CN204726655U - A kind of amphibious unmanned plane - Google Patents
A kind of amphibious unmanned plane Download PDFInfo
- Publication number
- CN204726655U CN204726655U CN201520343052.9U CN201520343052U CN204726655U CN 204726655 U CN204726655 U CN 204726655U CN 201520343052 U CN201520343052 U CN 201520343052U CN 204726655 U CN204726655 U CN 204726655U
- Authority
- CN
- China
- Prior art keywords
- aircraft
- wing
- unmanned plane
- fuselage
- steering wheel
- Prior art date
- 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.)
- Expired - Fee Related
Links
Landscapes
- Motorcycle And Bicycle Frame (AREA)
Abstract
The utility model discloses a kind of amphibious unmanned plane, be made up of flight control system, aircraft body, engine installation, take-off and landing device and equipment five major part of taking photo by plane.Unmanned controller and read-out support are fixed together, and according to the image of passback, can accomplish certain over the horizon flight.Engine installation adopts lithium ion polymer battery that is green, environmental protection, really accomplishes pollution-free, the environmental demands of zero-emission.This unmanned plane wing adopts high mounted wing design, and with the dihedral angle of certain angle, wing can auto modification to keep level.Not only allowed aircraft have larger lift and good stability, and make the picture of taking photo by plane more stable.This wing nut is fixed on fuselage simultaneously, and wing quick release, is convenient for carrying, and aircraft modularization is higher.Difference according to flight environment of vehicle can select different take-off and landing devices, have floating drum and alighting gear two kinds of modes available.This unmanned plane cost is low, the degree of modularity is high, feature richness is novel, simple to operate.
Description
Technical field
The utility model belongs to aviation aircraft field, especially relates to a kind of amphibious unmanned plane of taking photo by plane.
Background technology
The remote control fixed-wing unmanned plane used both at home and abroad is at present rely on alighting gear rolling start or direct hand to throw to fly mostly, and this restriction of Method compare by place of taking off, must at broad view, takes off in the land of Land leveling.And aquatic unmanned aerial vehicle compares land fixed-wing Development of UAV relatively slowly both at home and abroad, and existing aquatic unmanned aerial vehicle, be integration manufacture substantially, cost intensive, complicated operation; And the work circumstances safe degree of unmanned plane is lower, affect greatly by external factor, when therefore aircraft damages, maintenance difficulty is large, and maintenance cost is high.And current hydroairplane function singleness, well can not adapt to the flight demand of user.Therefore design a kind of low cost, modularization, feature richness, aquatic unmanned aerial vehicle simple to operate be significant and good market outlook.
Summary of the invention
The purpose of this utility model is to provide a kind of amphibious unmanned plane, this unmanned plane low cost, modularization, feature richness, simple to operate.
The utility model is achieved through the following technical solutions: a kind of amphibious unmanned plane, primarily of flight control system, aircraft body, engine installation, take-off and landing device and equipment five major part composition of taking photo by plane; Aircraft control system mainly comprises remote controller, remote control receiver, aileron steering wheel, yaw rudder steering wheel, elevating rudder steering wheel and navigation light; Aircraft body is formed primarily of fuselage, wing, empennage (comprising horizontal tail and vertical fin); Engine installation mainly comprises: screw propeller, brushless motor, motor fixed base, electronic governor, lithium ion polymer battery; Take-off and landing device is primarily of floating drum and alighting gear two parts composition; Equipment of taking photo by plane mainly comprises: small-sized image pickup head, diaxon The Cloud Terrace, lithium ion polymer battery, osd data laminating module, data transmitter, GPS, data receiver, display/panel bracket and read-out; It is characterized in that: read-out display/panel bracket is fixing on a remote control, and data receiver and data receiver electromechanical source are fixed on read-out; The screw propeller at head place is connected with the turning cylinder nut of motor, motor is fixed in motor fixed base and is connected with electronic governor with wire, the rearmounted lithium ion polymer battery of electronic governor, the signal wire (SW) of electronic governor is connected to and is positioned on the remote control receiver of waist, waist is provided with osd data laminating module and data transmitter, and both are connected with signal wire (SW); Fuselage bottom is provided with diaxon The Cloud Terrace, diaxon The Cloud Terrace secures small-sized image pickup head, and its AV output line is connected with osd data laminating module, is provided with GPS at the top of central fuselage; Install the green navigation light in the left red right side at wing two ends, fuselage connects vertical fin, connects horizontal tail after vertical fin.
