CN108860529A - A kind of underwater unmanned plane and midget submarine mixing arrangement - Google Patents

A kind of underwater unmanned plane and midget submarine mixing arrangement Download PDF

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Publication number
CN108860529A
CN108860529A CN201810940665.9A CN201810940665A CN108860529A CN 108860529 A CN108860529 A CN 108860529A CN 201810940665 A CN201810940665 A CN 201810940665A CN 108860529 A CN108860529 A CN 108860529A
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CN
China
Prior art keywords
motor
fuselage
output shaft
solenoid valve
unmanned plane
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Withdrawn
Application number
CN201810940665.9A
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Chinese (zh)
Inventor
林建斌
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Quangang Qimiao Industrial Design Services Center
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Quangang Qimiao Industrial Design Services Center
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Filing date
Publication date
Application filed by Quangang Qimiao Industrial Design Services Center filed Critical Quangang Qimiao Industrial Design Services Center
Priority to CN201810940665.9A priority Critical patent/CN108860529A/en
Publication of CN108860529A publication Critical patent/CN108860529A/en
Withdrawn legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63CLAUNCHING, HAULING-OUT, OR DRY-DOCKING OF VESSELS; LIFE-SAVING IN WATER; EQUIPMENT FOR DWELLING OR WORKING UNDER WATER; MEANS FOR SALVAGING OR SEARCHING FOR UNDERWATER OBJECTS
    • B63C11/00Equipment for dwelling or working underwater; Means for searching for underwater objects
    • B63C11/52Tools specially adapted for working underwater, not otherwise provided for
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/08Propulsion
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63GOFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS; MINE-LAYING; MINE-SWEEPING; SUBMARINES; AIRCRAFT CARRIERS
    • B63G8/00Underwater vessels, e.g. submarines; Equipment specially adapted therefor
    • B63G8/001Underwater vessels adapted for special purposes, e.g. unmanned underwater vessels; Equipment specially adapted therefor, e.g. docking stations
    • B63G2008/002Underwater 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)
  • Ocean & Marine Engineering (AREA)
  • Toys (AREA)

Abstract

The invention discloses a kind of underwater unmanned planes and midget submarine mixing arrangement,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,The underwater unmanned plane and midget submarine mixing arrangement are reasonable in design,It can carry out the work of the underwater and water surface,It is practical.

