CN101665153A - Plane wing with solar battery - Google Patents

Plane wing with solar battery Download PDF

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Publication number
CN101665153A
CN101665153A CN200910186097A CN200910186097A CN101665153A CN 101665153 A CN101665153 A CN 101665153A CN 200910186097 A CN200910186097 A CN 200910186097A CN 200910186097 A CN200910186097 A CN 200910186097A CN 101665153 A CN101665153 A CN 101665153A
Authority
CN
China
Prior art keywords
solar battery
plane
aircraft wing
wing
solar
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
CN200910186097A
Other languages
Chinese (zh)
Inventor
王庆
何兴道
朱泉水
蒋阳
庄淡盛
刘军
应俊永
杨芳
刘云龙
陈晓鹏
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.)
Nanchang Hangkong University
Original Assignee
Nanchang Hangkong University
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 Nanchang Hangkong University filed Critical Nanchang Hangkong University
Priority to CN200910186097A priority Critical patent/CN101665153A/en
Publication of CN101665153A publication Critical patent/CN101665153A/en
Pending legal-status Critical Current

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Abstract

A plane wing with a solar battery is characterized in that a solar battery piece is cut into multiple small pieces with different specifications based on the bending plane demand of the plane wing; the cut solar battery pieces are uniformly covered on the surface of the plane wing based on the change of curvature; the solar battery pieces are connected in series and in parallel through welding rods to form a solar battery pole; a layer of reflection-reducing membrane is covered on the solar battery plate; the reflecting membrane is connected with a protective membrane; and the protective membrane is consistent with the bending plane of the plane wing. The plane wing has the following advantages: the solar battery plate supplies power to the plane so as to achieve the application of the solar battery plate on the wing with the bending plane; and the plane wing has simple structure, reduces the oil amount of the plane and improves the flying distance of the plane.

Description

The aircraft wing of band solar cell
Technical field
The present invention relates to a kind of aircraft wing, relate in particular to a kind of aircraft wing with solar cell.
Background technology
Enter 21 century, along with the continuous development of heliotechnics, the solar power article are also more and more nearer from ordinary people life, and common have solar water heater, solar calculator, solar energy lamp or the like.Solar power has applied in each different industries; the universal better energy savings of solar power; the protection environment; realize sustainable development; but because the restriction of existing heliotechnics; the shape of silicon solar cell plate can only be plate shaped at present; therefore solar panel can only be used on the smooth object; so just limited the utilization of solar panel on many curved face objects; aircraft wing for example, aircraft mostly is to adopt conventional fossil fuel as power source now, so needs to load a large amount of fuel on the aircraft; increase aircraft weight, reduce planeload and aircraft flight time.
Summary of the invention
The object of the present invention is to provide a kind of aircraft wing with solar cell, because the aircraft wing area is big, can carry large-area curved solar energy battery, and (most of the time is in stratosphere flight in high-altitude flight for aircraft, therefore) good solar irradiation is arranged, improve curved solar energy battery electrogenesis efficient greatly.
The present invention is achieved like this, it comprise aircraft wing, too can battery sheet, it is characterized in that solar battery sheet requires to cut into the small pieces of some different sizes according to the curved surface of aircraft wing, some solar battery sheets after the cutting evenly cover the aircraft wing surface by curvature change, be connected to form solar panel by the welding rod connection in series-parallel between the solar battery sheet, cover one deck antireflection coating on the solar panel, antireflection coating is consistent with the aircraft wing curved surface.
The some solar battery sheets after the cutting of the present invention and the connection mode of aircraft wing are for embedding in the aircraft wing or adopting epoxy resin glue to paste.
Advantage of the present invention is: utilizes solar panel to give aviation power supply, realized the utilization of solar panel on the curved surface wing, and simple in structure, reduce the aircraft oil capacity, improve the aircraft flight distance.
Description of drawings
Fig. 1 is the structural representation of invention.
In the drawings, 1, aircraft wing 2, too can the battery sheet
The specific embodiment
As shown in Figure 1, the present invention is achieved like this, it comprise aircraft wing 1, too can battery sheet 2, it is characterized in that solar battery sheet 2 requires to cut into the small pieces of some different sizes according to the curved surface of aircraft wing 1, solar battery sheet 2 after the cutting of some backs evenly covers aircraft wing 1 surface by curvature change, be connected to form solar panel by the welding rod connection in series-parallel between the solar battery sheet 2, cover one deck antireflection coating on the solar panel, antireflection coating is consistent with aircraft wing 1 curved surface.

