CN106394862A - Folding type hybrid power unmanned aerial vehicle - Google Patents

Folding type hybrid power unmanned aerial vehicle Download PDF

Info

Publication number
CN106394862A
CN106394862A CN201610896008.XA CN201610896008A CN106394862A CN 106394862 A CN106394862 A CN 106394862A CN 201610896008 A CN201610896008 A CN 201610896008A CN 106394862 A CN106394862 A CN 106394862A
Authority
CN
China
Prior art keywords
fixed
wing
hybrid power
unmanned plane
cover
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.)
Pending
Application number
CN201610896008.XA
Other languages
Chinese (zh)
Inventor
马飞
Original Assignee
马飞
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 马飞 filed Critical 马飞
Priority to CN201610896008.XA priority Critical patent/CN106394862A/en
Publication of CN106394862A publication Critical patent/CN106394862A/en
Pending legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/30Parts of fuselage relatively movable to reduce overall size for storage
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/04Helicopters
    • B64C27/08Helicopters with two or more rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2201/00Unmanned aerial vehicles; Equipment therefor
    • B64C2201/02Unmanned aerial vehicles; Equipment therefor characterized by type of aircraft
    • B64C2201/024Helicopters, or autogiros
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2201/00Unmanned aerial vehicles; Equipment therefor
    • B64C2201/04Unmanned aerial vehicles; Equipment therefor characterised by type of power plant
    • B64C2201/042Unmanned aerial vehicles; Equipment therefor characterised by type of power plant by electric motors; Electric power sources therefor, e.g. fuel cells, solar panels or batteries

Abstract

The invention discloses a folding type hybrid power unmanned aerial vehicle which is characterized in that a vehicle body lower cover is connected with and fixed to a vehicle body upper cover through bolts for forming a vehicle body; a solar cell panel is fixed to the vehicle body upper cover through fixing bolts; one end of each wing is fixed to the vehicle body through an adjustment shaft, and a motor is arranged at the other end of the wing correspondingly; the motors are connected with and fixed to the wings through the bolts; one end of each transmission shaft is connected with a motor output shaft, and the other end thereof is connected with a propeller; support bases are connected with and fixed around the vehicle body lower cover through the bolts; and the vehicle body is internally provided with a storage battery bank, a switch module, a controller and a motor driver. The folding type hybrid power unmanned aerial vehicle is reasonable in design and convenient to use; solar power and storage battery simultaneous power supply can be realized; the battery endurance is high; and a folding type wing structure improves a space utilization ratio of the folding type hybrid power unmanned aerial vehicle.

