CN106275386A - A kind of wing, the manufacture method of wing and unmanned plane - Google Patents

A kind of wing, the manufacture method of wing and unmanned plane Download PDF

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Publication number
CN106275386A
CN106275386A CN201610802364.0A CN201610802364A CN106275386A CN 106275386 A CN106275386 A CN 106275386A CN 201610802364 A CN201610802364 A CN 201610802364A CN 106275386 A CN106275386 A CN 106275386A
Authority
CN
China
Prior art keywords
wing
battery chip
solar battery
unmanned plane
motor
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
CN201610802364.0A
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Chinese (zh)
Inventor
高鹏
王海峰
吴桂弟
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
CHENGDU INNOVATION TECHNOLOGY Co Ltd
Original Assignee
CHENGDU INNOVATION TECHNOLOGY Co Ltd
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 CHENGDU INNOVATION TECHNOLOGY Co Ltd filed Critical CHENGDU INNOVATION TECHNOLOGY Co Ltd
Priority to CN201610802364.0A priority Critical patent/CN106275386A/en
Publication of CN106275386A publication Critical patent/CN106275386A/en
Pending legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C2201/00Unmanned aerial vehicles; Equipment therefor
    • B64C2201/10Unmanned aerial vehicles; Equipment therefor characterised by the lift producing means
    • B64C2201/104Fixed wings
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D2211/00Arrangements of solar panels on aircraft

Abstract

The present invention provides a kind of wing, the manufacture method of wing and unmanned plane, wherein said wing, including wing-body, the upper face at described wing-body is provided with at least one piece of solar battery chip, and described solar battery chip installation by adhering is on described wing-body.The wing that the present invention provides, uses solar battery chip generating, adds the flying power of unmanned plane;And by the design of structure, alleviate the weight of body, extend the working flight time of unmanned plane.

