Battery backplane material

A battery backplane and raw material technology, applied in circuits, photovoltaic power generation, electrical components, etc., can solve the problems of mechanical properties such as poor neutral salt spray resistance and aging resistance, low breakdown voltage strength, and environmental pollution. The effect of not easy to environmental pollution, low production cost and good comprehensive performance

CN106117776AInactive Publication Date: 2016-11-16GUANGXI NANNING ZHICUI SCI TECH CONSULTATION CO LTD
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Patent Information

Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Publication Date
2016-11-16
Estimated Expiration
Not applicable · inactive patent

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Abstract

The invention discloses a battery backboard material, which is made of the following raw materials: EVA resin, dibutyl phthalate, tributoxyethyl phosphate, tris(2,4-di-tert-butylphenyl) Phosphate ester, oxalic acid polyester, maleic anhydride grafted EPDM rubber, chloropropyl styrene, maleic anhydride grafted polypropylene, hexabromocyclododecane, 3‑ethyl‑2‑butene ‑1‑alcohol, aluminum oxide, titanium oxide, paraffin, sodium tartrate, sodium polyphosphate, sodium hydroxymethylcellulose, silicon carbide fiber, extender pigment, coupling agent, compatibilizer, antioxidant, stabilizer, bridging agent Agents, regulators, strengthening agents, coagulants, toughening agents, plasticizers, thickeners, stabilizers, terminators. The battery back plate material prepared by the invention not only has good mechanical properties, neutral salt spray resistance and aging resistance, but also has excellent breakdown voltage strength, and can be widely used in solar battery back plate materials.
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Description

Technical field

[0001] The invention belongs to the technical field of environmental protection and the technical field of battery backboard material preparation, and in particular relates to a battery backboard material.

Background technique

[0002] The solar backsheet is located on the back of the solar panel. Fluorocarbon coatings made of PVDF, CTFE, and PTFE resins developed and produced by fluororesin multinational companies (such as Japan's Asahi Glass, Daikin, and France's Arkema, etc.) are widely used in It is used in the surface protection of bridges, buildings, railways, and communication facilities, and has withstood the harsh outdoor test for more than 40 years, showing excellent weather resistance. At the same time, material surface modification technologies including low-temperature plasma modification technology, radiation modification technology, and vacuum plasma chemical grafting technology are relatively mature. Therefore, fluorocarbon coatings, PET ...

Examples

preparation example Construction

[0036] The preparation method of the battery back plate material comprises the following steps:

[0037] S1: Graft EVA resin, dibutyl phthalate, tributoxyethyl phosphate, tris(2,4-di-tert-butylphenyl) phosphite, oxalic acid polyester and maleic anhydride Mix EPDM rubber and stir for 5-10 minutes at a temperature of 750-780°C and a rotation speed of 200-300r / min to obtain a mixture I;

[0038] S2: Under nitrogen protection, add chloropropyl styrene, maleic anhydride grafted polypropylene, hexabromocyclododecane, 3-ethyl-2-butene-1- Alcohol, paraffin, sodium tartrate, sodium polyphosphate, sodium hydroxymethylcellulose, coupling agent, compatibilizer, stabilizer, bridging agent, regulator, strengthening agent, coagulant, toughening agent, plasticizer 1. Thickener, stirring for 3-6 hours at a microwave power of 100-300W, a temperature of 650-700°C, and a rotation speed of 100-400r / min, to obtain mixture II;

[0039] S3: Add aluminum oxide, titanium oxide, silicon carbide fibers...

Embodiment 1

[0042] A battery back plate material, which is made of the following raw materials in units of weight: 150 parts of EVA resin, 40 parts of dibutyl phthalate, 32 parts of tributoxyethyl phosphate, tris(2,4-di 28 parts of tert-butylphenyl) phosphite, 18 parts of oxalic acid polyester, 20 parts of maleic anhydride grafted EPDM rubber, 20 parts of chloropropyl styrene, 18 parts of maleic anhydride grafted polypropylene , 13 parts of hexabromocyclododecane, 15 parts of 3-ethyl-2-buten-1-ol, 8 parts of aluminum oxide, 8 parts of titanium oxide, 20 parts of paraffin, 15 parts of sodium tartrate, 12 parts of sodium polyphosphate , 12 parts of sodium hydroxymethyl cellulose, 6 parts of silicon carbide fiber, 12 parts of extender pigment, 1.5 parts of coupling agent, 1.5 parts of compatibilizer, 1.2 parts of antioxidant, 1.2 parts of stabilizer, 0.8 part of bridging agent, adjustment 0.7 parts of agent, 0.5 parts of strengthening agent, 0.5 parts of coagulant, 0.4 parts of toughening ag...

Embodiment 2

[0050] A battery back plate material, in units of weight, made of the following raw materials: 115 parts of EVA resin, 35 parts of dibutyl phthalate, 30 parts of tributoxyethyl phosphate, three (2,4-di 25 parts of tert-butylphenyl) phosphite, 16 parts of oxalic acid polyester, 18 parts of maleic anhydride grafted EPDM rubber, 16 parts of chloropropyl styrene, 15 parts of maleic anhydride grafted polypropylene , 10 parts of hexabromocyclododecane, 12 parts of 3-ethyl-2-buten-1-ol, 6 parts of aluminum oxide, 6 parts of titanium oxide, 16 parts of paraffin, 10 parts of sodium tartrate, 8 parts of sodium polyphosphate , 9 parts of sodium hydroxymethyl cellulose, 4 parts of silicon carbide fiber, 18 parts of extender pigment, 1 part of coupling agent, 1 part of compatibilizer, 0.8 part of antioxidant, 0.8 part of stabilizer, 0.6 part of bridging agent, adjusting 0.5 parts of agent, 0.4 parts of strengthening agent, 0.4 parts of coagulant, 0.3 parts of toughening agent, 0.3 parts of...