Description

A kind of folding hybrid power unmanned plane
Technical field
The present invention relates to a kind of vehicle technology field, specifically a kind of folding hybrid power unmanned plane.
Background technology
At present, with the fast development of the communication technology, flight control technology, due to its small volume, light is excellent for unmanned plane Point, thus unmanned plane is gradually widely used in many fields.Unmanned plane mainly has fixed-wing unmanned plane, depopulated helicopter and many rotations Three kinds of wing unmanned plane, its small and medium size unmanned aerial vehicles also includes umbrella wing unmanned plane, flapping wing unmanned plane and unmanned spaceship/spacecraft etc..And fixed-wing is no Man-machine it is most widely used.On market, fixed-wing unmanned plane, using four-axle linked, is capable of the appearance of space optional position State.But fixed-wing unmanned plane often due to its huge structure lead to take up room larger, and due to adopting single battery Driving leads to the endurance of unmanned plane poor.
For above-mentioned deficiency, need design and develop a kind of folding hybrid power unmanned plane, can supply above-mentioned each Individual shortcoming.
Content of the invention
In order to solve above-mentioned problem, the present invention provides a kind of folding hybrid power unmanned plane.
The technical scheme is that:A kind of folding hybrid power unmanned plane, including wing, screw, solar energy Cell panel, organism top case, body lower cover it is characterised in that:Described body lower cover and organism top case are bolted fixation, structure Become body;Described base plate is fixed under body by tight fixed bolt and covers;Described solar panel is fixed by fixing bolt On organism top case;Described wing one end is fixed on body by adjustment axis, and the wing other end is provided with motor, using spiral shell Bolt is connected;Described power transmission shaft one end connects motor output shaft, and one end connects screw;Described support base is bolted It is fixed on the surrounding of body lower cover;Described stator is arranged on body, and stator one end connecting spring, other end coil insertion device In the draw-in groove of wing one end;Described internal body is provided with batteries, and batteries are connected with the output end of solar panel Connect the input of handover module;The output end of described handover module connects controller one end, and the other end of controller connects electricity Machine driver;Output end four motors of parallel connection of described motor driver;Described bluetooth module is connected with the communication interface of controller Connect;
Preferably, described organism top case and body lower cover surrounding are provided with four holes, and adjustment axis are fixed on this four holes, And organism top case and body lower cover profile adopt circular arc camber structure, reduce air drag, are provided with batteries, control in body Device processed, bluetooth module and handover module;
Preferably, the power of described solar panel is 100W, and thickness is 5MM, using circular configuration, and surrounding setting There are four installing holes, be connected on organism top case by fixing bolt;
Preferably, described wing is provided with four, using circular arc type structure, is fixed on body surrounding by adjustment axis, and One end that wing is connected with adjustment axis is provided with two T-shaped draw-in grooves, and both are in 90 degree, and the other end is provided with motor installing hole, Motor is bolted and is vertically fixed on wing;
Preferably, described motor is provided with four, using 100W brshless DC motor;
Preferably, described screw is provided with four, using APC1540 model, is fixed on power transmission shaft by spline connection On;
Preferably, described stator one end adopts arc structure, and in the T-slot of embedded wing, the other end is connected with spring, It is fixed in four grooves of body;
Preferably, the input of described handover module connects batteries and solar panel, wherein in handover module MPPT controller connect solar panel, control solar panel output voltage, PWM1 connect batteries, control In parallel with PWM2 after the break-make of batteries, and both series connection, PWM2 is in parallel with inductance L2, diode D3, electric capacity C2, leads to simultaneously The dutycycle overregulating PWM2 carrys out the output voltage of regulation power supply.
Compared with prior art, the effect of the present invention and effect are:The present invention is for a kind of folding hybrid power no Man-machine, it is reasonable in design, easy to use, is capable of solar energy and battery is powered simultaneously, endurance is long;Wireless blue tooth sets Meter disclosure satisfy that long-distance remote control unmanned plane;Passing through to adjust wing simultaneously, drawing four wings in thus improving the space of unmanned plane Utilization rate.The four axle power of the present invention are able to ensure that unmanned plane realizes the attitude of optional position in the air.
