CN204660029U - A kind of unmanned plane - Google Patents

A kind of unmanned plane Download PDF

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Publication number
CN204660029U
CN204660029U CN201520336868.9U CN201520336868U CN204660029U CN 204660029 U CN204660029 U CN 204660029U CN 201520336868 U CN201520336868 U CN 201520336868U CN 204660029 U CN204660029 U CN 204660029U
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China
Prior art keywords
power
wing
solar battery
unmanned plane
chip
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CN201520336868.9U
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Chinese (zh)
Inventor
赵奇
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Beijing Huihong Technology Co., Ltd
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Beijing Hanergy Solar Power Investment Co Ltd
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Priority to CN201520336868.9U priority Critical patent/CN204660029U/en
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    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft

Abstract

The utility model discloses a kind of unmanned plane, it power system comprising fuselage, be positioned at the wing of fuselage both sides, power is provided for wing, and by storage battery that controller is electrically connected with power system; Also comprise the first power system and the second power system; First power system comprises and is arranged at first solar battery chip of wing towards a side surface of light source, and the first solar battery chip is electrically connected with controller, and controller is connected with described storage battery; Described second power system comprises some wind wheels of the end being arranged at wing, and described wind wheel is connected with generator drive gear, and described electrical generator is electrically connected with described controller.Like this, unmanned plane provided by the utility model can utilize solar power and wind energy to obtain power, thus simplifies housing construction, reduces body weight, and then reduces its flight resistance, improves flying power; Meanwhile, the utilization of clean energy resource, also reduces energy consumption, decreases noise, improves its environmental-protecting performance.

