CN106627010A - Water-air amphibious unmanned aerial vehicle - Google Patents
Water-air amphibious unmanned aerial vehicle Download PDFInfo
- Publication number
- CN106627010A CN106627010A CN201611011596.0A CN201611011596A CN106627010A CN 106627010 A CN106627010 A CN 106627010A CN 201611011596 A CN201611011596 A CN 201611011596A CN 106627010 A CN106627010 A CN 106627010A
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- CN
- China
- Prior art keywords
- unmanned plane
- water
- amphibious unmanned
- detachable
- fuselage
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- 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.)
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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
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/25—Fixed-wing aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
Abstract
The invention discloses a water-air amphibious unmanned aerial vehicle. The water-air amphibious unmanned aerial vehicle comprises an unmanned aerial vehicle body, a detachable landing gear, an aerial video device, a main controller, a wireless communication module, a navigation module, a flight control system and power systems. The unmanned aerial vehicle body is composed of a fuselage, detachable wings and an empennage. Each power system comprises a lithium battery, a motor, a detachable propeller and jet pump thrusters. The flight control system comprises a lifting steering engine, a direction steering engine and a navigation sensor. The detachable landing gear is a buffering undercarriage or a float. The aerial video device comprises a high-definition camera and a data storage module. According to the water-air amphibious unmanned aerial vehicle, the two power systems, the detachable wings, the propeller and the float are adopted, rapid switching of an aerial cruising mode and an underwater cruising mode can be achieved, and a user can select a power assembly to conduct assembling according to a cruising task. The water-air amphibious unmanned aerial vehicle has the characteristics of being portable, capable of being disassembled and assembled quickly, abundant in function, stable and reliable in performance, capable of achieving quick switch of water and air dual-purpose modes and the like, and wide in application.
Description
Technical field
The invention belongs to unmanned air vehicle technique field, in particular to a kind of empty amphibious unmanned plane of water.
Background technology
With the fast development of modern science and technology, unmanned plane is also more and more extensive in the application of all trades and professions.For example in future
Environmental protection work aspect, in the urgent need to a kind of effectively inspection, supervising device and means.Especially as water it is empty it is amphibious nobody
Machine is this can to fly in the air, and needs can be complied with again to carry out patrolling and examining the unmanned machine of navigation in the water surface timely and conveniently, and it can
With make full use of its speed fast, detection broad covered area, it is ageing it is strong, the advantage such as be swift in response, be easy to carry, and realizes the water surface or sky
In inspection and monitoring, the function that cannot realize and efficiently of manually patrolling can be made up, improve inspection and the efficiency for monitoring, set up
The three-dimensional monitoring system of patrolling in effective land, sea and air.
But, at present both at home and abroad the development of the empty amphibious unmanned plane of water is still more slow compared to traditional unmanned plane, existing
The empty amphibious unmanned plane of water is substantially integration and makes, cost intensive, complex operation, it is impossible to farthest meet each of user
Plant flight and functional requirement, it is impossible to adapt to water surface mode landing, also there is no the flight performance under certain IFR conditions.
Therefore the empty amphibious unmanned plane of a kind of mobility strong, low cost, modularization, easy to assembly, feature richness, water simple to operate is designed
It is of great immediate significance and long-range market prospects.
The content of the invention
In order to make up the empty amphibious unmanned plane of existing water deficiency in technology and functionally, the present invention is intended to provide a kind of new
The empty amphibious unmanned plane of water, the unmanned plane have low cost, modularization, be easy to assemble, feature richness and it is simple to operate the features such as.
To realize above-mentioned technical purpose, above-mentioned technique effect is reached, the present invention is achieved through the following technical solutions：
A kind of empty amphibious unmanned plane of water, including unmanned plane body, be provided with the unmanned plane body detachable take-off and landing device and
Take photo by plane video equipment, be provided with the unmanned plane body master controller, wireless communication module, navigation module, flight control system and
Dynamical system.
