Thermal interface material assemblies and systems and methods for controllably changing surface tack of thermal interface materials

1. A thermal interface material assembly comprising a thermal interface material, a first liner, a first coating directly on the thermal interface material between a first surface of the thermal interface material and an inner surface of the first liner, a second liner, and a second coating directly on the thermal interface material between a second surface of the thermal interface material and an inner surface of the second liner, wherein the thermal interface material comprises a first silicone and thermally-conductive filler, the first coating comprises a second silicone, and the second coating comprises a third silicone, whereby the first coating is configured such that at least a portion of the first coating will remain along the first surface of the thermal interface material after removal of the first liner from the thermal interface material assembly to thereby decrease a surface tack of the first surface of the thermal interface material, and whereby the second coating is configured such that at least a portion of the second coating will remain along the second surface of the thermal interface material after removal of the second liner from the thermal interface material assembly to thereby increase a surface tack of the second surface of the thermal interface material.

2. The thermal interface material assembly of claim 1 , wherein the first coating comprises a one-part silane composition having a viscosity less than 400 centipoises and a number average molecular weight less than 10000.

3. The thermal interface material assembly of claim 2 , wherein the first coating further comprises:

a two-part silane composition having a viscosity from 400 centipoises to 2000 centipoises and a number average molecular weight from 10000 to 30000; or

a two-part silane composition having a viscosity greater than 2000 centipoises and a number average molecular weight greater than 30000.

4. The thermal interface material assembly of claim 1 , wherein:

the first liner comprises a polyethylene terephthalate liner; and

the first coating comprises a wet coating having a thickness within a range from about 8 micrometers to about 76 micrometers; and

the thermal interface material comprises a thermally-conductive gap filler sheet material having the first surface with the surface tack that is decreased by the first coating and the second surface with the surface tack that is increased by the second coating.

5. The thermal interface material assembly of claim 1 ,

wherein the second coating comprises a two-part silane composition.

6. The thermal interface material assembly of claim 1 , wherein:

the first coating and the second coating comprise a methyl vinyl silane composition and a platinum catalyzer; and

the second liner comprises a polyethylene terephthalate liner; and

the second coating comprises a wet coating having a thickness within a range from about 8 micrometers to about 76 micrometers; and

the thermal interface material comprises a thermally-conductive gap filler sheet material having the first surface with the surface tack that is decreased by the first coating and the second surface with the surface tack that is increased by the second coating.

7. A thermal interface material assembly comprising a thermal interface material having a first surface and a second surface, a first coating directly on the first surface of the thermal interface material, a second coating directly on the second surface of the thermal interface material, the thermal interface material comprising a first silicone and thermally-conductive filler, the first coating comprising a second silicone, the second coating comprising a third silicone, whereby the first coating decreases the surface tack of the first surface of the thermal interface material, and whereby the second coating increases the surface tack of the second surface of the thermal interface material.

8. The thermal interface material assembly of claim 7 , further comprising a first liner having an inner surface, wherein the first coating is between the first surface of the thermal interface material and the inner surface of the first liner, whereby the first coating is configured such that at least a portion of the first coating will remain along the first surface of the thermal interface material after removal of the first liner from the thermal interface material assembly to thereby decrease the surface tack of the first surface of the thermal interface material.

9. The thermal interface material assembly of claim 7 , wherein the first coating comprises a one-part silane composition having a viscosity less than 400 centipoises and a number average molecular weight less than 10000.

10. The thermal interface material assembly of claim 7 , wherein the thermal interface material comprises a thermally-conductive gap filler sheet material having the first surface with the surface tack that is decreased by the first coating and the second surface with the surface tack that is increased by the second coating.

11. The thermal interface material assembly of claim 7 , wherein

the second coating comprises a two-part silane composition.

12. The thermal interface material assembly of claim 8 , further comprising a second liner having an inner surface, wherein the second coating is between the second surface of the thermal interface material and the inner surface of the second liner, whereby the second coating is configured such that at least a portion of the second coating will remain along the second surface of the thermal interface material after removal of the second liner from the thermal interface material assembly to thereby increase the surface tack of the second surface of the thermal interface material.

13. A method of controllably changing surface tack of a thermal interface material, the method of comprising:

applying a first coating along an inner surface of a first liner;

applying a thermal interface material along the first liner such that the first coating is directly on the thermal interface material between a first surface of the thermal interface material and the inner surface of the first liner;

applying a second coating along an inner surface of a second liner; and

applying the second liner over a second surface of the thermal interface material such that the second coating is directly on the thermal interface material between the second surface of the thermal interface material and the inner surface of the second liner;

wherein the thermal interface material comprises a first silicone and thermally-conductive filler, the first coating comprises a second silicone, the second coating comprises a third silicone,

whereby the first coating is configured such that at least a portion of the first coating will remain along the first surface of the thermal interface material after removal of the first liner from the thermal interface material to thereby decrease a surface tack of the first surface of the thermal interface material, and whereby the second coating is configured such that at least a portion of the second coating will remain along the second surface of the thermal interface material after removal of the second liner from the thermal interface material assembly to thereby increase a surface tack of the second surface of the thermal interface material.

14. The method of claim 13 , further comprising forming and curing the thermal interface material after applying the first coating and after applying the thermal interface material to the first liner.

15. The method of claim 14 , wherein:

applying the first coating comprises wet coating the first coating along the inner surface of first liner;

forming the thermal interface material comprises compressing the thermal interface material to thereby reduce a thickness of the thermal interface material; and

curing the thermal interface material comprises heating the thermal interface material to a curing temperature.

16. The method of claim 13 , further comprising

forming and curing the thermal interface material while the thermal interface material is between the first and second liners.

17. The method of claim 13 , wherein the method further comprises removing the first and second liners from the respective first and second surfaces of the thermal interface materials, whereby the first and second coatings remain along the respective first and second surfaces of the thermal interface material after removal of the first and second liners to thereby decrease and increase, respectively, the surface tack of the respective first and second surfaces of the thermal interface material.