CN203876983U - Spherical flight device - Google Patents

Spherical flight device Download PDF

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Publication number
CN203876983U
CN203876983U CN201420219002.5U CN201420219002U CN203876983U CN 203876983 U CN203876983 U CN 203876983U CN 201420219002 U CN201420219002 U CN 201420219002U CN 203876983 U CN203876983 U CN 203876983U
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CN
China
Prior art keywords
vertical plane
iii
rudder
motor
plane
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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.)
Expired - Fee Related
Application number
CN201420219002.5U
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Chinese (zh)
Inventor
李佳辉
解晓亮
喻宏飞
毕耕
王妍玮
季寿天
曹雯雯
宋旭
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李佳辉
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Priority to CN201420219002.5U priority Critical patent/CN203876983U/en
Application granted granted Critical
Publication of CN203876983U publication Critical patent/CN203876983U/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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Abstract

The utility model belongs to the technical field of an aircraft, and definitely relates to a remote control aircraft model. The utility model relates to a spherical flight device which integrates the function of vertical takeoff and landing and the characteristics of a fixed wing aircraft. The spherical flight device is characterized in that the rear of a motor is fixedly connected with a motor fixing plate; the motor fixing plate is fixed at the intersection position of a vertical plane II and a vertical plane IV, so that the motor is positioned on the axis above the center of a sphere; solar cell panels are respectively arranged on the outer surfaces of a vertical plane I, the vertical plane II, a vertical plane III, the vertical plane IV and a horizontal plane V; a steering engine I and a steering engine III are respectively arranged on the two sides in the vertical plane III; a steering engine II is arranged at the intersection position of the vertical plane I and the vertical plane III; the vertical plane I and the vertical plane III are respectively provided with a control plane I, a control plane II, a control plane III and a control plane IV. The spherical flight device has the advantages and the positive effects of being simple in structure, low in cost, convenient to operate and use, simple and safe to control and long in duration of flight, and integrating the function of vertical takeoff and landing and the characteristics of the fixed wing aircraft; the spherical flight device can be used for multiple fields such as military reconnaissance, patrol, rescue, aerial photography, celebration activities, advertising, remote controlled toys, model airplanes and scientific research.