The unmanned plane body is made up of fuselage, detachable wing and empennage；The dynamical system includes lithium battery, electricity
Machine, dismountable screw and spray pump propeller；The flight control system includes lifting steering wheel, direction steering wheel and navigation sensor；
The detachable take-off and landing device includes buffering undercarriage or floating drum；The video equipment of taking photo by plane is deposited including high-definition camera and data
Storage module.
The detachable screw is arranged at the head of the fuselage；The both sides of the fuselage are respectively arranged with an institute
Spray pump propeller is stated, two spray pump propellers are respectively positioned on the lower rear of detachable wing described in homonymy；The navigation sensing
Device is arranged on the front end of the fuselage；The high-definition camera is arranged on the bottom of the fuselage；The bottom symmetrical of the fuselage
Be provided with the two buffering undercarriages or floating drum, two buffering undercarriages or the floating drum are respectively positioned on homonymy institute
State the underface of detachable wing.
The master controller respectively with the lithium battery, the wireless communication module, the navigation module, the motor,
The navigation sensor, the lifting steering wheel, the direction steering wheel and high-definition camera connection.
The lithium battery is that all systems and equipment on the empty amphibious unmanned plane of the water are powered, and is patrolled for the unmanned plane
The requirement of ETS estimated time of sailing, the lithium battery has that energy density is big, resistance to current values are higher, lightweight, it is safe the features such as.
The wireless communication module be mainly used in receive ground control terminal instruction and schedule information, and by it is described nobody
The data Real-time Feedback collected during machine cruise is to the ground control terminal.
The master controller can by the wireless communication module receive from the ground control terminal instruction, and
According to the switch of the instruction control motor, an electricity for adjusting its rotating speed is connected with the motor and is adjusted；The motor
Then the screw is respectively by transmission device and the spray pump propeller provides power.
The master controller can by the wireless communication module receive from the ground control terminal instruction, and
According to the operating of the instruction control lifting steering wheel and the direction steering wheel；The lifting steering wheel connects with the detachable wing
Connect, be mainly used in adjusting flight attitude according to site environment situation during taking off with landing, it is ensured that unmanned plane landing
The safety of journey；The direction steering wheel is connected with the empennage, be mainly used in unmanned plane in water and aerial navigation direction and
Attitude is adjusted and control.
The master controller can by the wireless communication module receive from the ground control terminal instruction, and
According to the shooting of the instruction control high-definition camera, to realize in real time to aerial and waterborne be monitored and image, video are adopted
Collection；The high-definition camera is connected with the data memory module, and captured image and video can not only be stored in the number
According to memory module, also the ground control can be sent to eventually by the wireless communication module via after the master controller
End, is eventually displayed on the display screen of the ground control terminal, realizes monitoring, storage, the real time implementation of transmission and synchronization.
The navigation sensor main will include velocity sensor, course transmitter, baroceptor and obstacle induction installation,
For carrying out the collection of flight information and parameter when the unmanned plane performs cruise task；The master controller can be collected respectively
The information that the individual navigation sensor is gathered, and these information are fed back to into the ground control by the wireless communication module
Terminal processed, the state of flight of unmanned plane described in monitor in real time, it is ensured that cruise task is smoothly completed.
The navigation module has satellite reception, positioning and the function of navigating, and the navigation module can be in real time to described
Unmanned plane location is positioned, and by coordinate information via anti-by the wireless communication module after the master controller
Feed the ground control terminal；The ground control terminal learns the unmanned plane location by coordinate information, is
The unmanned plane formulates the cruise route in aerial or water, and route information is sent to by the wireless communication module described
Unmanned plane, is the automatic cruising or the offer route guidance that makes a return voyage of the unmanned plane.
Further, warning lamp is provided with the unmanned plane body, the warning lamp is connected with the master controller, it is main
It is used to be identified the unmanned plane and warning function when task is cruised at night.
Further, the motor is brushless electric machine.
Further, the outside of the motor and the lithium battery is protected and water-proofing treatment, and arrange air inlet and
Gas outlet, when the empty amphibious unmanned plane of the water is navigated by water sealing is automatically turned on, and the motor and the lithium battery are protected.
Further, the high-definition camera adopts rotatable camera head, and does the steady stabilization of increasing and waterproofing design, works as institute
When stating unmanned plane in the air or navigating by water in water, it is ensured that the video for collecting and image frame are stable and clear.
