CN108248858A - A kind of amphibious unmanned plane - Google Patents
A kind of amphibious unmanned plane Download PDFInfo
- Publication number
- CN108248858A CN108248858A CN201711425523.0A CN201711425523A CN108248858A CN 108248858 A CN108248858 A CN 108248858A CN 201711425523 A CN201711425523 A CN 201711425523A CN 108248858 A CN108248858 A CN 108248858A
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- CN
- China
- Prior art keywords
- unmanned plane
- aircraft
- wing
- fuselage
- steering engine
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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
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/001—Flying-boats; Seaplanes with means for increasing stability on the water
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C35/00—Flying-boats; Seaplanes
- B64C35/005—Flying-boats; Seaplanes with propellers, rudders or brakes acting in the water
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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
-
- 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
- B64U2101/30—UAVs specially adapted for particular uses or applications for imaging, photography or videography
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2201/00—UAVs characterised by their flight controls
- B64U2201/20—Remote controls
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
The present invention provides a kind of amphibious unmanned plane, is made of flight control system, aircraft body, power plant, take-off and landing device and five major part of equipment of taking photo by plane.Unmanned controller is fixed together with display screen with stent, according to the image of passback, can accomplish certain over the horizon flight.Power plant has been truly realized pollution-free, the environmental requirement of zero-emission using green, the lithium ion polymer battery of environmental protection.This unmanned plane wing is designed using high mounted wing, and the upper counterangle with certain angle, and wing can be corrected to keep horizontal automatically.Aircraft is not only allowed to have the lift of bigger and good stability, and the picture taken photo by plane is allowed more to stablize.This wing is fixed on nut on fuselage simultaneously, and wing quick release is convenient for carrying, character module higher.Different take-off and landing devices can be selected according to the difference of flight environment of vehicle, have floating drum and the undercarriage two ways available.This unmanned plane is at low cost, the degree of modularity is high, feature-rich novel, easy to operate.
Description
Technical field
The invention belongs to aviation aircraft field, more particularly, to a kind of amphibious unmanned plane taken photo by plane.
Background technology
The remote control fixed-wing unmanned plane used both at home and abroad at present is by undercarriage takeoff mostly or directly hand is thrown
It takes off, this mode of taking off is more limited by the field, it is necessary to which unobscured, the land of Land leveling is taken off.And state
It is slower that inside and outside aquatic unmanned aerial vehicle compares land fixed-wing Development of UAV, and existing aquatic unmanned aerial vehicle, substantially one
Bodyization manufactures, expensive, complicated for operation；And the work circumstances safe degree of unmanned plane is relatively low, is influenced greatly by external factor, therefore
When aircraft damages, maintenance difficulty is big, and maintenance cost is high.And current seaplane function is single, can not fit well
Using the flight demand at family.Therefore designing a kind of low cost, modularization, aquatic unmanned aerial vehicle feature-rich, easy to operate has
Great meaning and good market prospects.
Invention content
The purpose of the present invention is to provide a kind of amphibious unmanned plane, the unmanned plane low cost, modularization, function are rich
It is rich, easy to operate.
The present invention is achieved through the following technical solutions：A kind of amphibious unmanned plane, mainly by flight control system
System, aircraft body, power plant, take-off and landing device and the most of composition of equipment five of taking photo by plane；Aircraft control system mainly includes remote control
Device, remote control receiver, aileron steering engine, rudder steering engine, elevator steering engine and navigation lights；Aircraft body is mainly by fuselage, machine
The wing, empennage (including horizontal tail and vertical fin) are formed；Power plant mainly includes：Propeller, brushless motor, motor fixed base, electricity
Sub- governor, lithium ion polymer battery；Take-off and landing device is mainly made of floating drum and undercarriage two parts；Equipment of taking photo by plane mainly is wrapped
It includes：Small-sized image pickup head, two axle The Cloud Terraces, lithium ion polymer battery, osd data laminating module, data transmitter, GPS, data connect
Receipts machine, display/panel bracket and display screen；It is characterized in that：Display screen is fixed on a remote control with display/panel bracket, data receiver
Machine and data receiver power supply are fixed on a display screen；Propeller at head is connected with the rotation axis of motor with nut, electricity
Machine is fixed in motor fixed base and is connect with conducting wire with electron speed regulator, electron speed regulator postposition lithium ion polymer battery,
The signal wire of electron speed regulator is connected on the remote control receiver of waist, and waist is equipped with osd data and folds
Add module and data transmitter, the two is connected with signal wire；Fuselage bottom is equipped with two axle The Cloud Terraces, is secured in two axle The Cloud Terraces
Small-sized image pickup head, AV output lines are connected with osd data laminating module, and GPS is equipped at the top of central fuselage；In wing two
The green navigation lights in the left red right side of end installation, fuselage connection vertical fin, vertical fin are followed by horizontal tail.
The board joints of fuselage bottom of the present invention use water-repellent paint.
During flight on the water of the present invention, aircraft installs floating drum, mounting bracket that there are two the installations of aircraft bottom, and floating drum is straight
It connects rack-mount, while one steering engine is installed in floating drum tail portion, to realize function that aircraft turns on the water surface.