Description

A kind of unmanned plane
Technical field
The utility model relates to vehicle technology field, particularly relates to a kind of unmanned plane based on clean energy resource energy supply.
Background technology
Along with the fast development of science and technology, robot airplane (abbreviation unmanned plane), with its maneuverability, reaction fast, the advantage such as unmanned flight, operation requirements be low, be applied to military affairs, scientific research, the field such as civilian more and more widely, unmanned plane is by carrying multiclass sensor, image real-time Transmission, high-risk areas detecting function can be realized, especially in electric power, communication, meteorology, agricultural, ocean, exploration, photograph, prevent and reduce natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the having a extensive future of the field such as public security anti-terrorism.
Unmanned plane mainly comprises fuselage, power system and for adapting to different field and the function device (equipment etc. of such as taking photo by plane) that carries, current unmanned plane uses storage battery and fuel to provide navigating power for it mostly, this just needs on unmanned plane, arrange the parts such as driving engine, transmission system, make the structure of unmanned plane comparatively complicated, and add body weight, cause body flight resistance to increase, and limit its flying power, constrain the Applicable scope of unmanned plane; Meanwhile, adopt the mode of fuel energy supply to consume energy higher, noise emission is comparatively serious, cannot reach environmental-protecting performance requirement.
Therefore, provide a kind of unmanned plane, to simplifying housing construction, reducing body weight, thus reduce its flight resistance, improve its flying power, reduce energy consumption simultaneously, reduce noise, improving its environmental-protecting performance, needing the problem of solution with regard to becoming those skilled in the art badly.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane, to simplifying housing construction, reducing body weight, thus reduces its flight resistance, improves its flying power, reduce energy consumption simultaneously, reduce noise, improve its environmental-protecting performance.
To achieve these goals, the utility model provides a kind of unmanned plane, comprise fuselage, be positioned at the wing of described fuselage both sides, provide the power system of power for described wing, with the storage battery be electrically connected with described power system by controller, also comprise the first power system and the second power system; Described first power system comprises and is arranged at first solar battery chip of described wing towards a side surface of light source, and described first solar battery chip is electrically connected with controller, and described controller is connected with described storage battery; Described second power system comprises some wind wheels of the end being arranged at described wing, and described wind wheel is connected with generator drive gear, and described electrical generator is electrically connected with described controller.
Preferably, described first solar battery chip is flexible chip, and fits fixing with the upper surface of described wing.
Preferably, described first solar battery chip is flexible thin-film battery.
Preferably, described first solar battery chip and described wing are integrated encapsulating structure.
Preferably, described first solar battery chip covers the upper surface of described wing.
Preferably, described first power system also comprises the second solar battery chip, and described second solar battery chip is layed on described fuselage, and described second solar battery chip is electrically connected with described controller.
Preferably, described second solar battery chip is flexible chip, and fits fixing with the upper surface of described fuselage.
Preferably, described second solar battery chip is flexible thin-film battery.
Preferably, described second solar battery chip and described fuselage are integrated encapsulating structure.
Preferably, described second solar battery chip covers the upper surface of described fuselage.
Unmanned plane provided by the utility model comprises fuselage, is positioned at the wing of described fuselage both sides, provide the power system of power for described wing, and by storage battery that controller is electrically connected with described power system; Also comprise the first power system and the second power system; Described first power system comprises and is arranged at first solar battery chip of described wing towards a side surface of light source, and described first solar battery chip is electrically connected with controller, and described controller is connected with described storage battery; Described second power system comprises some wind wheels of the end being arranged at described wing, and described wind wheel is connected with generator drive gear, and described electrical generator is electrically connected with described controller.
In flight course, the solar power absorbed is changed into electric energy and flows to controller by the first solar battery chip be arranged on wing, simultaneously, the wind wheel that wing is arranged rotates with the wind, and flow to controller after wind energy is changed into electric energy by electrical generator, controller by the wind-power electricity generation electric energy that receives and solar electrical energy generation delivery of electrical energy to storage battery, charge a battery, again by after controller constant current constant voltage during battery discharging, by power delivery to power system, for the motion of wing provides power; Like this, unmanned plane provided by the utility model can utilize solar power and wind energy to obtain power, thus simplifies housing construction, reduces body weight, and then reduces its flight resistance, improves flying power; Meanwhile, the utilization of clean energy resource, also reduces energy consumption, decreases noise, improves its environmental-protecting performance.
In a preferred embodiment, in unmanned plane provided by the utility model, its first solar battery chip is flexible chip, and fits fixing with the upper surface of described wing; Like this, the battery chip of flexible material and the stickiness of wing better, are convenient to be connected and fixed, and elasticity is better, and can avoid the stiffness cracks with occurring during wing motion, safety performance is higher; Meanwhile, the thinner thickness of flexible material chip, lighter in weight, can reduce body weight further, thus reduce flight resistance further, improves flying power.
In another preferred embodiment, in unmanned plane provided by the utility model, its first solar battery chip and wing are integrated encapsulating structure, to improve the connection reliability of the first solar battery chip and wing.
Accompanying drawing explanation
In order to be illustrated more clearly in the embodiment of the present application or technical scheme of the prior art, be briefly described to the accompanying drawing used required in embodiment below, apparently, the accompanying drawing that the following describes is only some embodiments recorded in the utility model, for those of ordinary skill in the art, other accompanying drawing can also be obtained according to these accompanying drawings.
Fig. 1 is the system schematic of unmanned plane provided by the utility model;
Fig. 2 is the part-structure schematic diagram of unmanned plane provided by the utility model.