Further, it is the requirement that meets long-time inspection work waterborne, it is the fuselage, the detachable wing, described
Empennage and the floating drum adopt waterproof material, and spray underwater paint in its surface and junction.
Further, the wireless communication module is 4G communication modules.
Further, the navigation module is GPS navigation module or Beidou navigation module.
Further, the detachable wing is upper single swept-back wing, and such design can not only allow aircraft to possess bigger
Lift and good stability, and can guarantee that the stability and definition of picture of taking photo by plane.
Patrolled and supervised with region where the unmanned plane is mainly used in arrive at people in the inspection work of field
Control.When related service personnel are outgoing performs inspection task, required component can be carried with according to inspection environmental demand, reach existing
After being assembled after, start unmanned plane cruise operation.
The course of work that the unmanned plane cruises in the air is as follows：
When the empty amphibious unmanned plane of water needs to carry out aerial cruise operation, can be by the detachable wing and the buffering undercarriage
The aerial dynamical system of the unmanned plane is opened after assembling.The aerial dynamical system is for the aerial cruise operation of the unmanned plane
Stability, persistence and security there is vital effect, the design of the aerial dynamical system must be with the nothing
Man-machine fuselage matched.The motor of the unmanned plane provides power, the unmanned plane lift-off and navigation master for the screw
The thrust for leaning on the screw rotation to produce.
The course of work that the unmanned plane cruises in water is as follows：
When the empty amphibious unmanned plane of the water needs to carry out cruise operation in water, by the detachable wing, the screw
Remove with the buffering undercarriage, be that surface navigation makes corresponding structural adjustment by the floating drum loaded under the fuselage
The surface navigation dynamical system of the unmanned plane is opened afterwards, realizes that unmanned plane is quickly cut by sail mode in aerial mode to water
Change.The floating drum can ensure that the unmanned plane is kept afloat, and the motor of the unmanned plane is provided for the spray pump propeller
Power, the spray pump propeller sprays backward generation thrust, so as to navigate by water offer motive power on the water for unmanned plane, while institute
Unmanned plane is stated by being arranged on the various described navigation sensor real-time collecting flying quality and surrounding environment of the front fuselage
Situation so that the unmanned plane can be dodged in advance when obstacle is run into, realizes that the empty amphibious unmanned plane of the water is complete in the water surface
Into cruise operation.
Compared with prior art, the invention has the beneficial effects as follows：
1st, the empty amphibious unmanned plane of water of the invention has easy to carry, quick release assembling, feature richness, stable performance can
By, be capable of achieving the empty dual-purpose pattern of water and be switched fast the features such as, strong adaptability is of many uses.
2nd, the empty amphibious unmanned plane of water of the invention adopts the high-definition camera of rotatable stabilization, the behaviour of ground control terminal
The image that work person can pass back according to camera, realizes certain over the horizon flight.
3rd, the empty amphibious unmanned plane of water of the invention carries navigation module, and cruise track and route can be recorded and to returning
Air route line planned, improves the security of unmanned plane recovery.
4th, using upper single swept-back wing design, wing can as the case may be certainly for the wing of the empty amphibious unmanned plane of water of the invention
To keep level, such design can not only allow aircraft to possess bigger lift and good stability to dynamic angle correction, and
And can guarantee that the stability and definition of picture of taking photo by plane.
5th, the empty amphibious unmanned plane of water of the invention employs two sets of dynamical systems and dismountable wing, screw and floats
Cylinder, is capable of achieving being switched fast for cruise mode in aerial cruise mode and water, and user can voluntarily select power according to cruise task
Component is assembled.
6th, the device such as the fuselage of the empty amphibious unmanned plane of water of the invention, detachable wing, empennage and floating drum adopts waterproof
Material, and underwater paint is sprayed in its surface and junction, to meet the requirement of work of realizing being patrolled for a long time in water.
Described above is only the general introduction of technical solution of the present invention, in order to better understand the technological means of the present invention,
And can be practiced according to the content of specification, below with presently preferred embodiments of the present invention and coordinate accompanying drawing describe in detail as after.
