High energy electron beam curing of epoxy resin systems incorporating cationic photoinitiators
First Claim
Patent Images
1. A non-thermal curing method characterized as not using external heat for curing an epoxy resin system comprising the following steps:
- Step 1. providing a blend of an epoxy resin system, said epoxy resin system comprising an epoxy resin and a cationic photoinitiator, said cationic photoinitiator being a diaryliodonium salt; and
Step 2. irradiating said blend with high energy electron beam ionizing radiation for a period of time sufficient to effectuate an efficient cross-linking and an essentially complete and uniform non-thermal curing of said epoxy resin system thereby forming a non-thermally cured epoxy resin system having a glass transition temperature essentially the same or greater than a glass transition temperature obtained by thermally curing said epoxy resin system.
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Abstract
A mixture of epoxy resins such as a semi-solid triglycidyl ether of tris (hydroxyphenyl) methane and a low viscosity bisphenol A glycidyl ether and a cationic photoinitiator such as a diaryliodonium salt is cured by irradiating with a dosage of electron beams from about 50 to about 150 kGy, forming a cross-linked epoxy resin polymer.
55 Citations
24 Claims
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1. A non-thermal curing method characterized as not using external heat for curing an epoxy resin system comprising the following steps:
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Step 1. providing a blend of an epoxy resin system, said epoxy resin system comprising an epoxy resin and a cationic photoinitiator, said cationic photoinitiator being a diaryliodonium salt; and Step 2. irradiating said blend with high energy electron beam ionizing radiation for a period of time sufficient to effectuate an efficient cross-linking and an essentially complete and uniform non-thermal curing of said epoxy resin system thereby forming a non-thermally cured epoxy resin system having a glass transition temperature essentially the same or greater than a glass transition temperature obtained by thermally curing said epoxy resin system. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 16, 17, 18, 19, 20)
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15. A non-thermal curing method characterized as not using external heat for curing an epoxy resin system comprising the following steps:
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Step 1. providing a blend of an epoxy resin system, said epoxy resin system consisting essentially of an epoxy resin and a cationic photoinitiator, said epoxy resin being a diglycidyl ether of bisphenol A and said cationic photoinitiator being from about 0.5 to about 4 parts of (4-octyloxyphenyl)phenyliodonium hexafluoroantimonate per hundred parts of said epoxy resin, and Step 2. irradiating said blend with high energy electron beam radiation for a period of time sufficient to effectuate an efficient cross-linking and an essentially complete and uniform non-thermal curing of said epoxy resin system thereby forming a non-thermally cured epoxy resin system having a glass transition temperature from about 124°
C. to about 207°
C. tan delta.
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21. A epoxy resin system consisting essentially of an epoxy resin and a cationic photoinitiator, said epoxy resin consists essentially of a fifty-fifty blend of bis(2,3-epoxycyclopentyl) ether and diglycidyl ether of bisphenol A and said cationic photoinitiator consists essentially of from about 1 part to about 5 parts of (4-octyloxyphenyl) phenyliodonium hexafluoroantimonate per 100 parts of said epoxy resin;
- said epoxy system being characterized as producing a non-thermally cured epoxy resin system having a glass transition temperature from about 147°
C. to about 205°
C. tan delta when exposed to high energy ionizing radiation generated by an electron beam accelerator having an energy of 10 MeV and a power of 1 kW.
- said epoxy system being characterized as producing a non-thermally cured epoxy resin system having a glass transition temperature from about 147°
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22. A epoxy resin system where in the epoxy resin consists essentially of diglycidyl ether of bisphenol A and the cationic photoinitiator consists essentially of from about 0.5 to about 4 parts of (4-octyloxyphenyl)phenyliodonium hexafluoroantimonate per 100 parts of said epoxy resin;
- said epoxy system being characterized as producing a non-thermally cured epoxy resin system having a glass transition temperature from about 124°
C. to about 207°
C. tan delta when exposed to high energy ionizing radiation generated by an electron beam accelerator having an energy of 10 MeV and a power of 1 kW.
- said epoxy system being characterized as producing a non-thermally cured epoxy resin system having a glass transition temperature from about 124°
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23. A epoxy resin system wherein the epoxy resin consists essentially of a epoxy phenolic novalac and the cationic photoinitiator consists essentially of about one part to about 5 parts of (4-octyloxyphenyl)phenyliodonium hexafluoroantimonate per 100 parts of said epoxy resin;
- said epoxy system being characterized as producing a non-thermally cured epoxy resin system having a glass transition temperature from about 128°
C. to about 197°
C. Tan delta when exposed to high energy ionizing radiation generated by an electron beam accelerator having an energy of 10 MeV and a power of 1 kW.
- said epoxy system being characterized as producing a non-thermally cured epoxy resin system having a glass transition temperature from about 128°
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24. A epoxy resin system wherein the epoxy resin consists essentially of a triglycidyl ether of tris(4-hydroxyphenyl)methane-based epoxy and the cationic photoinitiator consists essentially of about 3 parts of (4-Octyloxyphenyl) phenyliodonium hexafluoroantimonate per 100 parts of said epoxy resin;
- said epoxy system being characterized as producing a non-thermally cured epoxy resin system having a glass transition temperature being 362°
C. tan delta when exposed to high energy ionizing radiation generated by an electron beam accelerator having an energy of 10 MeV and a power of 1 kW.
- said epoxy system being characterized as producing a non-thermally cured epoxy resin system having a glass transition temperature being 362°
Specification