Description of reference numerals:
1-fuselage 2-wing 3-storage battery 4-first solar battery chip 5-controller 6-wind wheel 7-electrical generator 8-second solar battery chip 9-power system
Detailed description of the invention
Core of the present utility model is to provide a kind of unmanned plane, to simplifying housing construction, reducing body weight, thus reduces its flight resistance, improves its flying power, reduce energy consumption simultaneously, reduce noise, improve its environmental-protecting performance.
In order to make those skilled in the art understand the technical solution of the utility model better, below in conjunction with accompanying drawing, the utility model is further detailed.
Please refer to Fig. 1 and Fig. 2, Fig. 1 is the system schematic of unmanned plane provided by the utility model; Fig. 2 is the part-structure schematic diagram of unmanned plane provided by the utility model.
In a kind of detailed description of the invention, unmanned plane provided by the utility model comprises fuselage 1, is positioned at the wing 2 of described fuselage 1 both sides, provide the power system 9 of power for described wing 2, and by storage battery 3 that controller 5 is electrically connected with described power system 9; Also comprise the first power system and the second power system; Described first power system comprises and is arranged at first solar battery chip 4 of described wing 2 towards a side surface of light source, and described first solar battery chip 4 is electrically connected with controller 5, and described controller 5 is electrically connected with described storage battery 3; Described second power system comprises some wind wheels 6 of the end being arranged at described wing 2, and described wind wheel 6 is in transmission connection with electrical generator 7, and described electrical generator 7 is electrically connected with described controller 5.
Above-mentioned first solar battery chip 4 is preferably flexible chip, and fits fixing with the upper surface of described wing 2; Like this, the battery chip of flexible material and the stickiness of wing better, are convenient to be connected and fixed, and elasticity is better, the stiffness cracks occurred when can avoid moving with wing 2, and safety performance is higher; Meanwhile, the thinner thickness of flexible material chip, lighter in weight, can reduce body weight further, thus reduce flight resistance further, improves flying power.
Particularly, the first solar battery chip 4 can be flexible thin-film battery, such as CIGS hull cell, or the chip of the flexible material such as GaAs hull cell.
From theory, first solar battery chip 4 is also not limited to flexible chip, its version also can spliced mutually with flexible chip for rigid chips or rigid chips, such as, when moving, flexible chip can be set stressed larger part, and rigid chips is set at stressed smaller part.
Further, the first solar battery chip 4 is integrated encapsulating structure with wing 2, to improve the connection reliability of the first solar battery chip 4 and wing.Apparently, the first solar battery chip 4 be also not limited to by encapsulation form and wing one-body molded, as long as can be fixed on wing by the first solar battery chip 4, such as, the first solar battery chip 4 also can be adhered on wing.
In order to improve the area coverage of solar panel, improve solar powered ability, the first solar battery chip 4 preferably covers the upper surface of whole wing 2.Should be understood that, the layout of the first solar battery chip 4 also can be other forms, such as part covers the upper surface of wing 2, or the various ways such as the upper surface of wing 2 are covered in striped stride, its concrete position and overlay capacity should require to determine according to the power supply capacity of reality, do not limit at this.
In flight course, the solar power absorbed is changed into electric energy and flows to controller 5 by the first solar battery chip 4 be arranged on wing 2, simultaneously, the wind wheel 6 that wing 2 is arranged rotates with the wind, and flow to controller 5 after wind energy is changed into electric energy by electrical generator 7, controller 5 by the wind-power electricity generation electric energy that receives and solar electrical energy generation delivery of electrical energy to storage battery 3, accumulators 3 charges, when storage battery 3 discharges, pass through controller 5 again by power delivery to power system 9, for the motion of wing 2 provides power; Like this, unmanned plane provided by the utility model can utilize solar power and wind energy to obtain power, thus simplifies housing construction, reduces body weight, and then reduces its flight resistance, improves flying power; Meanwhile, the utilization of clean energy resource, also reduces energy consumption, decreases noise, improves its environmental-protecting performance.
Further, in order to improve power supply capacity, extend course continuation mileage, the second solar battery chip 8 can also be equipped with on the fuselage 1, described second solar battery chip 8 is electrically connected with controller 5, in flight course, the solar power absorbed is changed into electric energy and flows to controller 5 by the second solar battery chip 8.
Second solar battery chip 8 is preferably flexible chip equally, and fits fixing with described fuselage 1; The battery chip of flexible material and the stickiness of fuselage better, are convenient to be connected and fixed, and elasticity is better, and can avoid stiffness cracks occurs, safety performance is higher; Meanwhile, the thinner thickness of flexible material chip, lighter in weight, can reduce body weight further, thus reduce flight resistance further, improves flying power.
Particularly, the second solar battery chip 8 can be flexible thin-film battery, such as CIGS hull cell, or the chip of the flexible material such as GaAs hull cell.From theory, the second solar battery chip 8 is also not limited to flexible chip, its version also can spliced mutually with flexible chip for rigid chips or rigid chips.
For improving the connection reliability of the second solar battery chip 8 and fuselage, the second solar battery chip 8 can be integrated encapsulating structure with described fuselage 1.Apparently, both also can be fixedly connected with by bonding form.
Second solar battery chip 8 preferably covers the upper surface of whole fuselage 1, to improve the area coverage of solar panel, improves solar powered ability.Should be understood that, the layout of the second solar battery chip 8 also can be other forms, such as part covers the upper surface of fuselage 1, or the various ways such as the upper surface of fuselage 1 are covered in striped stride, its concrete position and overlay capacity should require to determine according to the power supply capacity of reality, do not limit at this.
It is pointed out that ordinal numbers such as " first, second " described in literary composition, is the different structure in order to distinguish same names, only for convenience, does not represent certain order, more should not be construed as any restriction.
Mode above only by illustrating describes some one exemplary embodiment of the present utility model, undoubtedly, for those of ordinary skill in the art, when not departing from spirit and scope of the present utility model, can revise described embodiment by various different mode.Therefore, above-mentioned accompanying drawing is illustrative with being described in essence, should not be construed as the restriction to the utility model claims.