The specific embodiment of the present invention is shown in detail in by following examples and its accompanying drawing.
Description of the drawings
Accompanying drawing described herein is used for providing a further understanding of the present invention, constitutes the part of the application, this
Bright schematic description and description does not constitute inappropriate limitation of the present invention for explaining the present invention.In the accompanying drawings：
Fig. 1 is unmanned plane of the present invention in the external structure top view in water during cruise mode；
Fig. 2 be unmanned plane of the present invention be in aerial cruise mode when external structure side view；
Fig. 3 is the equipment electric diagram of unmanned plane of the present invention.
Label declaration in figure：1st, master controller；2nd, wireless communication module；3rd, navigation module；4th, fuselage；5th, it is removable to unload the goods from the airplane
The wing；6th, empennage；7th, lithium battery；8th, motor；9th, screw；10th, pump propeller is sprayed；11st, steering wheel is lifted；12nd, direction steering wheel；13、
Navigation sensor；14th, ground control terminal；15th, undercarriage is buffered；16th, floating drum；17th, high-definition camera；18th, data storage mould
Block；19th, electricity is adjusted；20th, warning lamp.
Specific embodiment
Below with reference to the accompanying drawings and in conjunction with the embodiments describing the present invention in detail.
Referring to shown in Fig. 1-3, a kind of empty amphibious unmanned plane of water, including unmanned plane body, arrange on the unmanned plane body
Have detachable take-off and landing device and take photo by plane video equipment, be provided with the unmanned plane body master controller 1, wireless communication module 2,
Navigation module 3, flight control system and dynamical system.
The unmanned plane body is made up of fuselage 4, detachable wing 5 and empennage 6；The dynamical system include lithium battery 7,
Motor 8, dismountable screw 9 and spray pump propeller 10；The flight control system includes lifting steering wheel 11, direction steering wheel 12 and boat
Line sensor 13；The detachable take-off and landing device includes buffering undercarriage 15 or floating drum 16；The video equipment of taking photo by plane includes height
Clear camera 17 and data memory module 18.
The screw 9 is arranged at the head of the fuselage 4；The both sides of the fuselage 4 are respectively arranged with described in one
Spray pump propeller 10, two spray pump propellers 10 are respectively positioned on the lower rear of detachable wing 5 described in homonymy；The navigation is passed
Sensor 13 is arranged on the front end of the fuselage 4；The high-definition camera 17 is arranged on the bottom of the fuselage 4；The fuselage 4
It is provided with two buffering undercarriages 15 or the floating drum 16, two buffering undercarriages 15 or described floating bottom symmetrical
Cylinder 16 is respectively positioned on the underface of detachable wing 5 described in homonymy.
The master controller 1 respectively with the lithium battery 7, the wireless communication module 2, the navigation module 3, the electricity
Machine 8, the navigation sensor 13, the lifting steering wheel 11, the direction steering wheel 12 and the high-definition camera 17 connect.
The lithium battery 7 is that all systems and equipment on the empty amphibious unmanned plane of the water are powered, for the unmanned plane
The requirement of cruise time, the lithium battery 7 has the spies such as energy density is big, resistance to current values are higher, lightweight, security is high
Point.
The wireless communication module 2 is mainly used in receiving instruction and the schedule information of ground control terminal 14, and will be described
The data Real-time Feedback collected during unmanned plane cruise is to the ground control terminal.
The master controller 1 can receive the finger from the ground control terminal 14 by the wireless communication module 2
Order, and according to the switch of the instruction control motor 8, an electricity for adjusting its rotating speed is connected with the motor 8 and adjusts 19；
The motor 8 is then respectively the screw 9 by transmission device and the spray pump propeller 10 provides power.
The master controller 1 can receive the finger from the ground control terminal 14 by the wireless communication module 2
Order, and according to the operating of the instruction control lifting steering wheel 11 and the direction steering wheel 12；It is described lifting steering wheel 11 with it is described can
Dismounting wing 5 connects, and is mainly used in adjusting flight attitude according to site environment situation during taking off with landing, it is ensured that nothing
The safety of man-machine landing process；The direction steering wheel 12 is connected with the empennage 6, is mainly used in water and aerial to unmanned plane
Navigation direction and attitude be adjusted and control.