Description

A kind of wing, the manufacture method of wing and unmanned plane
Technical field
The present invention relates to a kind of unmanned air vehicle technique field, particularly relate to a kind of wing, the manufacture method of wing and unmanned Machine.
Background technology
The wing of middle-size and small-size unmanned plane the most on the market substantially uses common conventional plastic cement material, such as ABS Or carbon fiber, these materials be mostly density 1.0 grams more than every cubic centimetre, make the own weight of wing made inclined Weight, causes the power required for unmanned plane bigger, and with present battery technology limitation, finally makes the flying power of unmanned plane It is substantially reduced (flying power is mostly at 10-30 minute), reduces the practicality of product, along with the development of society, unmanned plane Wide model uses, and the mankind are more and more higher to the requirement of unmanned plane flying power, in the case of battery capacity determines, and continuing of unmanned plane Boat ability also determines that.
In prior art, CN201520729220.8 discloses a kind of unmanned plane using new forms of energy power, by multiple too Sun energy cell panel is arranged on the upper surface of unmanned plane shell, wing and empennage.Due to solar panel itself structure and Material characteristics, solar panel, during combining with unmanned plane (particularly wing), at least there is problems in that
(1) casing is protruding cambered surface, and solar panel is generally plane, so common solar panel is very The difficult cambered surface for casing;
(2) wing entirety uses solar panel, it is clear that can increase the weight of solar panel, and wing itself As be irregularly shaped, also make solar panel need cutting and apply when and the complete contract of shape of wing Close.
Summary of the invention
In view of this, the present invention provides a kind of wing, the manufacture method of wing and unmanned plane, increases unmanned plane continuation of the journey energy Power.
For reaching above-mentioned purpose, present invention generally provides following technical scheme:
On the one hand, the present invention provides a kind of wing, including wing-body, the upper face at described wing-body be provided with to Few one piece of solar battery chip, described solar battery chip installation by adhering is on described wing-body.
Preferably, described wing-body uses PU or EVA foam to make.
Preferably, described solar battery chip is combined on described wing-body by the way of heating is pressurizeed.
Preferably, the upper face of described solar battery chip is non-bulging in the upper face of described wing-body.
Preferably, the upper face at described solar battery chip is coated with layer protecting film.
Preferably, described protecting film is formed by spray epoxy at the upper face of described solar battery chip.
Preferably, the upper face of described wing-body is triangle.
Preferably, described solar battery chip includes being spaced between two or more, and described solar battery chip Arrangement, is connected by series system between the electrode of described solar battery chip.
On the other hand, the present invention also provides for the manufacture method of a kind of wing, including:
Solar battery chip is combined on wing-body by heating pressing technology.
Preferably, also include, at the upper face spray epoxy of described solar battery chip.
Another further aspect, the present invention also provides for a kind of unmanned plane, and including wing, described wing uses above-described wing.
Preferably, described unmanned plane also includes:
Accumulator, for providing electric energy for described unmanned plane, the electrode of described solar battery chip passes through wire and institute State accumulator to connect;
Receiver, is used for receiving control signal, and sends control signals to electron speed regulator or steering wheel;
Electron speed regulator, is used for controlling flight speed;
Steering wheel, is used for controlling heading;
Motor, is used for driving propeller.
Preferably, described steering wheel includes two, is symmetricly set on wing.
Preferably, described accumulator, receiver, electron speed regulator, motor installation by adhering are at the median plane of described wing On.
Preferably, described motor is positioned at the afterbody of described wing, and described propeller is arranged on the output shaft of described motor.
Preferably, described accumulator is lithium battery.
The wing that the present invention provides, uses solar battery chip generating, adds the flying power of unmanned plane;And lead to Cross the design of structure, alleviate the weight of body, extend the working flight time of unmanned plane.
The processing technology of wing of the present invention is simple, and cost of manufacture is low, and lightweight, workable, safety High;Utilize the generating of solar energy Infinite Cyclic, charging, pollution-free, belong to clean energy resource.
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 description, below with presently preferred embodiments of the present invention and coordinate accompanying drawing describe in detail as after.
Accompanying drawing explanation
Fig. 1 is the elevational schematic view of unmanned plane of the present invention;
Fig. 2 is the schematic side view of unmanned plane of the present invention;’
Fig. 3 is the schematic top plan view of unmanned plane of the present invention;
Fig. 4 is the schematic perspective view of unmanned plane of the present invention.
In figure:
10, wing-body;11, solar battery chip;
20, accumulator;
30, receiver;
40, electron speed regulator;
50, steering wheel;
60, motor;
70, propeller.
Detailed description of the invention
For making the object, technical solutions and advantages of the present invention clearer, below in conjunction with the specific embodiment of the invention and Technical solution of the present invention is clearly and completely described by corresponding accompanying drawing.Obviously, described embodiment is only the present invention one Section Example rather than whole embodiments.Based on the embodiment in the present invention, those of ordinary skill in the art are not doing Go out the every other embodiment obtained under creative work premise, broadly fall into the scope of protection of the invention.