Claims (2)

1, a kind of aircraft wing with solar cell, it comprise aircraft wing, too can battery sheet, it is characterized in that solar battery sheet requires to cut into the small pieces of some different sizes according to the curved surface of aircraft wing, some solar battery sheets after the cutting evenly cover the aircraft wing surface by curvature change, be connected to form solar panel by the welding rod connection in series-parallel between the solar battery sheet, cover one deck antireflection coating on the solar panel, antireflection coating is consistent with the aircraft wing curved surface.
2, the aircraft wing of band solar cell according to claim 1, the connection mode that it is characterized in that some solar battery sheets after the described cutting and aircraft wing is for embedding in the aircraft wing or adopting epoxy resin glue to paste.
CN200910186097A 2009-09-24 2009-09-24 Plane wing with solar battery Pending CN101665153A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN200910186097A CN101665153A (en) 2009-09-24 2009-09-24 Plane wing with solar battery

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN200910186097A CN101665153A (en) 2009-09-24 2009-09-24 Plane wing with solar battery

Publications (1)

Publication Number Publication Date
CN101665153A true CN101665153A (en) 2010-03-10

Family

ID=41801972

Family Applications (1)

Application Number Title Priority Date Filing Date
CN200910186097A Pending CN101665153A (en) 2009-09-24 2009-09-24 Plane wing with solar battery

Country Status (1)

Country Link
CN (1) CN101665153A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102381482A (en) * 2011-08-16 2012-03-21 南昌航空大学 Solar aerially-photographing plane
CN102424107A (en) * 2011-09-29 2012-04-25 北京航空航天大学 Manufacture method of solar airplane
CN104377803A (en) * 2014-11-29 2015-02-25 江西洪都航空工业集团有限责任公司 Solar photovoltaic energy combination device for plane power supplying
CN106143864A (en) * 2015-03-31 2016-11-23 东莞前沿技术研究院 Capsule leather material and its preparation method and aerostatics
CN106143865A (en) * 2015-03-31 2016-11-23 东莞前沿技术研究院 Capsule skin and its preparation method and aerostatics
CN106275386A (en) * 2016-09-05 2017-01-04 锋源创新科技成都有限公司 A kind of wing, the manufacture method of wing and unmanned plane
CN106379516A (en) * 2016-09-14 2017-02-08 中国电子科技集团公司第四十八研究所 Solar-powered airplane wing and manufacturing method thereof
CN106585956A (en) * 2016-11-03 2017-04-26 上海空间电源研究所 Integrated shaping method and structure for thin silicon solar cell module of large-size wing

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102381482A (en) * 2011-08-16 2012-03-21 南昌航空大学 Solar aerially-photographing plane
CN102424107A (en) * 2011-09-29 2012-04-25 北京航空航天大学 Manufacture method of solar airplane
CN102424107B (en) * 2011-09-29 2013-11-27 北京航空航天大学 Manufacture method of solar airplane
CN104377803A (en) * 2014-11-29 2015-02-25 江西洪都航空工业集团有限责任公司 Solar photovoltaic energy combination device for plane power supplying
CN104377803B (en) * 2014-11-29 2016-07-06 江西洪都航空工业集团有限责任公司 A kind of photovoltaic energy combination unit for aviation power supply
CN106143865A (en) * 2015-03-31 2016-11-23 东莞前沿技术研究院 Capsule skin and its preparation method and aerostatics
CN106143864A (en) * 2015-03-31 2016-11-23 东莞前沿技术研究院 Capsule leather material and its preparation method and aerostatics
CN106143865B (en) * 2015-03-31 2018-05-22 东莞前沿技术研究院 Capsule skin and its production method and aerostatics
CN106143864B (en) * 2015-03-31 2018-05-22 东莞前沿技术研究院 Capsule skin material and its production method and aerostatics
CN106275386A (en) * 2016-09-05 2017-01-04 锋源创新科技成都有限公司 A kind of wing, the manufacture method of wing and unmanned plane
CN106379516A (en) * 2016-09-14 2017-02-08 中国电子科技集团公司第四十八研究所 Solar-powered airplane wing and manufacturing method thereof
CN106585956A (en) * 2016-11-03 2017-04-26 上海空间电源研究所 Integrated shaping method and structure for thin silicon solar cell module of large-size wing
CN106585956B (en) * 2016-11-03 2019-04-12 上海空间电源研究所 The thin silicon solar module integration shaping method and structure of large scale wing

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Open date: 20100310

C02 Deemed withdrawal of patent application after publication (patent law 2001)