Brief description
Fig. 1 is the overall unfolding assumption diagram of the present invention;
Fig. 2 is that the entirety of the present invention draws Facad structure figure in;
Fig. 3 is that the entirety of the present invention draws backside structure figure in;
Fig. 4 is the overall control block diagram of the present invention;
Fig. 5 is the handover module circuit diagram of the present invention;
In figure:1st, motor;2nd, wing;3rd, power transmission shaft;4th, screw;5th, adjustment axis;6th, organism top case;7th, fixing bolt; 8th, solar panel;9th, support base;10th, stator;11st, body lower cover;12nd, tight fixed bolt;13rd, base plate;14th, battery Group;15th, handover module;16th, bluetooth module;17th, motor driver;18th, controller.
Specific embodiment
With specific embodiment, the present invention is described in further detail below in conjunction with the accompanying drawings:
As Figure 1-3, a kind of folding hybrid power unmanned plane, including wing 2, screw 4, solar panel 8th, organism top case 6, body lower cover 11.Wherein, body lower cover 11 and organism top case 6 are bolted fixing composition body;Bottom Plate 13 is fixed on body lower cover 11 by tight fixed bolt 12;Solar panel 8 is fixed on organism top case by fixing bolt 7 On 6;Wing 2 one end is fixed on body by adjustment axis 5, and wing 2 other end is provided with motor 1, with bolts solid Fixed;Power transmission shaft 3 one end connects motor 1 output shaft, and one end connects screw 4;Support base 9 is bolted and is fixed under body The surrounding of lid 11;Stator 10 is arranged on body, and stator 10 one end connecting spring, and the other end embeds wing 2 one end In draw-in groove.
Wherein, organism top case 6 and body lower cover 11 surrounding are provided with four holes, and adjustment axis 5 are fixed on this four holes, and Organism top case 6 and body lower cover 11 profile adopt circular arc camber structure, reduce air drag, are provided with batteries in body 14th, controller 18, bluetooth module 16 and handover module 15;The power of solar panel 8 is 100W, and thickness is 5MM, using circle Shape structure, and surrounding is provided with four installing holes, is connected on organism top case by fixing bolt 7;Motor 1 is provided with four, Using 100W brshless DC motor.
Wing 2 is provided with four, using circular arc type structure, is fixed on body surrounding by adjustment axis 5, and wing 2 and tune One end that nodal axisn 5 connects is provided with two T-shaped draw-in grooves, and both are in 90 degree, and the other end is provided with motor installing hole, and motor 1 leads to Cross bolt connection to be vertically fixed on wing 2;Screw 4 is provided with four, using APC1540 model, solid by spline connection It is scheduled on power transmission shaft 3;Stator 10 one end adopts arc structure, and in the T-slot of embedded wing 2, the other end is connected with spring, Gu It is scheduled in four grooves of body.
As shown in figure 4, internal body is provided with batteries 14, and the output of batteries 14 and solar panel 8 End connects the input of handover module 15;The output end of handover module 15 connects controller 18 one end, and controller 18 is another End connects motor driver 17;Output end four motors 1 of parallel connection of motor driver 17;Bluetooth module 16 is logical with controller 18 Letter interface connects.
As shown in figure 5, the input of handover module 15 connects batteries 14 and solar panel 8, wherein switch mould MPPT controller in block 15 connects solar panel 8, controls the output voltage of solar panel 8, and PWM1 connects electric power storage Pond group 14, controls the break-make of batteries 14, and, PWM2 and inductance L2, diode D3, electric capacity in parallel with PWM2 after both series connection C2 is in parallel, simultaneously by adjusting the dutycycle of PWM2 come the output voltage of regulation power supply.
The present invention is using as follows:When needing to open unmanned plane, turn clockwise wing 2, thus opening four wings 2, Start unmanned plane afterwards.After stopping unmanned plane, rotate counterclockwise wing 2, thus draw four wings 2 in.It is in unmanned plane Under state of flight, when sunny, the electric energy that solar panel 8 is collected is in maximum power output, by handover module 15 power to motor 1, and now solar panel 8 power supply is powered more than batteries 14;When sunlight is inadequate, solar-electricity The electric energy that pond plate 8 is collected is not enough, is now mainly powered by batteries 14, and batteries 14 power supply is more than solar panel 8 power supplies.
Above by the introduction to described embodiment, elaborate general principle and the design of the present invention.But the present invention is exhausted It is not limited to embodiment described above, every similar changes and improvements made based on technical scheme, these changes Change and improvement both falls within scope of the claimed invention.Claimed scope by appending claims and its Equivalent thereof.

