Claims
- 1. An information carrying disk comprising
- a substrate with a recording medium thereon;
- first and second hub halves, each hub half having an annular outer surface area facing the substrate and an inner annular surface area facing the other hub half;
- a bond layer having a thickness of less than one millimeter bonding the outer annular surface area of a hub half to the substrate, the bond layer including a cross-linked adhesive and a monolayer of spheroids dispersed within the adhesive, the spheroids made of a material selected from the group consisting of aluminum, glass and other ceramics, the bond layer thickness being no less than the maximum diameter of the spheroids; and
- a cross-linked adhesive disposed between the inner annular surface areas of the hub halves, wherein an air space is positioned between the cross-linked adhesive and the cross-linked adhesive with spheroids and the substrate.
- 2. The disk of claim 1 wherein the cross-linked adhesive in the bond layer is an epoxy.
- 3. The disk of claim 2 wherein the spheroids have a coefficient of thermal expansion which approximates that of the substrate.
- 4. The disk of claim 3 in which the substrate comprises glass.
- 5. The disk of claim 2 in which the size distribution of the spheroids is between 40% and 95% of the thickness of the bond layer.
- 6. The disk of claim 1 wherein the bond layer thickness is within the range of from about 200 to 350 micrometers.
- 7. A method for assembling a recording disk having a hub, and a recording medium disposed on a substrate, wherein the hub includes first and second hub halves, each hub half having an annular outer surface area facing the substrate and an inner annular surface area facing the other hub half, the method comprising:
- applying a bonding layer between the outer annular surface area of each hub half and the substrate, the bonding layer including a cross-linkable adhesive and a monolayer of spheroids dispersed within the adhesive, wherein the bonding layer has a thickness of less than 1 millimeter but no less than the maximum diameter of the spheroids;
- applying a cross-linkable adhesive between the inner annular surface areas of the hub halves, wherein an air space is positioned between the cross-linkable adhesive and the cross-linkable adhesive with spheroids and the substrate; and curing the adhesives.
- 8. The method of claim 7 wherein the cross-linkable adhesive in the bonding layer is an epoxy.
- 9. The method of claim 7 wherein the spheroids have an effective diameter range of from about 200 to 350 micrometers.
- 10. The method of claim 7 further including applying a selected pressure to the dispersed bonding layer prior to curing such that the bonding layer thickness conforms to the maximum diameter of the spheroids.
Government Interests
This invention was made with Government support under Contract No. 30602-89-C-0008 awarded by the United States Air Force Rome Air Development Center. The Government has certain rights in the invention.
US Referenced Citations (14)
Foreign Referenced Citations (1)
Number |
Date |
Country |
49-30259 |
Aug 1974 |
JPX |