Description

A kind of underwater unmanned plane and midget submarine mixing arrangement
Technical field
The present invention is a kind of underwater unmanned plane and midget submarine mixing arrangement, belongs 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 which a kind of underwater unmanned plane brings help to solve the above problems with midget submarine mixing arrangement.
Summary of the invention
In view of the deficienciess of the prior art, it is an object of the present invention to provide a kind of underwater unmanned planes to mix dress with midget submarine It sets, to solve the problems mentioned in the above background technology, the present invention is novel in design, and underwater unmanned plane and submarine mixing arrangement are real With property height, good working effect.
To achieve the above object, the present invention provides the following technical solutions:A kind of underwater unmanned plane mixes dress with midget submarine It sets, including fuselage and single-chip microcontroller, the fuselage side is provided with starboard wing, and the starboard wing bottom is provided with right aircraft engine Machine, the fuselage other side are provided with port wing, and the port wing bottom is provided with left aircraft engine, and the fuselage two sides are set It is equipped with floating plate, air bag is provided on the floating plate, the fuselage roof is provided with ventilation head, is provided with photograph on the fuselage Bright lamp, the headlamp bottom are provided with camera, and motor one is provided in the fuselage, is provided on the motor one Output shaft one is provided with propeller one on the output shaft one, and one side of motor is provided with motor two, described electronic It is provided with output shaft two on machine two, propeller two is provided on the output shaft two, two side of motor is provided with electric power storage Pond, the battery top are provided with lifting chamber, and the lifting is intracavitary to be provided with elevating lever, and collection is provided on the elevating lever Head, the lifting chamber side are provided with water pump, are provided with drinking-water pipe at the top of the water pump, are provided with solenoid valve on the drinking-water pipe One, the water pump bottom is provided with water inlet pipe, and the lifting chamber is connect by water inlet pipe with water pump, the battery side setting There is air pump, the air pump side is provided with air inlet pipe, and the air bag is connect by air inlet pipe with air pump, and the air pump other side is set It is equipped with exhaust tube, the ventilation head is connect by exhaust tube with air pump, and solenoid valve two, the air pump are provided on the exhaust tube Side is provided with motor three, and output shaft three is provided on the motor three, is provided with propeller three on the output shaft three, Three side of motor is provided with submarine engine, and rotation axis is provided on the submarine engine, is set in the rotation axis It is equipped with power blade, the single-chip microcontroller includes monitoring device, control device and data transmission device, and the monitoring device includes water Pressure sensor, water depth sensor, infrared sensor and luminosity sensor, the hydraulic pressure sensor are arranged in fuselage bottom, institute It states water depth sensor to be arranged at the top of floating plate, the infrared sensor is arranged at the top of headlamp, the luminosity sensor It is arranged in camera bottom, the control device includes 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, the electricity Magnet valve four is arranged on left aircraft engine, and 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, the confession Electric valve four is arranged on headlamp, and the data transmission device includes operating terminal.
As a kind of preferred embodiment of the invention, active carbon layer is provided on the battery.
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.
As a kind of preferred embodiment of the invention, transparent panel is provided on the 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 model 80C51 of the single motor.
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. the underwater unmanned plane and midget submarine mixing arrangement carry out mixed structure design using underwater unmanned plane and midget submarine, The function that underwater unmanned plane and midget submarine can be effectively combined works, practical, and work efficiency is high.
2. the underwater unmanned plane is worked using aircraft engine with submarine engine with midget submarine mixing arrangement, make Device is more convenient in operation, and multiple propellers are capable of the position of effective ensuring equipment movement, easy to use efficient.
3. the underwater unmanned plane and midget submarine mixing arrangement are novel in design, practicability is high, has good development prospect.
Detailed description of the invention
Fig. 1 is a kind of structural schematic diagram of underwater unmanned plane and midget submarine mixing arrangement of the present invention;
Fig. 2 is a kind of cross-sectional view of underwater unmanned plane and midget submarine mixing arrangement of the present invention;
Fig. 3 is a kind of system block diagram of underwater unmanned plane and midget submarine mixing arrangement of the present invention;
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.
Fig. 1-3 is please referred to, the present invention provides a kind of technical solution:A kind of underwater unmanned plane and midget submarine mixing arrangement, Including fuselage 1 and single-chip microcontroller 37,1 side of fuselage is provided with starboard wing 2, and 2 bottom of starboard wing is provided with right aircraft hair Motivation 4,1 other side of fuselage are provided with port wing 3, and 3 bottom of port wing is provided with left aircraft engine 5, the machine 1 two sides of body are provided with floating plate 6, and air bag is provided on the floating plate 6, and ventilation head 7 is provided at the top of the fuselage 1, described Headlamp 8 is provided on fuselage 1,8 bottom of headlamp is provided with camera 9, is provided with motor one in the fuselage 1 10, output shaft 1 is provided on the motor 1, and propeller 1 is provided on the output shaft 1, it is described electronic One 10 side of machine is provided with motor 2 13, is provided with output shaft 2 14 on the motor 2 13, on the output shaft 2 14 It is provided with propeller 2 15,2 13 side of motor is provided with battery 21, is provided with lifting at the top of the battery 21 Chamber 16 is provided with elevating lever 17 in the lifting chamber 16, is provided on the elevating lever 17 and collects head 31, the lifting chamber 16 1 Side is provided with water pump 18, and drinking-water pipe 20 is provided at the top of the water pump 18, solenoid valve 1, institute are provided on the