The master controller 1 can receive the finger from the ground control terminal 14 by the wireless communication module 2
Order, and according to the shooting of the instruction control high-definition camera 17, with realize in real time to be monitored in aerial and water and image,
Video acquisition；The high-definition camera 17 is connected with the data memory module 18, and captured picture can not only be stored in institute
In stating data memory module 18, also the ground can be sent to by the wireless communication module 2 via after the master controller 1
Control terminal 14, is eventually displayed on the display screen of the ground control terminal 14, realizes monitoring, storage, the real time implementation of transmission
And synchronization.
The navigation sensor 13 mainly should be filled including velocity sensor, course transmitter, baroceptor and obstacle sense
Put, for carrying out the collection of flight information and parameter when the unmanned plane performs cruise task；The master controller 1 can be received
Collect the information that each described navigation sensor 13 is gathered, and these information are fed back to into institute by the wireless communication module 2
Ground control terminal 14 is stated, the state of flight of unmanned plane described in monitor in real time, it is ensured that cruise task is smoothly completed.
The navigation module 3 has satellite reception, positioning and the function of navigating, and the navigation module 3 can in real time to institute
State unmanned plane location to be positioned, and by coordinate information via after the master controller 1 by the radio communication mold
Block 2 feeds back to the ground control terminal 14；The ground control terminal 14 is learned residing for the unmanned plane by coordinate information
Position, be cruise route that the unmanned plane is formulated in aerial or water, and route information is passed through into the wireless communication module 2
The unmanned plane is sent to, is the automatic cruising or the offer route guidance that makes a return voyage of the unmanned plane.
Further, warning lamp 20 is provided with the unmanned plane body, the warning lamp 20 connects with the master controller 1
Connect, be mainly used in being identified the unmanned plane and warning function when task is cruised at night.
Further, the motor 8 is brushless electric machine.
Further, the outside of the motor 8 and the lithium battery 7 is protected and water-proofing treatment, and arranges air inlet
And gas outlet, sealing is automatically turned on when the empty amphibious unmanned plane of the water is navigated by water, the motor 8 and the lithium battery 7 are carried out
Protection.
Further, the high-definition camera 17 adopts rotatable camera head, and does the steady stabilization of increasing and waterproofing design, when
When the unmanned plane is navigated by water in the air or in water, it is ensured that the video for collecting and image frame are stable and clear.
Further, it is the requirement that meets work of patrolling for a long time in water, the fuselage 4, the detachable wing 5, institute
The device such as empennage 6 and the floating drum 16 is stated using waterproof material, and underwater paint is sprayed in its surface and junction.
Further, the wireless communication module 2 is 4G communication modules.
Further, the navigation module 3 is GPS navigation module or Beidou navigation module.
Further, the detachable wing 5 is upper single swept-back wing, and such design can not only allow aircraft to possess bigger
Lift and good stability, and can guarantee that the stability and definition of picture of taking photo by plane.
Patrolled and supervised with region where the unmanned plane is mainly used in arrive at people in the inspection work of field
Control.When related service personnel are outgoing performs inspection task, required component can be carried with according to inspection environmental demand, reach existing
After being assembled after, start unmanned plane cruise operation.
The course of work that the unmanned plane cruises in the air is as follows：
When the empty amphibious unmanned plane of water needs to carry out aerial cruise operation, the detachable wing 5 and the buffering can be risen and fallen
Frame 15 opens the aerial dynamical system of the unmanned plane after assembling.The aerial dynamical system is cruised in the air for the unmanned plane
The stability of work, persistence and security have vital effect, and the design of the aerial dynamical system must be with institute
State unmanned aerial vehicle body matched.The motor 8 of the unmanned plane is that the screw 9 provides power, unmanned plane lift-off and
Navigate by water and the thrust for producing is rotated mainly by the screw 9.
