초록 ▼

A method of in situ stabilizing a composite lubricant in order to reduce or subtantially eliminate phase separation of the components of the composite lubricant, comprising sequential steps of: (a) providing a substrate including a surface; (b) applying a thin layer or film of the composite lubr

A method of in situ stabilizing a composite lubricant in order to reduce or subtantially eliminate phase separation of the components of the composite lubricant, comprising sequential steps of: (a) providing a substrate including a surface; (b) applying a thin layer or film of the composite lubricant to the substrate surface, the composite lubricant comprising at least two lubricant components which are normally mutually immiscible; and (c) treating the thin layer or film of composite lubricant solely with UV radiation for an interval sufficient to reduce or substantially eliminate phase separation of the at least two normally mutually immiscible lubricant components. Embodiments of the invention include magnetic and magneto-optical (MO) media including stabilized composite lubricant layers formed in situ according to the inventive process.

대표청구항 ▼

A method of in situ stabilizing a composite lubricant in order to reduce or subtantially eliminate phase separation of the components of the composite lubricant, comprising sequential steps of: (a) providing a substrate including a surface; (b) applying a thin layer or film of the composite lubr

A method of in situ stabilizing a composite lubricant in order to reduce or subtantially eliminate phase separation of the components of the composite lubricant, comprising sequential steps of: (a) providing a substrate including a surface; (b) applying a thin layer or film of the composite lubricant to the substrate surface, the composite lubricant comprising at least two lubricant components which are normally mutually immiscible; and (c) treating the thin layer or film of composite lubricant solely with UV radiation for an interval sufficient to reduce or substantially eliminate phase separation of the at least two normally mutually immiscible lubricant components. Embodiments of the invention include magnetic and magneto-optical (MO) media including stabilized composite lubricant layers formed in situ according to the inventive process. ote from said first surface region of said plurality of resilient elements. 10. The assembly as claimed in claim 9, wherein said plurality of resilient elements are wound in a spiral between the first surface of the liner and the second surface of the liner. 11. A transferable resilient element assembly for fabricating a microelectronic package comprising: a first liner including a cure-inhibiting material; and a resilient element having regions with different degrees of cure being in contact with said first liner. 12. The assembly as claimed in claim 11, wherein said resilient element has a first surface region in contact with said first liner and an interior region remote from said first liner, said first surface region of said resilient element having a lesser degree of cure than said interior region of said resilient element. 13. The assembly of claim 11, wherein said cure-inhibiting material is selected from the group consisting of amines and chelating agents. 14. The assembly as claimed in claim 11, wherein said resilient element includes a porous resilient layer. 15. The assembly as claimed in claim 14, wherein said porous resilient layer includes a plurality of compliant pads. 16. The assembly as claimed in claim 15, wherein said porous resilient layer further includes a web interconnecting said plurality of compliant pads with one another so that define channels therebetween. 17. The assembly as claimed in claim 15, wherein said resilient element is a continuous resilient layer. 18. The assembly as claimed in claim 12, further comprising a second liner including a cure-inhibiting material being abutted against a second surface region of said resilient element remote from said first surface region, wherein said second surface region is in contact with the second liner. 19. The assembly as claimed in claim 18, wherein the level of adhesion between the first liner and said first surface region of said resilient element is lower than the level of adhesion between the second liner and said second surface region of said resilient element. 20. The assembly as claimed in claim 12, wherein said first liner includes a second surface being abutted against a second surface region of said resilient element, said second surface region of said resilient element being remote from said first surface region of said resilient element. 21. The assembly as claimed in claim 20, wherein a plurality of resilient elements are in engagement with said first liner, said resilient elements being wound in a spiral between the first surface of the liner and the second surface of the liner. 22. The assembly as claimed in claim 1, wherein the tacky material is a single continuous layer on said first liner. 23. The assembly as claimed in claim 2, wherein the adhesive is a single continuous layer on said first liner.