The board joints of fuselage bottom described in the utility model uses water-reducible finish.
Described in the utility model when flying on the water, floating drum installed by aircraft, and be provided with two mounting brackets bottom aircraft, floating drum is directly installed on support, while at floating drum afterbody, a steering wheel is installed, to realize the function that aircraft turns on the water surface.
Described in the utility model when flying on land, alighting gear installed by aircraft, after adopting, bikini is installed, tail wheel thicker wire is arranged on afterbody, steel wire one end and yaw rudder are fixed together simultaneously, when so just can not install a steering wheel additional, realize turning to of aircraft, greatly reduce the cost of manufacture of aircraft.
Wing at aircraft described in the utility model and rear body are provided with aileron steering wheel, elevating rudder steering wheel, yaw rudder steering wheel.
Described in the utility modelly at empennage, a white navigation light is installed.
Forebody top described in the utility model hinge is connected with the fuselage of side, and top is connected with opposite side fuselage VELCRO.
Installed four bolt of rear end plates in both sides fuselage in the middle part of aircraft described in the utility model, bolt of rear end plate is through wing, and wing opening two ends plank is reinforced, and directly wing is fixed on fuselage with nut.
Floating drum described in the utility model and alighting gear two kinds of available installations of mode.
The utility model has the advantages that: this unmanned plane low cost, modularization, feature richness, simple to operate, this unmanned plane wing adopts high mounted wing design, and with the dihedral angle of certain angle, wing can auto modification to keep level.Not only allowed aircraft have larger lift and good stability, and make the picture of taking photo by plane more stable.This wing nut is fixed on fuselage simultaneously, and wing quick release, is convenient for carrying, and aircraft modularization is higher.Difference according to flight environment of vehicle can select different take-off and landing devices, have floating drum and alighting gear two kinds of modes available.This unmanned plane cost is low, the degree of modularity is high, feature richness is novel, simple to operate.
Accompanying drawing explanation
Fig. 1 is the surface facility structural representation of the utility model unmanned plane.
Fig. 2 is the structure birds-eye view of the utility model unmanned plane.
Structure left view when Fig. 3 is the utility model unmanned plane installation floating drum.
Structure left view when Fig. 4 is the utility model unmanned plane installation alighting gear.
Fig. 5 is the structural front view of the utility model unmanned plane.
In the drawings: 1. remote controller 2. display/panel bracket 3. data receiver electromechanical source 4. read-out 5. data receiver 6. screw propeller 7. motor 8. motor fixed base 9. electronic governor 10. lithium ion polymer battery 11. remote control receiver 12.OSD data investigation module 13. data transmitter 14. small-sized image pickup head 15. diaxon The Cloud Terrace 16. wing 17. navigation light 18.GPS 19. horizontal tail 20. vertical fin 21. floating drum 22. alighting gear.
Detailed description of the invention
Below in conjunction with accompanying drawing and concrete assemble method, the utility model is further described.
The utility model is achieved in that it comprises flight control system, aircraft body, engine installation, take-off and landing device and equipment five major part of taking photo by plane.Read-out 4 display/panel bracket 2 is fixed on remote controller 1, and very convenient like this operator manipulates aircraft according to the picture of passback of taking photo by plane, and allows aircraft have more operability, safety.Data receiver 5 is fixing on the display screen 4, powers to data receiver 5 with one piece of lithium ion polymer battery 3.The screw propeller 6 at head place is connected with the turning cylinder nut of motor 7, motor is fixed in motor fixed base 8 and is connected with electronic governor 9 with wire, lithium cell 10 powers to electronic governor 9 simultaneously, and the signal wire (SW) of electronic governor 9 is connected to and is positioned on the remote control receiver 11 of waist.Waist is provided with osd data laminating module 12 and data transmitter 13, and both are connected with signal wire (SW).Lithium cell 10 powers to osd data laminating module 12 and electronic governor 9 simultaneously, while reduction manufacturing cost, alleviates the weight of aircraft greatly, enhances the maneuverability of aircraft.Fuselage bottom is provided with diaxon The Cloud Terrace 15, diaxon The Cloud Terrace 15 secures small-sized image pickup head 14, and its AV output line is connected with osd data laminating module 12, is provided with GPS18 at the top of central fuselage.GPS18 is arranged on outside fuselage and can fuselage material is avoided the stop of signal by actv., improves the signal strength of GPS.Simultaneously the green navigation light 17 in the left red right side is installed at wing 16 two ends, at vertical fin 20, a white navigation light 17 is installed.Installing navigation light 17 can allow operator better see unmanned plane during flying attitude clearly, improves the safety and stability of flight.Use water-reducible finish at the board joints of fuselage bottom, while improving unmanned plane water resistance, owing to creating waterproofing membrane, substantially increase junction by force intensity, make aircraft safer, firm.When flying on the water, floating drum 21 installed by aircraft, and be provided with two mounting brackets bottom aircraft, floating drum is directly installed on support, installs a steering wheel, to realize the function that aircraft turns on the water surface at floating drum afterbody simultaneously.When flying on land, alighting gear 22 installed by aircraft, and after adopting, bikini is installed, tail wheel thicker wire is arranged on afterbody, and steel wire one end and yaw rudder are fixed together, when so just can not install a steering wheel additional simultaneously, realize turning to of aircraft, greatly reduce the cost of manufacture of aircraft.