Description

Spherical flight instruments
Technical field
The utility model belongs to vehicle technology field, is exactly a kind of telecontrolled aircraft model, relates to a kind of feature of vertical takeoff and landing and fixed wing aircraft that has both in the spherical flight instruments of one.This aircraft can be used for military surveillance, patrol, and rescue, takes photo by plane, celebration activity, advertising, remote-control toy, model airplane, a plurality of fields such as scientific research.
Background technology
Existing fixed wing aircraft and helicopter are from the structure of engine installation, whole aerodynamic arrangement, handle basic continuity traditional mode in principle and control method, conventionally adopt the screw propeller of High Rotation Speed for flying, to provide power in the outside of aircraft, once aircraft is in the situation that out of control like this, the screw propeller of aircraft High Rotation Speed will damage people or thing around, has potential safety hazard; Aircraft also needs to have sufficient power resources to extend the time of duration flight in the process of flight, using at present more way is to use clean energy resource solar panel, but these aircraft just surface, with a part of solar panel, are not very high to the degree of utilization of solar power; Aircraft is in military surveillance, and patrol, rescues, the aspect such as take photo by plane requires aircraft easy to use and control simple while using, and the operation of flying in complicated space environment, existing can vertical takeoff and landing to have both fixed wing aircraft feature complicated in the Flight Vehicle Structure of one, controls more difficult; Aircraft is generally just controlled flight during as telecontrolled aircraft model by day, and can not carry out night.
Summary of the invention
It is simple, with low cost, easy for operation that the purpose of this utility model is to provide a kind of novel ball Flight Vehicle Structure, control simple and safety, cruise duration is long, and the feature of vertical takeoff and landing and fixed wing aircraft that has both, in one, can be controlled the spherical flight instruments of flight night.The purpose of this utility model is achieved in that the vertical plane surface that it comprises four vertical direction, vertical plane surface I, vertical plane surface II, vertical plane surface III, vertical plane surface IV, horizontal plane V forms spheroid profile, it is characterized in that: motor rear is fixedly connected with motor stator, motor stator is fixed on vertical plane surface II and vertical plane surface IV intersection, motor is positioned on the axis of ball centre top, solar panel is arranged at vertical plane surface I, vertical plane surface II, vertical plane surface III, vertical plane surface IV, on the outside face of horizontal plane V, steering wheel I, steering wheel III is arranged at two side positions in vertical plane surface III, in vertical plane surface I and vertical plane surface III intersection location place, be provided with steering wheel II, on vertical plane surface I and vertical plane surface III position, be respectively equipped with rudder face I, rudder face II, rudder face III, rudder face IV.Advantage of the present utility model and good effect are simple in structure, with low cost, easy for operation, control simple and safety, and cruise duration is long, and the feature of vertical takeoff and landing and fixed wing aircraft that has both is in one; By controlling the rotating speed of rudder face and motor, realize the control of heading and flying speed; Aircraft can suspend, and can in complicated space environment, operation fly; The solar panel that aircraft adheres to by outside face large area, increases the utilization ratio to solar power, and sustainable power supply increases cruise duration; Screw propeller is positioned at the middle part of spheroid aircraft, by the outer rim protection of aircraft, can prevent that aircraft is in the situation that out of control by actv., the injury of the screw propeller of High Rotation Speed to external staff etc.; Aircraft surface, with increasable emitting led pipe, makes aircraft Integral luminous, controls control aircraft flight at night; Can be used for military surveillance, patrol, rescue, takes photo by plane, celebration activity, advertising, remote-control toy, model airplane, a plurality of fields such as scientific research.
Accompanying drawing explanation
Fig. 1 is spatial structure principle schematic of the present utility model;
Fig. 2 is that the utility model is with the spatial structure principle schematic of emitting led pipe;
Fig. 3 is birds-eye view structural principle schematic diagram of the present utility model:
Fig. 4 circuit supply of the present utility model and control principle block diagram;
Fig. 5 is control principle block diagram of the present utility model.
The specific embodiment
The vertical plane surface that it comprises four vertical direction, vertical plane surface I, vertical plane surface II, vertical plane surface III, vertical plane surface IV, horizontal plane V forms spheroid profile, it is characterized in that: motor 2 rears are fixedly connected with motor stator 3, motor stator 3 is fixed on vertical plane surface II and vertical plane surface IV intersection, motor 2 is positioned on the axis of ball centre top, solar panel 5 is arranged at vertical plane surface I, vertical plane surface II, vertical plane surface III, vertical plane surface IV, on the outside face of horizontal plane V, steering wheel I 6, steering wheel III 8 is arranged at two side positions in vertical plane surface III, in vertical plane surface I and vertical plane surface III intersection location place, be provided with steering wheel II 7, on vertical plane surface I and vertical plane surface III position, be respectively equipped with rudder face I 14, rudder face II 16, rudder face III 18, rudder face IV 23.Below in conjunction with the drawings and specific embodiments to the utility model be elaborated principle of work and working process.The vertical