As Figure 1-4, on the one hand, the present invention provides a kind of wing, including wing-body 10, at described wing-body 10 Upper face be provided with at least one piece of solar battery chip 11, described solar battery chip 11 installation by adhering is at described machine On wing body 10.
The wing that the present embodiment provides, it will pass through Embedded side between solar battery chip 11 and wing-body 10 Formula combines, and generates electricity with solar battery chip 11, adds the flying power of unmanned plane.
Preferably, described wing-body uses PU or EVA foam to make.
Owing to PU or eva foam density are low, time on the wing of unmanned plane, the weight of unmanned plane can be substantially reduced, Reduce the energy consumption of unmanned plane, thus extend the flight time of unmanned plane.
Preferably, described solar battery chip is combined on described wing-body by the way of heating is pressurizeed.
Using the mode of heating pressurization, make solar battery chip be combined with wing-body, not only technique is simple, Er Qieke So that wing-body is more firm with the combination of solar battery chip, reduce the destruction to wing-body structural behaviour.
Preferably, the upper face of described solar battery chip 11 is non-bulging in the top table of described wing-body 10 Face, thus keep the surface conformance of described wing-body 10, meet aerodynamic structures design, make the mistake of unmanned plane during flying Cheng Zhong, described wing-body 10 has better aerodynamic performance.
Preferably, the upper face at described solar battery chip is coated with layer protecting film, and described protecting film can The surface of solar battery chip is played a protective role so that it is be difficult to aging, extend the use of described solar battery chip Life-span.
Preferably, described protecting film is formed by spray epoxy at the upper face of described solar battery chip. By the way of even application epoxy resin, the surface of described solar battery chip can be made to form uniform protecting film, and And epoxy resin density also complies with requirement, can effectively control the weight of wing.
Preferably, the upper face of described wing-body is triangle.Described wing-body is typically designed to symmetrical Structure, so the upper face of wing-body is also typically designed to isosceles triangle.
Preferably, described solar battery chip includes being spaced between two or more, and described solar battery chip Arrangement, is connected by series system between the electrode of described solar battery chip.Use spaced layout type, permissible Making to retain certain space between solar battery chip, this portion void wing-body 10 is filled, and can make solar energy Battery chip is more firm, stable.
On the other hand, the present invention also provides for the manufacture method of a kind of wing, including:
Solar battery chip is combined on wing-body by heating pressing technology.
Preferably, also include, at the upper face spray epoxy of described solar battery chip.
The manufacture method of wing of the present invention, technique is simple, and cost of manufacture is low, and lightweight, workable, peace Quan Xinggao;Utilize the generating of solar energy Infinite Cyclic, charging, pollution-free, belong to clean energy resource.
As Figure 1-4, another further aspect, the present invention also provides for a kind of unmanned plane, including wing, more than the use of described wing Described wing.
Preferably, described unmanned plane also includes:
Accumulator 20, for for described unmanned plane provide electric energy, the electrode of described solar battery chip by wire with Described accumulator connects;
Receiver 30, is used for receiving control signal, and sends control signals to electron speed regulator or steering wheel;
Electron speed regulator 40, is used for controlling flight speed;
Steering wheel 50, is used for controlling heading;
Motor 60, is used for driving propeller 70.
Preferably, described steering wheel 50 includes two, is symmetricly set on wing.Coordinated by two steering wheels, it is achieved to nothing The control of man-machine heading.
Preferably, described accumulator 20, receiver 30, electron speed regulator 40, motor 60 installation by adhering are at described wing Median plane on.Said structure is arranged on the median plane of described wing, it is ensured that the center of gravity of whole unmanned plane is positioned at wing On median plane.
Preferably, described motor 60 is positioned at the afterbody of described wing, and described propeller 70 is arranged on the output of described motor On axle.Propeller 70 is arranged on the afterbody of wing, it is achieved the forerunner that mostly uses in the rear-guard of unmanned plane, with prior art or on The type of drive that portion drives is different, can preferably manipulate the flight attitude of whole unmanned plane.
Preferably, described accumulator 20 is lithium battery.
The wing that the present invention provides, uses solar battery chip generating, adds the flying power of unmanned plane;And lead to Cross the design of structure, alleviate the weight of body, extend the working flight time of unmanned plane.
The processing technology of wing of the present invention is simple, and cost of manufacture is low, and lightweight, workable, safety High;Utilize the generating of solar energy Infinite Cyclic, charging, pollution-free, belong to clean energy resource.
In sum, skilled addressee readily understands that, on the premise of not conflicting, above-mentioned each advantageous manner can Freely to combine, superposition.
The above, be only presently preferred embodiments of the present invention, the present invention not makees any pro forma restriction, depends on Any simple modification, equivalent variations and the modification made above example according to the technical spirit of the present invention, all still falls within this In the range of bright technical scheme.

