination, and the picture of camera 9 is transferred in operating terminal 40 by data transmission device 39, convenient
Operator operates, and when needing to collect information, water pump 18 is started to work, and the solenoid valve 1 on drinking-water pipe 20 is opened,
Water pump 18 is drawn water by 20 pairs of external worlds of drinking-water pipe, and water is entered in lifting chamber 16 by the water inlet pipe 19 on water pump 18, is squeezed
The elevating lever 17 gone up and down in chamber 16 rises, and the collection head 31 on elevating lever 17 rises, and then collects 31 pairs of external worlds of head and carries out information
Collection and storage, after information is collected, water pump 18 is drawn water by 19 pairs of lifting chambers 16 of water inlet pipe, passes through drinking-water pipe
20 are drained, and elevating lever 17 drives collection head 31 to return to original place, and solenoid valve 1 is closed, and hydraulic pressure sensor 32 can be supervised effectively
The pressure for surveying fuselage 1, prevent from declining because of fuselage 1 it is too deep lead to the case where being damaged by pressure by hydraulic pressure, when infrared sensor 34 is supervised
When measuring front has barrier, solenoid valve 3 43 is closed, and submarine engine 28 stops working, and fuselage 1 halts, and passes through change
The revolving speed of motor 2 13 and motor 3 25 is adjusted the direction of fuselage operation, when mixing arrangement ontology needs on the water surface
When being worked, fuselage 1 is set to emerge by motor 2 13 and motor 3 25, when water depth sensor 33 monitors fuselage
When the 1 arrival water surface, air pump 22 is started to work, and the solenoid valve 2 42 on exhaust tube 24 is opened, and air pump 22 is external by exhaust tube 24
Boundary is evacuated, and is then inflated by air inlet pipe 23 to the air bag on floating plate 6, after inflation, solenoid valve 2 42
It closes, the buoyancy and 1 self gravity of fuselage of air bag and floating plate 6 balance, and fuselage 1 is swum on the water surface, power valve 2 47 and confession
Electric valve 3 48 is closed, and motor 2 13 and motor 3 25 stop working, and propeller 2 15 and propeller 3 27 stop operating, electricity
Magnet valve 3 43 is closed, and submarine engine 28 stops working, and power blade 30 stops operating, solenoid valve 4 44 and solenoid valve 5 45 dozens
It opens, left aircraft engine 5 and right aircraft engine 4 are started to work, and are provided power for fuselage 1, are moved on fuselage 1, when need
When turning, the revolving speed of left aircraft engine 5 and right aircraft engine 4 is controlled respectively by operating terminal 40, to reach
To the effect of steering, port wing 3 and starboard wing 2 can effectively reduce 1 self gravity of fuselage when fuselage 1 moves, and make movement more
Add conveniently, rationally, good working effect is easy to operate, practical for links design of the present invention.
Embodiment 2
It is with what embodiment 1 distinguished：The model 80C51 of the single motor 37.
The above shows and describes the basic principles and main features of the present invention and the advantages of the present invention, for this field skill
For art personnel, it is clear that invention is not limited to the details of the above exemplary embodiments, and without departing substantially from spirit of the invention or
In the case where essential characteristic, the present invention can be realized in other specific forms.Therefore, in all respects, should all incite somebody to action
Embodiment regards exemplary as, and is non-limiting, the scope of the present invention by appended claims rather than on state
Bright restriction, it is intended that including all changes that fall within the meaning and scope of the equivalent elements of the claims in the present invention
It is interior.Any reference signs in the claims should not be construed as limiting the involved claims.
In addition, it should be understood that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
It considers the specification as a whole, the technical solutions in the various embodiments may also be suitably combined, forms those skilled in the art
The other embodiments being understood that.
Claims (9)
1. one kind can air-sea switching submarine, which is characterized in that including fuselage（1）And single-chip microcontroller（37）, the fuselage（1）On set
There are flying power mechanism and submarine power mechanism, the fuselage（1）It is equipped with and is supplied for flying power mechanism and submarine power mechanism
The battery of electricity（21）；
The single-chip microcontroller（37）Including monitoring device（36）, control device（38）And data transmission device（39）；
The monitoring device（36）Including hydraulic pressure sensor（32）, water depth sensor（33）, infrared sensor（34）And luminosity
Sensor（35）, the hydraulic pressure sensor（32）It is arranged in fuselage（1）Bottom；
The control device（38）Including solenoid valve one（41）, solenoid valve two（42）, solenoid valve three（43）, solenoid valve four（44）,
Solenoid valve five（45）, power supply valve one（46）, power supply valve two（47）, power supply valve three（48）With power supply valve four（49）, the data biography
Defeated device（39）Including operating terminal（40）.