plane surface of four vertical direction, vertical plane surface I, vertical plane surface II, vertical plane surface III, vertical plane surface IV, horizontal plane V forms spheroid profile, screw propeller 1 is connected with motor 2, motor 2 is connected with motor stator 3, motor stator 3 is fixed on vertical plane surface II and vertical plane surface IV intersection, motor is positioned on the axis of ball centre top, rotation by motor 2 drives screw propeller 1 to rotate, screw propeller 1 rotates and will produce lift, drive the whole flight of aircraft, the control of the rotating speed by motor realizes the control of flying speed, in vertical plane surface II above motor and vertical plane surface IV, in axial location, by removal, form draw-in groove 4 for laying lithium cell 25 and receiver 26 circuit controller parts, solar panel 5 is evenly distributed on the outside face of ball-type aircraft, solar panel 5 is lithium cell 25 chargings with mode in parallel through lithium cell charging module 28 by series connection, lithium cell can be receiver 26, motor 2, steering wheel I 6, steering wheel II 7, steering wheel III 8, noctilucent emitting led pipe 24, 29 power supplies of voltage demodulator, a plurality of emitting led pipes 24 connect by connection mode in parallel, a plurality of emitting led pipes 24 are connected with lithium cell 25 when night flying is used, to make aircraft Integral luminous, steering wheel I 6 and steering wheel III 8 are placed in respectively two side positions in vertical plane surface III, single armed rudder arm I 9 and single armed rudder arm II 21 are installed in steering wheel I 6 and steering wheel III 8, in vertical plane surface I and vertical plane surface III intersection location place, lay a steering wheel II 7, both arms rudder arm 11 is installed in steering wheel II 7, on vertical plane surface I and vertical plane surface III position, be equipped with respectively four rudder faces, four rudder faces are respectively rudder face I 14, rudder face II 16, rudder face III 18, rudder face IV 23, rudder face I 14 is connected in vertical plane surface I through hinge IV 32, rudder face II 16 is connected in vertical plane surface III through hinge I 15, rudder face III 18 is connected in vertical plane surface III through hinge II 17, rudder face IV 23 is connected in vertical plane surface I through hinge III 31, on each rudder face, there is corresponding rudder angle, have four rudder angles: rudder pin I 22, rudder pin II 30, rudder pin III 33, rudder pin IV 34, rudder pin I 22 is connected with corresponding rudder face II 16 through connecting rod IV 20, rudder pin II 30 is connected with corresponding rudder face III 18 through connecting rod I 10, rudder pin III 33 is connected with corresponding rudder face I 14 through connecting rod II 12, rudder pin IV 34 is connected with corresponding rudder face IV 23 through connecting rod III 19, by steering wheel I 6, drive single armed rudder arm II 21.Steering wheel II 7 drives both arms rudder arm 11, steering wheel III 8 drives single armed rudder arm I 9, single armed rudder arm II 21 drivening rod IV 20, both arms rudder arm 11 drivening rod II 12 and connecting rod III 19, single armed rudder arm I 9 drivening rod I 10, by controlling three above-mentioned steering wheels, drive four rudder arms to move, four rudder arms drive four link works, four connecting rods drive four rudder pin motions, four rudder faces will be with four rudder angle motions, thereby by controlling the anglec of rotation of steering wheel, control rudder face rotation respective angles change air flow line, thereby realize the direction control of aircraft.Remote controller 27 is at ground emissioning controling signal, carry-on receiver 26 receives signal and adjusts 29 to control motor 2 drive screw propellers 1 rotations by electricity, by controlling the rotating speed of motor 2, realize the control of flying speed, the signal control steering wheel I 6 receiving by receiver 26, steering wheel II 7, steering wheel III 8 is rotated, thereby steering wheel rotates the direction that drives rudder face rotation to realize aircraft, controls.The utility model is by spherical main, power pack section, actuating element forms, its formation is that plane and a horizontal plane of four vertical direction forms spheroid profile, the interplanar angle of each adjacent vertical direction is 45 degree angles, the set of planes that horizontal plane is fixed on four vertical direction becomes spheroid, plays a supporting role in protection, electrical motor is positioned at spheroid inside, the flight that drives screw propeller to rotate to be aircraft by electric machine rotation provides power, screw propeller by spheroid outer rim protection High Rotation Speed, by controlling the rotating speed of motor, realize the control of flying speed, the solar panel that power resources have in power supply and the outer surface of spheroid of aircraft inside, owing to adopting multiple surface assembled to become the scheme of spheroid, spheroid is arranged solar panel at each outside face, greatly increased the absorption area to space sunlight, improved the space utilization efficiency of solar power, solar panel is aircraft battery electric power storage by the electric energy of changing, increased the time of continuation of the journey, operating system is comprised of servomechanism manipulation rudder face, rudder face is positioned at the below that machine shaft extended line is screw propeller, aircraft has four rudder faces, thereby change air flow line control aircraft flight track by controlling rudder face, by the surface at aircraft, increase luminous LED and manage, make aircraft Integral luminous, when controlling aircraft flight night, can distinguish flight controlling party to, increase the sight of flight.The model of voltage demodulator 29 is: DF04030X3, solar panel 5 is flexible amorphous silicon solar panel, receiver 26 is the R6208SB of Japanese Futaba company, remote controller 27 is the 10C2.4GHZ remote controller of Japanese Futaba company, and lithium cell charging module 28 is Aili026 charging modules.

