Rigid-flexible integrated solar cell considering heat insulation and development method thereof

A technology of solar cells and solar cells, which is applied in circuits, photovoltaic power generation, electrical components, etc., can solve the problems of limiting the use of airborne equipment, failure to effectively solve, small temperature difference between the surface and the back of solar cells, and achieve effective combination Problems, good working temperature environment, and the effect of meeting battery conversion efficiency

Inactive Publication Date: 2016-02-24
BEIHANG UNIV
View PDF7 Cites 9 Cited by
  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

For the application of high-efficiency solar cell arrays, rigid solar cells are currently the first to be used. The main applications are gallium arsenide solar cells and monocrystalline silicon solar cells. , the problem of rational combination of rigid battery array plane and airfoil surface has not been effectively solved so far
In addition, the temperature difference between the surface and the back of the solar cell on the high-altitude solar drone is small (0.5-2°C), and the internal temperature environment of the solar drone limits the use of airborne equipment

Method used

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
View more

Image

Smart Image Click on the blue labels to locate them in the text.
Viewing Examples
Smart Image
  • Rigid-flexible integrated solar cell considering heat insulation and development method thereof
  • Rigid-flexible integrated solar cell considering heat insulation and development method thereof
  • Rigid-flexible integrated solar cell considering heat insulation and development method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment Construction

[0035] Combine below figure 1 , 2 3. A further description is given to a rigid-flexible integrated solar cell that takes into account thermal insulation and its development method in the present invention:

[0036] The rigid-flexible integrated solar cell module of the present invention is applied to a specific solar drone wing, such as figure 1 shown.

[0037] The specific structural form of the rigid-flexible integrated solar cell with thermal insulation is as follows: figure 2 As shown, it mainly includes a surface encapsulation film 1, a transparent film 2, a high-efficiency rigid solar cell 3, a light film A4, a substrate film 5, a high-strength fiber 6, a light film B7, and a total of eight heat insulation layers 8. part.

[0038] The surface encapsulation film 1 is located on the outer surface of the battery assembly of the present invention. In this embodiment, modified PET with a light transmittance of 91% is used, which can protect the high-efficiency rigid sola...

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

PUM

No PUM Login to view more

Abstract

The invention provides a rigid-flexible integrated solar cell considering heat insulation and a development method thereof. According to the method, a high-efficiency rigid solar cell serves as a basis, flexible modular package is carried out on the rigid solar cell through reasonable reference and improvement of a flexible thin film solar cell package technology and by a dual-layer film material matched with a glue film, and a rigid-flexible integrated solar cell module is formed; and a hollow flexible heat insulation material serves as a heat insulation layer and is mainly used for effective control on temperature difference between the upper surface and the lower surface of a substrate structure. With the rigid-flexible integrated solar cell considering heat insulation, developed on the basis of the method, the problem of effective combination of a rigid solar cell array and an airplane sectional curved surface can be effectively solved; since the rigid-flexible integrated solar cell considers heat insulation, a favorable working temperature environment can be provided for an onboard device; the comprehensive requirements of a solar unmanned aerial vehicle on two aspects of battery conversion efficiency and unit area battery specific power can be met; and the flight performance of the solar unmanned aerial vehicle is improved.

Description

1. Technical field: [0001] The invention provides a rigid-flexible integrated solar cell with thermal insulation and a development method thereof, belonging to the technical field of aerospace vehicle energy systems. 2. Background technology: [0002] High-altitude long-endurance UAVs, as unmanned aerial vehicles that can operate at altitudes above the stratosphere, can perform intelligence, surveillance and reconnaissance, communication relay, target indication, damage assessment, telecommunication and television services, atmospheric environment monitoring and weather Forecasting and other military and civil tasks have become the hotspot of today's research. [0003] On the other hand, the use of solar energy as the auxiliary energy and even the main energy of future aircraft is an important research goal with direction and frontier for human development. Solar-powered airplanes appeared in the 1970s with the reduction of the cost of solar cells. Since solar-powered airpl...

Claims

the structure of the environmentally friendly knitted fabric provided by the present invention; figure 2 Flow chart of the yarn wrapping machine for environmentally friendly knitted fabrics and storage devices; image 3 Is the parameter map of the yarn covering machine
Login to view more

Application Information

Patent Timeline
no application Login to view more
Patent Type & Authority Applications(China)
IPC IPC(8): H01L31/048H01L31/18
CPCH01L31/0481Y02E10/50Y02P70/50
Inventor 孙康文贺双新史立峰许冬冬张馨运
Owner BEIHANG UNIV
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products