drinking-water pipe 20 It states 18 bottom of water pump and is provided with water inlet pipe 19, the lifting chamber 16 is connect by water inlet pipe 19 with water pump 18, the battery 21 Side is provided with air pump 22, and 22 side of air pump is provided with air inlet pipe 23, and the air bag is connected by air inlet pipe 23 and air pump 22 It connects, 22 other side of air pump is provided with exhaust tube 24, and the ventilation head 7 is connect by exhaust tube 24 with air pump 22, the pumping Solenoid valve 2 42 is provided on tracheae 24,22 side of air pump is provided with motor 3 25, is arranged on the motor 3 25 There is output shaft 3 26, propeller 3 27 is provided on the output shaft 3 26,3 25 side of motor is provided with submarine hair Motivation 28 is provided with rotation axis 29 on the submarine engine 28, power blade 30, the list is provided in the rotation axis 29 Piece machine 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 hydraulic pressure sensor 32 are arranged in 1 bottom of fuselage, The setting of water depth sensor 33 is at 6 top of floating plate, and the setting of infrared sensor 34 is in 8 top of headlamp, the light The setting of sensor 35 is spent in 9 bottom of camera, and the control device 38 includes solenoid valve 1, solenoid valve 2 42, solenoid valve three 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 4 49, the electricity Magnet valve 3 43 is arranged on submarine engine 28, and the solenoid valve 4 44 is arranged on left aircraft engine 5, the solenoid valve five 45 are arranged on right aircraft engine 4, and the power supply valve 1 is arranged on motor 1, and the setting of power supply valve 2 47 exists On motor 2 13, the power supply valve 3 48 is arranged on motor 3 25, and the power supply valve 4 49 is arranged 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 model 80C51 of the single motor 37.
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:When using the underwater unmanned plane and midget submarine mixing arrangement, battery 21 is the present apparatus first Electric energy needed for providing, when mixing arrangement ontology works under water, solenoid valve 3 43 is opened, and submarine engine 28 works, and is driven Rotation axis 29 is rotated, and rotation axis 29 is moved power blade 30 and rotated, the rotation of power blade 30 be fuselage 1 provide to Preceding power, water depth sensor 33 can monitor the depth of mixing arrangement ontology, then be transferred to behaviour by data transmission device 39 Make terminal 40, when mixing arrangement ontology needs to rise, operated by operating terminal 40, power supply valve 2 47 is opened, electronic Machine 2 13 is started to work, and motor 2 13 drives output shaft 2 14 to rotate, and output shaft 2 14 drives propeller 2 15 to start turning, Propeller 2 15 provides upward power for 1 head of fuselage, is moved up, while the opening of valve 3 48 of powering, motor three 25 start to work, and motor 3 25 drives output shaft 3 26 to start turning, and output shaft 3 26 drives propeller 3 27 to start turning, Propeller 3 27 provides upward power for 1 tail portion of fuselage, increase fuselage 1, when depth transducer 33 monitors that fuselage 1 reaches When designated depth, the revolving speed of motor 2 13 and motor 3 25 is controlled by operating terminal 40, reaches fuselage 1 in the depth Balance, when depth transducer 33 monitors that fuselage 1 needs to decline, power supply valve 1 is opened, and motor 1 is started to work, electricity Motivation 1 drives output shaft 1 to start turning, and output shaft 1 drives propeller 1 to start turning, and propeller 1 is 1 head of fuselage provides power, moves down fuselage 1, and when depth transducer 33 monitors that depth is suitable, power supply valve 1 is closed It closes, motor 1 stops working, and when luminosity sensor 35 monitors that light is poor, power supply valve 4 49 is opened, and headlamp 8 is bright It rises, provides illumination for the camera 9 of 8 bottom of headlamp, the picture of camera 9 is transferred to operation eventually by data transmission device 39 On end 40, operator is facilitated to operate, when needing to collect information, water pump 18 is started to work, the electromagnetism on drinking-water pipe 20 Valve 1 is opened, and water pump 18 is drawn water by 20 pairs of external worlds of drinking-water pipe, and water enters lifting by the water inlet pipe 19 on water pump 18 In chamber 16, the elevating lever 17 squeezed in lifting chamber 16 rises, and the collection head 31 on elevating lever 17 rises, and it is external then to collect head 31 Boundary carries out the collection and storage of information, and after information is collected, water pump 18 is drawn water by 19 pairs of lifting chambers 16 of water inlet pipe, It is drained by drinking-water pipe 20, elevating lever 17 drives collection head 31 to return to original place, and solenoid valve 1 is closed, hydraulic pressure sensor 32 The pressure that fuselage 1 can effectively be monitored, prevent from declining because of fuselage 1 it is too deep lead to the case where being damaged by pressure by hydraulic pressure, work as infrared ray When sensor 34 monitors that there is barrier in front, solenoid valve 3 43 is closed, and submarine engine 28 stops working, before fuselage 1 stops Into the revolving speed by changing motor 2 13 and motor 3 25 is adjusted the direction of fuselage operation, when mixing arrangement ontology It needs when being worked on the water surface, so that fuselage 1 is emerged by motor 2 13 and motor 3 25, work as water depth sensor 33 when monitoring that fuselage 1 reaches the water surface, and air pump 22 is started to work, and the solenoid valve 2 42 on exhaust tube 24 is opened, and air pump 22 passes through 24 pairs of external worlds of exhaust tube are evacuated, and are then inflated by air inlet pipe 23 to the air bag on floating plate 6, when inflation finishes Afterwards, solenoid valve 2 42 is closed, and 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, is supplied Electric valve 2 47 and power supply valve 3 48 are closed, and motor 2 13 and motor 3 25 stop working, propeller 2 15 and propeller three 27 stop operating, and solenoid valve 3 43 is closed, and submarine engine 28 stops working, and power blade 30 stops operating, solenoid valve 4 44 It is opened with solenoid valve 5 45, left aircraft engine 5 and right aircraft engine 4 are started to work, and are provided power for fuselage 1, are made fuselage 1 It moves on, when needing to turn, left aircraft engine 5 and right aircraft engine 4 is controlled by operating terminal 40 respectively Revolving speed, to achieve the effect that steering, port wing 3 and starboard wing 2 can effectively reduce fuselage 1 itself when fuselage 1 moves Gravity, makes to move more convenient, and rationally, good working effect is easy to operate, practical for links of the present invention design.
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 (8)