Of the present invention in land flight, aircraft installs undercarriage, is installed using rear bikini, tail wheel is pacified with thicker wire
Mounted in afterbody, while steel wire one end is fixed together with rudder, thus can be withouyt a steering engine in the case of,
It realizes the steering of aircraft, greatly reduces the cost of manufacture of aircraft.
It is of the present invention that aileron steering engine, elevator steering engine, rudder steering engine are installed on the wing and rear body of aircraft.
It is of the present invention that in empennage installation, there are one the navigation lights of white.
It is connected at the top of forebody of the present invention with hinge with the fuselage of side, top and opposite side fuselage velcro
Connection.
Four fixing bolts are mounted in both sides fuselage in the middle part of aircraft of the present invention, fixing bolt passes through wing, machine
Wing opening both ends are reinforced with plank, and directly wing is fixed on fuselage with nut.
The available installation of floating drum and undercarriage two ways of the present invention.
It is an advantage of the invention that：The unmanned plane low cost, modularization, feature-rich, easy to operate, this unmanned plane wing is adopted
It is designed with high mounted wing, and the upper counterangle with certain angle, wing can be corrected to keep horizontal automatically.Not only aircraft is allowed to have
The lift of bigger and good stability, and the picture taken photo by plane is allowed more to stablize.This wing is fixed on machine with nut simultaneously
With, wing quick release is convenient for carrying, character module higher.It can be selected according to the difference of flight environment of vehicle different
Take-off and landing device, has floating drum and the undercarriage two ways available.This unmanned plane is at low cost, the degree of modularity is high, feature-rich
It is novel, easy to operate.
Description of the drawings
Fig. 1 is the ground installation structure diagram of unmanned plane of the present invention.
Fig. 2 is the structure top view of unmanned plane of the present invention.
Fig. 3 is the structure left view when unmanned plane of the present invention installs floating drum.
Fig. 4 is the structure left view when unmanned plane of the present invention installs undercarriage.
Fig. 5 is the structural front view of unmanned plane of the present invention.
In figure：1. 5. data receiver of remote controler 2. display/panel bracket, 3. data receiver electromechanical source, 4. display screen, 6. spiral
10. lithium ion polymer battery of paddle 7. motor, 8. motor fixed base, 9. electron speed regulator, 11. remote control receiver 12.OSD numbers
According to 16. wing of laminating module 13. data transmitter, 14. small-sized image pickup head, 15. two axle The Cloud Terraces, 17. navigation lights 18.GPS19. horizontal tails
20. 21. floating drum of vertical fin, 22. undercarriage.
Specific embodiment
The present invention is further illustrated with specific assemble method below in conjunction with the accompanying drawings.
The invention is realized in this way it includes flight control system, aircraft body, power plant, take-off and landing device and boat
It is most of to clap equipment five.Display screen 4 is fixed on display/panel bracket 2 on remote controler 1, and operator very convenient in this way is according to taking photo by plane
The picture of passback manipulates aircraft, allows aircraft with more operability, safety.Data receiver 5 is fixed on the display screen 4, is used
One piece of lithium ion polymer battery 3 is powered to data receiver 5.The rotation axis nut phase of propeller 6 and motor 7 at head
Connection, motor is fixed in motor fixed base 8 to be connect with conducting wire with electron speed regulator 9, while 10 electron speed governing of lithium battery
Device 9 is powered, and the signal wire of electron speed regulator 9 is connected on the remote control receiver 11 of waist.Waist is installed
There are osd data laminating module 12 and data transmitter 13, the two is connected with signal wire.Lithium battery 10 is superimposed simultaneously to osd data
Module 12 and electron speed regulator 9 are powered, and while manufacture cost is reduced, are greatly alleviated the weight of aircraft, are enhanced winged
The maneuverability of machine.Fuselage bottom is equipped with two axle The Cloud Terraces 15, small-sized image pickup head 14 is secured in two axle The Cloud Terraces 15, AV is defeated
Outlet is connected with osd data laminating module 12, and GPS18 is equipped at the top of central fuselage.GPS18 is mounted on can outside fuselage
Blocking of the fuselage material to signal effectively is avoided, improves the signal strength of GPS.Simultaneously on the left red right side of 16 both ends of wing installation
Green navigation lights 17, in the installation of vertical fin 20, there are one the navigation lights 17 of white.Installation navigation lights 17 can allow operator better
See unmanned plane during flying posture clearly, improve the safety and stability of flight.Waterproof is used in the board joints of fuselage bottom
Coating, while improving unmanned plane water resistance, due to producing waterproofing membrane, the stress for substantially increasing junction is strong
Degree, makes aircraft more safely, securely.On the water during flight, aircraft installation floating drum 21, there are two installation branch for the installation of aircraft bottom
Frame, floating drum are directly installed on stent, while install a steering engine in floating drum tail portion, to realize that aircraft turns on the water surface
Function.On land during flight, aircraft installation undercarriage 22 is installed, tail wheel is mounted on fuselage with thicker wire using rear bikini
Tail portion, while steel wire one end is fixed together with rudder, thus can be withouyt a steering engine in the case of, realize aircraft
Steering, greatly reduce the cost of manufacture of aircraft.