Claims (8)

1. a kind of folding hybrid power unmanned plane, including on wing (2), screw (4), solar panel (8), body Lid (6), body lower cover (11) it is characterised in that:Described body lower cover (11) and organism top case (6) are bolted fixing structure Become body;Described base plate (13) is fixed on body lower cover (11) by tight fixed bolt (12);Described solar panel (8) is led to Cross fixing bolt (7) to be fixed on organism top case (6);Described wing (2) one end is fixed on body by adjustment axis (5), and Wing (2) other end is provided with motor (1), is fixed with bolts;Described power transmission shaft (3) one end connects motor (1) output Axle, one end connects screw (4);Described support base (9) is bolted the surrounding being fixed on body lower cover (11);Described solid Stator (10) is arranged on body, and stator (10) one end connecting spring, and the other end embeds in the draw-in groove of wing (2) one end; Described internal body is provided with batteries (14), and batteries (14) are connected with the output end of solar panel (8) and cut The input of die change block (15);Output end connection controller (18) one end of described handover module (15), and controller (18) The other end connects motor driver (17);Output end four motors (1) of parallel connection of described motor driver (17);Described bluetooth mould Block (16) is connected with the communication interface of controller (18).
2. a kind of folding hybrid power unmanned plane according to claim 1 it is characterised in that:Described organism top case (6) and body lower cover (11) surrounding is provided with four holes, adjustment axis (5) are fixed on this four holes, and organism top case (6) and machine Body lower cover (11) profile adopts circular arc camber structure, reduces air drag, is provided with batteries (14), controller in body (18), bluetooth module (16) and handover module (15).
3. a kind of folding hybrid power unmanned plane according to claim 1 it is characterised in that:Described solar cell The power of plate (8) is 100W, and thickness is 5MM, and using circular configuration, and surrounding is provided with four installing holes, by fixing bolt (7) it is connected on organism top case.
4. a kind of folding hybrid power unmanned plane according to claim 1 it is characterised in that:Described wing (2) sets It is equipped with four, using circular arc type structure, is fixed on body surrounding by adjustment axis (5), and wing (2) is connected with adjustment axis (5) One end be provided with two T-shaped draw-in grooves, and both be in 90 degree, the other end is provided with motor installing hole, motor (1) by bolt company Connect and be vertically fixed on wing (2).
5. a kind of folding hybrid power unmanned plane according to claim 1 it is characterised in that:Described motor (1) sets It is equipped with four, using 100W brshless DC motor.
6. a kind of folding hybrid power unmanned plane according to claim 1 it is characterised in that:Described screw (4) It is provided with four, using APC1540 model, be fixed on power transmission shaft (3) by spline connection.
7. a kind of folding hybrid power unmanned plane according to claim 1 it is characterised in that:Described stator (10) One end adopts arc structure, and in the T-slot of embedded wing (2), the other end is connected with spring, is fixed in four grooves of body.
8. a kind of folding hybrid power unmanned plane according to claim 1 it is characterised in that:Described handover module (15) input connects batteries (14) and solar panel (8), the wherein MPPT controller in handover module (15) Connect solar panel (8), control the output voltage of solar panel (8), PWM1 connects batteries (14), control and store In parallel with PWM2 after the break-make of battery pack (14), and both series connection, PWM2 is in parallel with inductance L2, diode D3, electric capacity C2, simultaneously By adjusting the dutycycle of PWM2 come the output voltage of regulation power supply.
CN201610896008.XA 2016-10-13 2016-10-13 Folding type hybrid power unmanned aerial vehicle Pending CN106394862A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610896008.XA CN106394862A (en) 2016-10-13 2016-10-13 Folding type hybrid power unmanned aerial vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610896008.XA CN106394862A (en) 2016-10-13 2016-10-13 Folding type hybrid power unmanned aerial vehicle

Publications (1)

Publication Number Publication Date
CN106394862A true CN106394862A (en) 2017-02-15

Family

ID=59229340

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201610896008.XA Pending CN106394862A (en) 2016-10-13 2016-10-13 Folding type hybrid power unmanned aerial vehicle

Country Status (1)

Country Link
CN (1) CN106394862A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107117296A (en) * 2017-04-05 2017-09-01 西北工业大学 A kind of foldable quadrotor frame
CN107512390A (en) * 2017-08-22 2017-12-26 北京航宇测通电子科技有限公司 A kind of disc-shaped unmanned machine
CN108408033A (en) * 2018-01-31 2018-08-17 芜湖市海联机械设备有限公司 A kind of Backpack type unmanned plane
CN108820229A (en) * 2018-06-22 2018-11-16 李帷笳 Hybrid power unmanned plane based on computer mode control
CN111268091A (en) * 2020-02-20 2020-06-12 南京航空航天大学 Four rotor unmanned aerial vehicle of folded cascade of high continuation of journey
CN111703580A (en) * 2020-05-28 2020-09-25 上海交通大学 Electric propulsion rotor craft power system and control method thereof

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103840745A (en) * 2013-09-13 2014-06-04 武汉美格科技有限公司 Solar energy system for unmanned plane to use
CN204368418U (en) * 2014-11-27 2015-06-03 成都盛世普益科技有限公司 A kind of double dynamical four rotor wing unmanned aerial vehicles
CN204895868U (en) * 2015-06-04 2015-12-23 东莞中寰智能航空科技有限公司 Novel foldable unmanned aerial vehicle
CN205044949U (en) * 2015-09-21 2016-02-24 温州乐享科技信息有限公司 Unmanned aerial vehicle with multiple rotor wings
JP3202876U (en) * 2015-12-15 2016-02-25 忠久 福田 Diagnostic equipment
CN205366072U (en) * 2015-12-31 2016-07-06 天津御遨航空科技发展有限公司 Unmanned aerial vehicle