The course of work that the unmanned plane cruises in water is as follows：
When the empty amphibious unmanned plane of the water needs to carry out cruise operation in water, by the detachable wing 5, the screw
9 and the buffering undercarriage 15 remove, by the floating drum 16 loaded under the fuselage 4, being that surface navigation makes corresponding knot
The surface navigation dynamical system of the unmanned plane is opened after structure adjustment, realizes unmanned plane by sail mode in aerial mode to water
It is switched fast.The floating drum 16 can ensure that the unmanned plane is kept afloat, and the motor 8 of the unmanned plane is pushed away for the spray pump
Enter device 10 and power is provided, the spray pump propeller 10 sprays backward generation thrust, dynamic so as to navigate by water offer on the water for unmanned plane
Power is supported, while the unmanned plane is flown by being arranged on various described navigation sensor 13 real-time collecting of the front fuselage
Data and ambient environmental conditions so that the unmanned plane can be dodged in advance when obstacle is run into, realize that the water sky is amphibious
Unmanned plane completes cruise operation in the water surface.
The preferred embodiments of the present invention are the foregoing is only, the present invention is not limited to, for those skilled in the art
For member, the present invention can have various modifications and variations.All any modifications within the spirit and principles in the present invention, made,
Equivalent, improvement etc., should be included within the scope of the present invention.
Claims (10)
1. the empty amphibious unmanned plane of a kind of water, it is characterised in that：Including unmanned plane body, it is provided with the unmanned plane body removable
Unload take-off and landing device and video equipment of taking photo by plane, in the unmanned plane body master controller is provided with（1）, wireless communication module（2）, lead
Model plane block（3）, flight control system and dynamical system；
The unmanned plane body is by fuselage（4）, detachable wing（5）And empennage（6）Composition；The dynamical system includes lithium battery
（7）, motor（8）, dismountable screw（9）With spray pump propeller（10）；The flight control system includes lifting steering wheel（11）, side
To steering wheel（12）With navigation sensor（13）；The detachable take-off and landing device is buffering undercarriage（15）Or floating drum（16）；It is described
Video equipment of taking photo by plane includes high-definition camera（17）And data memory module（18）；
The screw（9）It is arranged on the fuselage（4）Head at；The fuselage（4）Both sides be respectively arranged with an institute
State spray pump propeller（10）, two spray pump propellers（10）It is respectively positioned on detachable wing described in homonymy（5）Lower rear；Institute
State navigation sensor（13）It is arranged on the fuselage（4）Front end；The high-definition camera（17）It is arranged on the fuselage（4）'s
Bottom；The fuselage（4）Bottom symmetrical be provided with two buffering undercarriages（15）Or the floating drum（16）, two institutes
State buffering undercarriage（15）Or the floating drum（16）It is respectively positioned on detachable wing described in homonymy（5）Underface；
The master controller（1）Respectively with the lithium battery（7）, the wireless communication module（2）, the navigation module（3）, institute
State motor（8）, the navigation sensor（13）, the lifting steering wheel（11）, the direction steering wheel（12）With the high-definition camera
Head（17）Connection；The lithium battery（7）Power for all systems and equipment on the empty amphibious unmanned plane of the water；The main control
Device（1）By the wireless communication module（2）With ground control terminal（14）Carry out information exchange；The motor（8）By passing
Dynamic device respectively with the screw（9）With the spray pump propeller（10）Connection, the motor（8）One is connected with for controlling
The electricity tune of its rotating speed（19）；The lifting steering wheel（11）With the detachable wing（5）Connection；The direction steering wheel（12）With institute
State empennage（6）Connection；The high-definition camera（17）With the data memory module（18）Connection.
2. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：The motor（8）For brushless electric machine.
3. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：The motor（8）, the lithium battery（7）
With the high-definition camera（17）Outside protect and water-proofing treatment.
4. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：The navigation sensor（13）Including speed
Sensor, course transmitter, baroceptor and obstacle induction installation.
5. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：Warning is provided with the unmanned plane body
Lamp（20）, the warning lamp（20）With the master controller（1）Connection.
6. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：The high-definition camera（17）Using can revolve
Rotatable camera, and do the steady stabilization design of increasing.
7. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：The fuselage（4）, the detachable wing
（5）, the empennage（6）With the floating drum（16）Waterproof material is adopted, and in its surface spraying underwater paint.
8. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：The wireless communication module（2）It is logical for 4G
Letter module.
9. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：The navigation module（3）For GPS navigation mould
Block or Beidou navigation module.
10. the empty amphibious unmanned plane of water according to claim 1, it is characterised in that：The detachable wing（5）After upper list
Plunder the wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611011596.0A CN106627010A (en) | 2016-11-17 | 2016-11-17 | Water-air amphibious unmanned aerial vehicle |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611011596.0A CN106627010A (en) | 2016-11-17 | 2016-11-17 | Water-air amphibious unmanned aerial vehicle |
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| CN106627010A true CN106627010A (en) | 2017-05-10 |
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ID=58809063
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| Application Number | Title | Priority Date | Filing Date |
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| CN201611011596.0A Pending CN106627010A (en) | 2016-11-17 | 2016-11-17 | Water-air amphibious unmanned aerial vehicle |
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| CN107323656A (en) * | 2017-08-23 | 2017-11-07 | 吉林省彬生蓝航天际无人机科技有限公司 | A kind of high definition is taken photo by plane unmanned plane undercarriage protector and the localization method that rises and falls |
| CN108762298A (en) * | 2018-05-30 | 2018-11-06 | 佛山市神风航空科技有限公司 | A kind of aquatic unmanned aerial vehicle landing self-control system |
| CN109624628A (en) * | 2018-12-20 | 2019-04-16 | 吉林大学 | A kind of across the medium Power System of Flight Vehicle of scalable integral type of propeller |
| CN109665074A (en) * | 2019-01-25 | 2019-04-23 | 深圳市合泰英龙科技有限公司 | A kind of laser guidance water surface rescue aid and its rescue mode |
| CN109738453A (en) * | 2019-02-25 | 2019-05-10 | 黄鹏 | Unmanned plane monitor video image processing apparatus and image processing method |
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| CN110217064B (en) * | 2019-05-07 | 2022-08-30 | 上海海事大学 | Amphibious submersible vehicle |
| CN110217064A (en) * | 2019-05-07 | 2019-09-10 | 上海海事大学 | A kind of water sky land three is dwelt submariner device |
| CN110667842A (en) * | 2019-10-10 | 2020-01-10 | 佛山职业技术学院 | Unmanned inspection equipment and unmanned inspection machine group system |
| CN111532430A (en) * | 2020-05-26 | 2020-08-14 | 广州扬坪机电科技有限公司 | Unmanned aerial vehicle capable of triphibious operation between water, land and air |
| CN112072739A (en) * | 2020-09-02 | 2020-12-11 | 厦门市汉飞鹰航空科技有限公司 | Unmanned aerial vehicle distributing type power supply system |
| CN112550699A (en) * | 2020-12-24 | 2021-03-26 | 重庆工程职业技术学院 | Unmanned aerial vehicle on water with balanced actuating system of surface of water traveling |
| CN113664845A (en) * | 2021-08-19 | 2021-11-19 | 重庆七腾科技有限公司 | Water surface inspection robot and inspection method |
| CN114160214A (en) * | 2021-11-10 | 2022-03-11 | 中国空气动力研究与发展中心空天技术研究所 | Unmanned aerial vehicle extreme environment simulation laboratory |
| CN114160214B (en) * | 2021-11-10 | 2023-10-27 | 中国空气动力研究与发展中心空天技术研究所 | Unmanned aerial vehicle extreme environment simulation laboratory |
| CN115303483A (en) * | 2022-08-31 | 2022-11-08 | 南京航空航天大学 | Amphibious rotor unmanned aerial vehicle with blade reuse function and control method thereof |
| CN116980051A (en) * | 2023-08-04 | 2023-10-31 | 广东工业大学 | Communication system of water-air dual-purpose unmanned aerial vehicle and operation method thereof |
| CN116980051B (en) * | 2023-08-04 | 2024-01-26 | 广东工业大学 | Communication system of water-air dual-purpose unmanned aerial vehicle and operation method thereof |
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