First mmi machine body top hinge is connected with the fuselage of side, and top is connected with opposite side fuselage VELCRO, and such benefit is conveniently to change battery and convenient maintenance engine installation.Installed four bolt of rear end plates in both sides fuselage in the middle part of aircraft, bolt of rear end plate is through wing, and wing 16 opening two ends plank is reinforced, and therefore using nuts is directly fixed on wing on fuselage.Allow aircraft easily can unload lower wing, be convenient for carrying, simultaneously when wing is damaged, only need change wing, greatly reduce service expenditure.High mounted wing design that what wing adopted is, simultaneously with certain dihedral angle, while allowing aircraft have larger lift and good stability, indirectly also allows the picture of taking photo by plane more stable.When flying on land, alighting gear installed by aircraft, and after adopting, bikini is installed, tail wheel thicker wire is arranged on afterbody, and steel wire one end and yaw rudder are fixed together, when so just can not install a steering wheel additional simultaneously, realize turning to of aircraft, greatly reduce the cost of manufacture of aircraft.When flying on the water, floating drum installed by aircraft, and be provided with two mounting brackets bottom aircraft, floating drum is directly installed on support, installs a steering wheel, to realize the function that aircraft turns on the water surface at floating drum afterbody simultaneously.Read-out is directly fixed on a remote control, makes operation more simple and convenient.
Claims (8)
1. an amphibious unmanned plane, primarily of flight control system, aircraft body, engine installation, take-off and landing device and equipment five major part composition of taking photo by plane; Aircraft control system mainly comprises remote controller, remote control receiver, aileron steering wheel, yaw rudder steering wheel, elevating rudder steering wheel and navigation light; Aircraft body is formed primarily of fuselage, wing, empennage; Engine installation mainly comprises: screw propeller, brushless motor, motor fixed base, electronic governor, lithium ion polymer battery; Take-off and landing device is primarily of floating drum and alighting gear two parts composition; Equipment of taking photo by plane mainly comprises: small-sized image pickup head, diaxon The Cloud Terrace, lithium ion polymer battery, osd data laminating module, data transmitter, GPS, data receiver, display/panel bracket and read-out; It is characterized in that: read-out display/panel bracket is fixing on a remote control, and data receiver and data receiver electromechanical source are fixed on read-out; The screw propeller at head place is connected with the turning cylinder nut of motor, motor is fixed in motor fixed base and is connected with electronic governor with wire, the rearmounted lithium ion polymer battery of electronic governor, the signal wire (SW) of electronic governor is connected to and is positioned on the remote control receiver of waist, waist is provided with osd data laminating module and data transmitter, and both are connected with signal wire (SW); Fuselage bottom is provided with diaxon The Cloud Terrace, diaxon The Cloud Terrace secures small-sized image pickup head, and its AV output line is connected with osd data laminating module, is provided with GPS at the top of central fuselage; Install the green navigation light in the left red right side at wing two ends, fuselage connects vertical fin, connects horizontal tail after vertical fin.
2. the amphibious unmanned plane of one according to claim 1, is characterized in that: the board joints of described fuselage bottom uses water-reducible finish.
3. the amphibious unmanned plane of one according to claim 1, is characterized in that: when flying on the water, and floating drum installed by aircraft, and be provided with two mounting brackets bottom aircraft, floating drum is directly installed on support, installs a steering wheel at floating drum afterbody simultaneously.