Claims (1)

1. a spherical flight instruments, the vertical plane surface that it comprises four vertical direction, vertical plane surface I, vertical plane surface II, vertical plane surface III, vertical plane surface IV, horizontal plane V forms spheroid profile, it is characterized in that: motor rear is fixedly connected with motor stator, motor stator is fixed on vertical plane surface II and vertical plane surface IV intersection, motor is positioned on the axis of ball centre top, solar panel is arranged at vertical plane surface I, vertical plane surface II, vertical plane surface III, vertical plane surface IV, on the outside face of horizontal plane V, steering wheel I, steering wheel III is arranged at two side positions in vertical plane surface III, in vertical plane surface I and vertical plane surface III intersection location place, be provided with steering wheel II, on vertical plane surface I and vertical plane surface III position, be respectively equipped with rudder face I, rudder face II, rudder face III, rudder face IV, screw propeller is connected with motor, motor is connected with motor stator, motor stator is fixed on vertical plane surface II and vertical plane surface IV intersection, motor is positioned on the axis of ball centre top, rotation by motor drives screw propeller to rotate, screw propeller rotates will produce lift, drive the whole flight of aircraft.
CN201420219002.5U 2014-05-02 2014-05-02 Spherical flight device Expired - Fee Related CN203876983U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201420219002.5U CN203876983U (en) 2014-05-02 2014-05-02 Spherical flight device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201420219002.5U CN203876983U (en) 2014-05-02 2014-05-02 Spherical flight device

Publications (1)

Publication Number Publication Date
CN203876983U true CN203876983U (en) 2014-10-15

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CN201420219002.5U Expired - Fee Related CN203876983U (en) 2014-05-02 2014-05-02 Spherical flight device

Country Status (1)

Country Link
CN (1) CN203876983U (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104565875A (en) * 2015-01-05 2015-04-29 惠州市加迈电器有限公司 Lighting device
CN104960665A (en) * 2015-06-29 2015-10-07 田悦丰 Aircraft having multiple flight modes
CN105129088A (en) * 2015-09-25 2015-12-09 高翔宇 Spherical uniaxial rudder oriented intelligent aircraft
CN106005392A (en) * 2016-06-29 2016-10-12 汇星海科技(天津)有限公司 Spherical aerial vehicle
CN106347654A (en) * 2016-10-09 2017-01-25 南京信息工程大学 Spherical unmanned aerial vehicle
CN106467168A (en) * 2015-08-17 2017-03-01 富士通株式会社 Aircraft frame structure, aircraft, aircraft using method
US10683098B2 (en) 2015-06-29 2020-06-16 Yuefeng TIAN Driving device assembly with multiple drive devices and application thereof

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN104565875A (en) * 2015-01-05 2015-04-29 惠州市加迈电器有限公司 Lighting device
CN104565875B (en) * 2015-01-05 2018-06-08 永春锐拓信息技术中心 Lighting apparatus
US10683098B2 (en) 2015-06-29 2020-06-16 Yuefeng TIAN Driving device assembly with multiple drive devices and application thereof
CN104960665A (en) * 2015-06-29 2015-10-07 田悦丰 Aircraft having multiple flight modes
CN106467168B (en) * 2015-08-17 2019-07-09 富士通株式会社 Aircraft frame structural body, aircraft, aircraft application method
CN106467168A (en) * 2015-08-17 2017-03-01 富士通株式会社 Aircraft frame structure, aircraft, aircraft using method
CN105129088B (en) * 2015-09-25 2017-03-22 高翔宇 Spherical uniaxial rudder oriented intelligent aircraft
CN105129088A (en) * 2015-09-25 2015-12-09 高翔宇 Spherical uniaxial rudder oriented intelligent aircraft
CN106005392A (en) * 2016-06-29 2016-10-12 汇星海科技(天津)有限公司 Spherical aerial vehicle
CN106347654A (en) * 2016-10-09 2017-01-25 南京信息工程大学 Spherical unmanned aerial vehicle

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GR01 Patent grant
C14 Grant of patent or utility model
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20141015

Termination date: 20170502

CF01 Termination of patent right due to non-payment of annual fee