Radiation curable ink compositions and applications thereof
View Patent ↗Radiation curable ink compositions that include a curable component having a functionality that is greater than two, is present in the ink composition in an amount greater than 30 percent by weight, and has a molecular weight in the range of about 400 g/mole to about 10,000 g/mole; a component that has a functionality that is less than or equal to 2; and an initiator component. A solvent component, pigment, a surface tension modifier and other materials also can be included. The radiation curable inks are employed in ink jet printers and are particularly suited for use in printing on large-scale substrates. The printed images described herein have good adhesion to polymeric substrates such as styrene-based, polycarbonates, polyolefins, polyethylene terephthalate glycol ester, acrylic and others.
1. A printing method comprising:
a) depositing a curable ink composition from an inkjet print head onto a substrate, wherein the ink composition comprises:
i. a first curable component that is present in the ink composition in an amount greater than 30 weight percent, has a functionality that is greater than 2 and a molecular weight in the range of from about 400 g/mole to about 10,000 g/mole, wherein the first curable component includes any of: (1) a hyperbranched or a dendridic acrylate oligomer; or (2) a polyester tetraacrylate oligomer;
ii. a second curable component that has a functionality that is less than or equal to 2; and
iii. an initiator component; and
b) curing the ink composition.
2. The method of claim 1 , wherein the ink composition is UV curable.
3. The method of claim 1 , wherein the first curable component includes ethoxylated trimethyloipropane triacrylate.
4. The method of claim 3 , wherein ethoxylated trimethylolpropane triacrylate is present in the radiation curable ink composition in an amount of at least about 16 weight percent.
5. The method of claim 4 , wherein ethoxylated trimethylolpropane triacrylate is present in the radiation curable ink composition in an amount in the range of from about 22 to about 31 weight percent.
6. The method of claim 1 , wherein the first curable component includes a hyperbranched or dendridic acrylate oligomer that is present in the radiation curable ink composition in an amount of no more than 9 weight percent.
7. The method of claim 1 , wherein the first curable component has a viscosity greater than 50 centipoise at 25° Celsius.
8. The method of claim 1 , wherein the second curable component includes at least one monofunctional (meth)acrylate compound and at least one difunctional (meth)acrylate compound.
9. The method of claim 1 , wherein the second curable component includes ethoxylated (2) neopentylglycol diacrylate, propoxylated (2) neopentylglycol diacrylate, 1,4-cyclohaxanedimethanol diacrylate, tetrahydrofurfuryl acrylate, isobornyl acrylate, ethoxylated 1,6-hexanediol diacrylate, propoxylated-1,6-hexanediol diacrylate, dipropylene glycol diacrylate or any combination thereof.
10. The method of claim 1 , wherein the second curable component is present in the curable ink composition in an amount of less than about 70 weight percent.
11. The method of claim 10 , wherein the second curable component is present in the curable ink composition in an amount in the range of from about 45 to about 51 weight percent.
12. The method of claim 1 , wherein the second curable component has a viscosity that is less than 50 centipoise at 25° centigrade.
13. The method of claim 1 , wherein the initiator component includes at least one photoinitiator.
14. The method of claim 1 , wherein the initiator component is present in the curable ink composition in an amount in the range of from about 2 to about 20 weight percent.
15. The method of claim 14 , wherein the initiator component is present in the curable ink composition in an amount in the range of from about 7 to about 16 weight percent.
16. The method of claim 1 , further including any of a pigment, a solvent and a surface tension modifier.
17. The method of claim 1 , wherein the radiation curable ink composition has a viscosity that is less than 25 centipoise at jet temperature.
18. The method of claim 17 , wherein the radiation curable ink composition has a viscosity in the range of from 10 to about 13 centipoise at a temperature in the range of from about 40° C. to about 58° C.
19. The method of claim 1 , wherein the radiation curable ink composition has a surface tension that is less than 30 dynes/cm 2 .
20. The method of claim 19 , wherein the radiation curable ink composition has a surface tension in the range of from about 25.5 to about 26.5 dynes/cm 2 .