1. a kind of underwater unmanned plane and midget submarine mixing arrangement, which is characterized in that including fuselage(1)And single-chip microcontroller(37), institute State fuselage(1)Side is provided with starboard wing(2), the starboard wing(2)Bottom is provided with right aircraft engine(4), the fuselage (1)The other side is provided with port wing(3), the port wing(3)Bottom is provided with left aircraft engine(5), the fuselage(1)Two Side is provided with floating plate(6), the floating plate(6)On be provided with air bag, the fuselage(1)Top is provided with ventilation head(7), institute State fuselage(1)On be provided with headlamp(8), the headlamp(8)Bottom is provided with camera(9), the fuselage(1)Interior setting There is 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 motor two(13)Side is provided with Battery(21), the battery(21)Top is provided with 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, the battery(21) Side is provided with air pump(22), the air pump(22)Side is provided with air inlet pipe(23), the air bag passes through air inlet pipe(23)With Air pump(22)Connection, the air pump(22)The other side is provided with exhaust tube(24), the ventilation head(7)Pass through exhaust tube(24)With Air pump(22)Connection, the exhaust tube(24)On be provided with solenoid valve two(42), the air pump(22)Side is provided with 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), the 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), 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 depth of water Sensor(33)It is arranged in floating plate(6)Top, the infrared sensor(34)It is arranged in headlamp(8)Top, the light Spend sensor(35)It is arranged in camera(9)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 solenoid valve three(43)It is arranged in submarine engine(28)On, the solenoid valve four(44) It is arranged in left aircraft engine(5)On, the solenoid valve five(45)It is arranged in right aircraft engine(4)On, the power supply valve one (46)It is arranged in motor one(10)On, the power supply valve two(47)It is arranged in motor two(13)On, the power supply valve three (48)It is arranged in motor three(25)On, the power supply valve four(49)It is arranged in headlamp(8)On, the data transmission device (39)Including operating terminal(40).
2. a kind of underwater unmanned plane according to claim 1 and midget submarine mixing arrangement, it is characterised in that:The electric power storage Pond(21)On be provided with active carbon layer.
3. a kind of underwater unmanned plane according to claim 1 and midget submarine mixing arrangement, it is characterised in that:The output Axis one(11), output shaft two(14), output shaft three(26)And rotation axis(29)On be arranged with collision mat.
4. a kind of underwater unmanned plane according to claim 1 and midget submarine mixing arrangement, it is characterised in that:The illumination Lamp(8)On be provided with transparent panel.
5. a kind of underwater unmanned plane according to claim 1 and midget submarine mixing arrangement, it is characterised in that:The lifting Bar(17)On be arranged with rubber ring.
6. a kind of underwater unmanned plane according to claim 1 and midget submarine mixing arrangement, it is characterised in that:It is described left winged Machine engine(5), right aircraft engine(4), floating plate(6)Quantity with air bag is 2.
7. a kind of underwater unmanned plane according to claim 1 and midget submarine mixing arrangement, it is characterised in that:Single electricity Machine(37)Model 80C51.
8. a kind of underwater unmanned plane according to claim 1 and midget submarine mixing arrangement, it is characterised in that:The electric power storage Pond(21)Pass through electric wire and motor one(10), motor two(13), motor three(35), water pump(18), air pump(22)And photograph Bright lamp(8)Connection.
CN201810940665.9A 2018-08-17 2018-08-17 A kind of underwater unmanned plane and midget submarine mixing arrangement Withdrawn CN108860529A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201810940665.9A CN108860529A (en) 2018-08-17 2018-08-17 A kind of underwater unmanned plane and midget submarine mixing arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201810940665.9A CN108860529A (en) 2018-08-17 2018-08-17 A kind of underwater unmanned plane and midget submarine mixing arrangement

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CN108860529A true CN108860529A (en) 2018-11-23

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CN201810940665.9A Withdrawn CN108860529A (en) 2018-08-17 2018-08-17 A kind of underwater unmanned plane and midget submarine mixing arrangement

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Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020257879A1 (en) * 2019-06-26 2020-12-30 Ron Allum Deepsea Services Pty Ltd Underwater glider
CN112572707A (en) * 2020-12-29 2021-03-30 广东海洋大学 Intelligent inspection system for offshore wind power

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2020257879A1 (en) * 2019-06-26 2020-12-30 Ron Allum Deepsea Services Pty Ltd Underwater glider
CN112572707A (en) * 2020-12-29 2021-03-30 广东海洋大学 Intelligent inspection system for offshore wind power

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