2. one kind according to claim 1 can air-sea switching submarine, it is characterised in that：Work is provided on the battery
Property layer of charcoal, flying power mechanism include be located at fuselage（1）The starboard wing of side（2）, the starboard wing（2）Bottom is provided with right fly
Machine engine（4）, the fuselage（1）The other side is provided with port wing（3）, the port wing（3）Bottom is provided with left aircraft hair
Motivation（5）, the fuselage（1）Two sides are provided with floating plate（6）, the floating plate（6）On be provided with air bag.
3. one kind according to claim 1 can air-sea switching submarine, it is characterised in that：The output shaft one, output shaft
Two, it is arranged with collision mat in output shaft three and rotation axis, submarine power mechanism includes being located at fuselage（1）On motor one
（10）, the motor one（10）On be provided with output shaft one（11）, the output shaft one（11）On be provided with propeller one
（12）, the motor one（10）Side is provided with motor two（13）, the motor two（13）On be provided with output shaft two
（14）, the output shaft two（14）On be provided with propeller two（15）, the submarine power mechanism further includes motor three（25）,
The motor three（25）On be provided with output shaft three（26）, the output shaft three（26）On be provided with propeller three（27）, institute
State motor three（25）Side is provided with submarine engine（28）, the submarine engine（28）On be provided with rotation axis（29）,
The rotation axis（29）On be provided with power blade（30）.
4. one kind according to claim 1 can air-sea switching submarine, it is characterised in that：The fuselage（1）Top setting
There is ventilation head（7）, the fuselage（1）Head is provided with headlamp（8）, the headlamp（8）Bottom is provided with camera（9）,
Transparent panel is provided on headlamp.
5. one kind according to claim 1 can air-sea switching submarine, it is characterised in that：Rubber is arranged on the elevating lever
Cushion rubber.
6. one kind according to claim 2 can air-sea switching submarine, it is characterised in that：The left aircraft engine, the right side
The quantity of aircraft engine, floating plate and air bag is 2.
7. one kind according to claim 1 can air-sea switching submarine, it is characterised in that：The fuselage（1）It is equipped with and receives
Collecting mechanism, collecting mechanism include being located at fuselage（1）On lifting chamber（16）, the lifting chamber（16）Inside it is provided with elevating lever
（17）, the elevating lever（17）On be provided with collection head（31）, the lifting chamber（16）Side is provided with water pump（18）, the water
Pump（18）Top is provided with drinking-water pipe（20）, the drinking-water pipe（20）On be provided with solenoid valve one（41）, the water pump（18）Bottom
Portion is provided with water inlet pipe（19）, the lifting chamber（16）Pass through water inlet pipe（19）With water pump（18）Connection.
8. one kind according to claim 2 can air-sea switching submarine, it is characterised in that：The fuselage（1）Be equipped with
The inflatable structure that air bag matches, inflatable structure include air pump（22）, the air pump（22）Side is provided with air inlet pipe（23）, institute
It states air bag and passes through air inlet pipe（23）With air pump（22）Connection, the air pump（22）The other side is provided with exhaust tube（24）, described logical
Gas head（7）Pass through exhaust tube（24）With air pump（22）Connection, the exhaust tube（24）On be provided with solenoid valve two（42）.
9. according to claim 1-8 it is any it is described it is a kind of can air-sea switching submarine, it is characterised in that：The single motor
（37）Model 80C51.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810940642.8A CN108891565A (en) | 2018-08-17 | 2018-08-17 | It is a kind of can air-sea switching submarine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810940642.8A CN108891565A (en) | 2018-08-17 | 2018-08-17 | It is a kind of can air-sea switching submarine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108891565A true CN108891565A (en) | 2018-11-27 |
Family
ID=64354736
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810940642.8A Withdrawn CN108891565A (en) | 2018-08-17 | 2018-08-17 | It is a kind of can air-sea switching submarine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108891565A (en) |
-
2018
- 2018-08-17 CN CN201810940642.8A patent/CN108891565A/en not_active Withdrawn
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Application publication date: 20181127 |