Claims (10)

1. a unmanned plane, the power system (9) comprising fuselage (1), be positioned at the wing (2) of described fuselage (1) both sides, power is provided for described wing (2), and the storage battery (3) be electrically connected with described power system (9) by controller (5); It is characterized in that, also comprise the first power system and the second power system; Described first power system comprises and is arranged at first solar battery chip (4) of described wing (2) towards a side surface of light source, described first solar battery chip (4) is electrically connected with described controller (5), and described controller (5) is electrically connected with described storage battery (3); Described second power system comprises some wind wheels (6) of the end being arranged at described wing (2), described wind wheel (6) and electrical generator (7) are in transmission connection, and described electrical generator (7) is electrically connected with described controller (5).
2. unmanned plane according to claim 1, is characterized in that, described first solar battery chip (4) is flexible chip, and fits fixing with the upper surface of described wing (2).
3. unmanned plane according to claim 2, is characterized in that, described first solar battery chip (4) is flexible thin-film battery.
4. unmanned plane according to claim 3, is characterized in that, described first solar battery chip (4) and described wing (2) are integrated encapsulating structure.
5. unmanned plane according to claim 4, is characterized in that, described first solar battery chip (4) covers the upper surface of described wing (2).
6. the unmanned plane according to any one of claim 1 to 5, it is characterized in that, described first power system also comprises the second solar battery chip (8), described second solar battery chip (8) is layed on described fuselage (1), and described second solar battery chip (8) is electrically connected with described controller (5).
7. unmanned plane according to claim 6, is characterized in that, described second solar battery chip (8) is flexible chip, and fits fixing with the upper surface of described fuselage (1).
8. unmanned plane according to claim 7, is characterized in that, described second solar battery chip (8) is flexible thin-film battery.
9. unmanned plane according to claim 8, is characterized in that, described second solar battery chip (8) and described fuselage (1) are integrated encapsulating structure.
10. unmanned plane according to claim 9, is characterized in that, described second solar battery chip (8) covers the upper surface of described fuselage (1).
CN201520336868.9U 2015-05-22 2015-05-22 A kind of unmanned plane Active CN204660029U (en)

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105872413A (en) * 2016-05-31 2016-08-17 成都德善能科技有限公司 Intelligent aerial photographing system
CN106143919A (en) * 2016-07-14 2016-11-23 安徽状元郎电子科技有限公司 A kind of flight formula power driven mist blower
CN106364679A (en) * 2016-10-20 2017-02-01 云南电网有限责任公司电力科学研究院 Unmanned aerial vehicle control system provided with wind energy storage device, energy storage controller and control method
CN107253528A (en) * 2017-06-21 2017-10-17 深圳市雷凌广通技术研发有限公司 A kind of unmanned plane with function of energy reclaiming

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105872413A (en) * 2016-05-31 2016-08-17 成都德善能科技有限公司 Intelligent aerial photographing system
CN106143919A (en) * 2016-07-14 2016-11-23 安徽状元郎电子科技有限公司 A kind of flight formula power driven mist blower
CN106364679A (en) * 2016-10-20 2017-02-01 云南电网有限责任公司电力科学研究院 Unmanned aerial vehicle control system provided with wind energy storage device, energy storage controller and control method
CN107253528A (en) * 2017-06-21 2017-10-17 深圳市雷凌广通技术研发有限公司 A kind of unmanned plane with function of energy reclaiming

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C14 Grant of patent or utility model
GR01 Patent grant
C41 Transfer of patent application or patent right or utility model
TR01 Transfer of patent right

Effective date of registration: 20160204

Address after: 100176 Beijing economic and Technological Development Zone, Kangding street, No. 11, building three, floor 11

Patentee after: APOLLO PREC KUNMING YUANHONG LTD

Address before: 100101 Beijing city Huairou area yangsongzhen Fengxiang East Street, No. 5

Patentee before: Beijing Han Neng photovoltaic Investment Co., Ltd

Effective date of registration: 20160204

Address after: 100176 Beijing economic and Technological Development Zone, Kangding street, No. 11, building three, floor 11

Patentee after: APOLLO PREC KUNMING YUANHONG LTD

Address before: 100101 Beijing city Huairou area yangsongzhen Fengxiang East Street, No. 5

Patentee before: Beijing Han Neng photovoltaic Investment Co., Ltd

TR01 Transfer of patent right
TR01 Transfer of patent right

Effective date of registration: 20201221

Address after: 101400 Yanqi Street, Yanqi Economic Development Zone, Huairou District, Beijing

Patentee after: Beijing Huihong Technology Co., Ltd

Address before: 100176 3rd floor, 11 Kangding Street, Beijing Economic and Technological Development Zone

Patentee before: BEIJING APOLLO DING RONG SOLAR TECHNOLOGY Co.,Ltd.