It is connected first at the top of forebody with hinge with the fuselage of side, top connects with opposite side fuselage velcro
It connects, such be advantageous in that can conveniently replace battery and more convenient repair power plant.Two in the middle part of aircraft
Four fixing bolts are mounted in the fuselage of side, fixing bolt passes through wing, and the opening of wing 16 both ends are reinforced, therefore available with plank
Nut is directly fixed on wing on fuselage.It allows aircraft that can easily unload lower wing, is convenient for carrying, while be damaged in wing
When, wing is only needed to change, greatly reduces maintenance cost.Wing is designed using high mounted wing simultaneous with certain upper anti-
Angle while aircraft is allowed to have the lift of bigger and good stability, indirectly also allows the picture taken photo by plane more to be stablized.On land
During flight, aircraft installation undercarriage is installed using rear bikini, and tail wheel thicker wire is mounted on afterbody, while steel wire one
End be fixed together with rudder, thus can be withouyt a steering engine in the case of, realize the steering of aircraft, greatly reduce
The cost of manufacture of aircraft.On the water during flight, aircraft installs floating drum, mounting bracket that there are two the installations of aircraft bottom, and floating drum is straight
It connects rack-mount, while one steering engine is installed in floating drum tail portion, to realize function that aircraft turns on the water surface.It is aobvious
Display screen is directly anchored on remote controler, makes the simpler convenience of operation.
Claims (7)
1. a kind of amphibious unmanned plane, mainly by flight control system, aircraft body, power plant, take-off and landing device and take photo by plane
The most of composition of equipment five；Aircraft control system mainly include remote controler, remote control receiver, aileron steering engine, rudder steering engine,
Elevator steering engine and navigation lights；Aircraft body is mainly made of fuselage, wing, empennage；Power plant mainly includes：Propeller,
Brushless motor, motor fixed base, electron speed regulator, lithium ion polymer battery；Take-off and landing device is mainly by floating drum and undercarriage
Two parts form；Equipment of taking photo by plane mainly includes：Small-sized image pickup head, two axle The Cloud Terraces, lithium ion polymer battery, osd data superposition
Module, data transmitter, GPS, data receiver, display/panel bracket and display screen；It is characterized in that：Display screen display screen branch
Frame is fixed on a remote control, and data receiver and data receiver power supply are fixed on a display screen；Propeller and electricity at head
The rotation axis of machine is connected with nut, and motor is fixed in motor fixed base and is connect with conducting wire with electron speed regulator, electronics tune
Fast device postposition lithium ion polymer battery, the signal wire of electron speed regulator are connected to the remote control receiver positioned at waist
On, waist is equipped with osd data laminating module and data transmitter, and the two is connected with signal wire；Fuselage bottom is installed
There are two axle The Cloud Terraces, small-sized image pickup head is secured in two axle The Cloud Terraces, AV output lines are connected with osd data laminating module, at middle part
GPS is installed at the top of fuselage；The green navigation lights in the left red right side of installation at wing both ends, fuselage connection vertical fin, vertical fin are followed by horizontal tail.
2. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：The plank connection of the fuselage bottom
Place uses water-repellent paint.
3. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：On the water during flight, aircraft installation
Floating drum, there are two mounting bracket, floating drum is directly installed on stent the installation of aircraft bottom, while installs a rudder in floating drum tail portion
Machine.
4. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：On land during flight, aircraft installation
Undercarriage is installed using rear bikini, and tail wheel is mounted on afterbody with thicker wire, while steel wire one end is fixed on rudder
Together.
5. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：On the wing and rear body of aircraft
Aileron steering engine, elevator steering engine, rudder steering engine are installed.
6. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：In empennage installation, there are one whites
Navigation lights.
7. a kind of amphibious unmanned plane according to claim 1, it is characterised in that：Forebody top hinge and side
Fuselage be connected, top is connect with opposite side fuselage with velcro.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711425523.0A CN108248858A (en) | 2017-12-25 | 2017-12-25 | A kind of amphibious unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201711425523.0A CN108248858A (en) | 2017-12-25 | 2017-12-25 | A kind of amphibious unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108248858A true CN108248858A (en) | 2018-07-06 |
Family
ID=62723605
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201711425523.0A Pending CN108248858A (en) | 2017-12-25 | 2017-12-25 | A kind of amphibious unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108248858A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111152923A (en) * | 2020-01-07 | 2020-05-15 | 长江水利委员会长江科学院 | Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle |
-
2017
- 2017-12-25 CN CN201711425523.0A patent/CN108248858A/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111152923A (en) * | 2020-01-07 | 2020-05-15 | 长江水利委员会长江科学院 | Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle |
| CN111152923B (en) * | 2020-01-07 | 2021-06-25 | 长江水利委员会长江科学院 | Underwater terrain measuring device based on vertical take-off and landing fixed wing amphibious unmanned aerial vehicle |
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Legal Events
| Date | Code | Title | Description |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180706 |
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| WD01 | Invention patent application deemed withdrawn after publication |