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103840745A (en) * 2013-09-13 2014-06-04 武汉美格科技有限公司 Solar energy system for unmanned plane to use
CN204368418U (en) * 2014-11-27 2015-06-03 成都盛世普益科技有限公司 A kind of double dynamical four rotor wing unmanned aerial vehicles
CN204895868U (en) * 2015-06-04 2015-12-23 东莞中寰智能航空科技有限公司 Novel foldable unmanned aerial vehicle
CN205044949U (en) * 2015-09-21 2016-02-24 温州乐享科技信息有限公司 Unmanned aerial vehicle with multiple rotor wings
JP3202876U (en) * 2015-12-15 2016-02-25 忠久 福田 Diagnostic equipment
CN205366072U (en) * 2015-12-31 2016-07-06 天津御遨航空科技发展有限公司 Unmanned aerial vehicle

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107117296A (en) * 2017-04-05 2017-09-01 西北工业大学 A kind of foldable quadrotor frame
CN107512390A (en) * 2017-08-22 2017-12-26 北京航宇测通电子科技有限公司 A kind of disc-shaped unmanned machine
CN108408033A (en) * 2018-01-31 2018-08-17 芜湖市海联机械设备有限公司 A kind of Backpack type unmanned plane
CN108820229A (en) * 2018-06-22 2018-11-16 李帷笳 Hybrid power unmanned plane based on computer mode control
CN111268091A (en) * 2020-02-20 2020-06-12 南京航空航天大学 Four rotor unmanned aerial vehicle of folded cascade of high continuation of journey
CN111268091B (en) * 2020-02-20 2021-05-11 南京航空航天大学 Four rotor unmanned aerial vehicle of folded cascade of high continuation of journey
CN111703580A (en) * 2020-05-28 2020-09-25 上海交通大学 Electric propulsion rotor craft power system and control method thereof
CN111703580B (en) * 2020-05-28 2021-02-12 上海交通大学 Electric propulsion rotor craft power system and control method thereof

Similar Documents

Publication Publication Date Title
CN106394862A (en) Folding type hybrid power unmanned aerial vehicle
CN204606221U (en) A kind of many rotor fuel-electrics energy conversion aircraft
CN103840745A (en) Solar energy system for unmanned plane to use
CN205901416U (en) Unmanned aerial vehicle
CN105129079A (en) Hybrid power long-endurance multi-shaft air vehicle
CN201494324U (en) Solar electric motor car
CN203753316U (en) Auxiliary power generation device for electric vehicle
CN205203380U (en) Adopt gaseous unmanned vehicles who increases continuation of journey
CN205044954U (en) Coaxial two thick liquid hybrid gyroplane
CN101607600A (en) Solar-wind hybrid power airplane
CN202237261U (en) Solar toy airplane
CN202463597U (en) Electric vehicle adopting wind-solar hybrid power generation
CN203246336U (en) Solar energy-driven tricycle
CN203154819U (en) Hydrogen power toy plane
CN207208470U (en) A kind of modular unmanned plane of dynamical system
CN201932016U (en) Solar-energy electric vehicle
CN109606623A (en) Intelligent modularized solar energy unmanned plane
CN206910801U (en) One kind folds model aircraft
CN204568048U (en) A kind of eight axles drive the small-sized dirigible of solar power remote control
CN204749876U (en) Electric automobile power generation facility
CN205931255U (en) Spherical unmanned aerial vehicle based on ARM
CN206261005U (en) A kind of umbrella using solar energy with fan assembly
CN103660966A (en) Integrated automatic charging system for new energy automobiles and electric automobile
CN205265327U (en) A portable charging device for electric automobile
CN204871615U (en) Aircraft of double cell power supply

Legal Events

Date Code Title Description
PB01 Publication
C06 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20170215