4. the amphibious unmanned plane of one according to claim 1, is characterized in that: when flying on land, and alighting gear installed by aircraft, and after adopting, bikini is installed, and tail wheel thicker wire is arranged on afterbody, and steel wire one end and yaw rudder are fixed together simultaneously.
5. the amphibious unmanned plane of one according to claim 1, is characterized in that: on the wing and rear body of aircraft, be provided with aileron steering wheel, elevating rudder steering wheel, yaw rudder steering wheel.
6. the amphibious unmanned plane of one according to claim 1, is characterized in that: be provided with a white navigation light at empennage.
7. the amphibious unmanned plane of one according to claim 1, is characterized in that: forebody top hinge is connected with the fuselage of side, and top is connected with opposite side fuselage VELCRO.
8. the amphibious unmanned plane of one according to claim 1, it is characterized in that: four bolt of rear end plates have been installed in the both sides fuselage in the middle part of described aircraft, bolt of rear end plate is through wing, and wing opening two ends plank is reinforced, and directly wing is fixed on fuselage with nut.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520343052.9U CN204726655U (en) | 2015-05-26 | 2015-05-26 | A kind of amphibious unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520343052.9U CN204726655U (en) | 2015-05-26 | 2015-05-26 | A kind of amphibious unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204726655U true CN204726655U (en) | 2015-10-28 |
Family
ID=54385027
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520343052.9U Expired - Fee Related CN204726655U (en) | 2015-05-26 | 2015-05-26 | A kind of amphibious unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204726655U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106627010A (en) * | 2016-11-17 | 2017-05-10 | 苏州航天系统工程有限公司 | Water-air amphibious unmanned aerial vehicle |
| CN106621379A (en) * | 2017-01-16 | 2017-05-10 | 王长民 | Telecontrolled amphibious aircraft |
-
2015
- 2015-05-26 CN CN201520343052.9U patent/CN204726655U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106627010A (en) * | 2016-11-17 | 2017-05-10 | 苏州航天系统工程有限公司 | Water-air amphibious unmanned aerial vehicle |
| CN106621379A (en) * | 2017-01-16 | 2017-05-10 | 王长民 | Telecontrolled amphibious aircraft |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN106143898B (en) | A kind of VTOL tilting rotor fixed wing aircraft | |
| CN202080435U (en) | Ranked dual-rotor vertically-lifted unmanned aerial vehicle (UAV) | |
| CN105620735B (en) | High-speed multi-rotor vertical take-off and landing aircraft | |
| CN106809402B (en) | Automatic auxiliary landing system of rotor unmanned aerial vehicle and control method thereof | |
| CN207758993U (en) | The aerofoil system of unmanned plane | |
| CN205293106U (en) | Novel unmanned aerial vehicle nacelle mounting structure | |
| CN202657252U (en) | Vehicle-mounted flying frame | |
| CN204642152U (en) | New oil moves many rotors plant protection unmanned plane | |
| CN111731475B (en) | Vertical take-off and landing tilting composite wing aircraft | |
| CN103264626A (en) | Electric air-ground dual-purpose helicopter | |
| CN105116933A (en) | Unmanned aircraft and method preventing unmanned aircraft from separation from control area | |
| CN203593161U (en) | Variable multi-rotor UAV (unmanned aerial vehicle) | |
| CN204726655U (en) | A kind of amphibious unmanned plane | |
| CN213414216U (en) | Vertical take-off and landing fixed wing unmanned aerial vehicle | |
| CN105129097A (en) | Unmanned aerial vehicle capable of taking off and landing vertically | |
| CN103350624B (en) | Propelling type flying car with spiral wings | |
| CN201941976U (en) | Amphibious aircraft with tilt rotor | |
| CN205044948U (en) | Solar energy unmanned aerial vehicle | |
| CN107161329A (en) | A kind of restructural amphibious robot | |
| CN105759837A (en) | Power transmission line multi-rotor airship inspection system | |
| CN207450221U (en) | A kind of unmanned plane of variable aerodynamic arrangement | |
| CN104149565A (en) | Air and ground dual-purpose multifunctional trolley | |
| CN108248858A (en) | A kind of amphibious unmanned plane | |
| CN213768958U (en) | Vertical take-off and landing fixed wing unmanned aerial vehicle | |
| CN112644686B (en) | Tandem wing overall arrangement solar energy unmanned aerial vehicle |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20151028 Termination date: 20160526 |