Claims (10)

1. a wing, including wing-body, it is characterised in that the upper face at described wing-body is provided with at least one piece too Sun energy battery chip, described solar battery chip installation by adhering is on described wing-body;Preferably, described wing-body PU or EVA foam is used to make.
2. wing as claimed in claim 1, it is characterised in that:
Described solar battery chip is combined on described wing-body by the way of heating is pressurizeed;Preferably, the described sun The upper face of energy battery chip is non-bulging in the upper face of described wing-body.
3. wing as claimed in claim 1 or 2, it is characterised in that:
Upper face at described solar battery chip is coated with layer protecting film;Preferably, existed by spray epoxy The upper face of described solar battery chip forms described protecting film.
4. the wing as described in one of claim 1-3, it is characterised in that:
The upper face of described wing-body is triangle.
5. the wing as described in one of claim 1-7, it is characterised in that:
Described solar battery chip includes being spaced between two or more, and described solar battery chip, described too Sun can be connected by series system between the electrode of battery chip.
6. a manufacture method for wing, including:
Solar battery chip is combined on wing-body by heating pressing technology.
7. method as claimed in claim 6, it is characterised in that:
Also include, at the upper face spray epoxy of described solar battery chip.
8. a unmanned plane, including wing, it is characterised in that: described wing uses the wing that one of claim 1-5 is described.
9. unmanned plane as claimed in claim 8, it is characterised in that: described unmanned plane also includes:
Accumulator, for providing electric energy for described unmanned plane, the electrode of described solar battery chip is by wire and described storage Battery connects;
Receiver, is used for receiving control signal, and sends control signals to electron speed regulator or steering wheel;
Electron speed regulator, is used for controlling flight speed;
Steering wheel, is used for controlling heading;
Motor, is used for driving propeller.
10. unmanned plane as claimed in claim 9, it is characterised in that:
Described steering wheel includes two, is symmetricly set on wing;
And/or, described accumulator, receiver, electron speed regulator, motor installation by adhering are on the median plane of described wing;
And/or, described motor is positioned at the afterbody of described wing, and described propeller is arranged on the output shaft of described motor.
CN201610802364.0A 2016-09-05 2016-09-05 A kind of wing, the manufacture method of wing and unmanned plane Pending CN106275386A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201610802364.0A CN106275386A (en) 2016-09-05 2016-09-05 A kind of wing, the manufacture method of wing and unmanned plane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201610802364.0A CN106275386A (en) 2016-09-05 2016-09-05 A kind of wing, the manufacture method of wing and unmanned plane

Publications (1)

Publication Number Publication Date
CN106275386A true CN106275386A (en) 2017-01-04

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Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009036465A1 (en) * 2007-09-14 2009-03-19 Aurora Flight Sciences Corporation Non-planar adaptive wing solar aircraft
CN101665153A (en) * 2009-09-24 2010-03-10 南昌航空大学 Plane wing with solar battery
CN204802071U (en) * 2015-07-03 2015-11-25 苏州峰通光电有限公司 Helios
CN105398561A (en) * 2015-11-12 2016-03-16 中国人民解放军国防科学技术大学 Solar aircraft
CN205150216U (en) * 2015-11-24 2016-04-13 中国航天时代电子公司 Unmanned aerial vehicle's foam presss from both sides core wing
CN205971806U (en) * 2016-09-05 2017-02-22 锋源创新科技成都有限公司 Wing and unmanned aerial vehicle

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009036465A1 (en) * 2007-09-14 2009-03-19 Aurora Flight Sciences Corporation Non-planar adaptive wing solar aircraft
CN101665153A (en) * 2009-09-24 2010-03-10 南昌航空大学 Plane wing with solar battery
CN204802071U (en) * 2015-07-03 2015-11-25 苏州峰通光电有限公司 Helios
CN105398561A (en) * 2015-11-12 2016-03-16 中国人民解放军国防科学技术大学 Solar aircraft
CN205150216U (en) * 2015-11-24 2016-04-13 中国航天时代电子公司 Unmanned aerial vehicle's foam presss from both sides core wing
CN205971806U (en) * 2016-09-05 2017-02-22 锋源创新科技成都有限公司 Wing and unmanned aerial vehicle

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Application publication date: 20170104