High conductivity hydrid material for thermal management

• US 5,296,310 A
• Filed: 02/14/1992
• Issued: 03/22/1994
• Est. Priority Date: 02/14/1992
• Status: Expired due to Term

• Current Assignee: Thermal Corporation (Roper Technologies, Inc.)
• Original Assignee: Material Sciences Corporation (New Star Metals Holdings LLC)
• Inventors: Cassin, Thomas G., Kibler, John J.
• Primary Examiner(s): ZIMMERMAN, JOHN J
• Application Number:
  US07/836,130
• Time in Patent Office: 767 Days
• Field of Search: 428/614, 428/634, 428/588, 428/594, 428/654, 174/252, 165/185, 165/905, 361/386, 361/387, 361/388
• US Class Current: 428/614
• CPC Class Codes: B32B 15/16 next to a particulate layer
• CPC Class Codes: B32B 15/20 comprising aluminium or copper B32B15/016 and B32B15/017 take precedence
• CPC Class Codes: B32B 2307/302 Conductive
• CPC Class Codes: B32B 2457/00 Electrical equipment
• CPC Class Codes: B32B 5/16 characterised by features of a layer formed of particles, e.g. chips, powder or granules layer formed of natural mineral particles B32B19/00; layer being formed of wood fibres, chips or particles B32B21/02
• CPC Class Codes: B32B 9/007 comprising carbon, e.g. graphite, composite carbon
• CPC Class Codes: B32B 9/041 of metal
• CPC Class Codes: H01L 23/3733 having a heterogeneous or anisotropic structure, e.g. powder or fibres in a matrix, wire mesh, porous structures H01L23/3732, H01L23/3737 take precedence
• CPC Class Codes: H01L 23/3735 Laminates or multilayers, e.g. direct bond copper ceramic substrates
• CPC Class Codes: H01L 2924/00 Indexing scheme for arrangements or methods for connecting or disconnecting semiconductor or solid-state bodies as covered by H01L24/00
• CPC Class Codes: H01L 2924/0002 Not covered by any one of groups H01L24/00, H01L24/00 and H01L2224/00
• CPC Class Codes: Y10T 428/12486 Laterally noncoextensive components [e.g., embedded, etc.]
• CPC Class Codes: Y10T 428/12625 Free carbon containing component

Abstract

A hybrid structural material combines high thermal conductivity and pre-determined mechanical properties compatible with adjacent or attached materials. It has three elements: (1) a non-structural, high thermal conductivity core material which defines the thermal conductivity of the hybrid structural material; (2) a pair of face sheets, which form opposing surfaces of the hybrid structural material and help to define its mechanical properties, disposed on opposite sides of the core material to create a face sheet-core material-face sheet sandwich construction; and (3) a frame substantially surrounding the core material and bonded to the face sheets for helping to define (along with the face sheets) the mechanical properties of the hybrid structural material.

The interfaces between the face sheets and the core material allow physical contact, but prevent structural interaction, between the face sheets and the core material. Consequently, the hybrid structural material achieves a high fraction of the thermal conductivity of the core material while maintaining the thermal expansion (and other mechanical properties) of the face sheets and frame.

Claims

1. A hybrid structural material for thermal management including heat gathering and heat removal and allowing independent tailoring of mechanical properties, thermal expansion characteristics, and thermal conductivities, said hybrid structural material comprising:

a non-structural, high thermal conductivity core material defining the thermal conductivity of said hybrid structural material;

a pair of face sheets forming opposing surfaces of said hybrid structural material and helping to define the mechanical properties of said hybrid structural material, the first of said face sheets disposed on one side of said core material and the second of said face sheets disposed on the opposite side of said core material to create a face sheet-core material-face sheet sandwich construction;

a first interface between said first face sheet and said core material allowing physical contact between said first face sheet and said core material and allowing said first face sheet to slide over said core material on heating and cooling;

a second interface between said second face sheet and said core material allowing physical contact between said second face sheet and said core material and allowing said second face sheet to slide over said core material on heating and cooling; and

a frame substantially surrounding said core material and attached, by one of bonding to and integrally forming with, said face sheets for helping to define the mechanical properties of said hybrid structural material.

2. A hybrid structural material according to claim 1 wherein said hybrid structural material is adapted to mount electronic components and transfer heat generated by the electronic components.

3. A hybrid structural material according to claim 1 wherein said core material has an in-plane isotropic thermal conductivity greater than 1400 W/m-k.

4. A hybrid structural material according to claim 3 wherein said core material is compression annealed pyrolytic graphite.

5. A hybrid structural material according to claim 1 wherein said core material is not in structural interaction with said frame and said face sheets.

6. A hybrid structural material according to claim 1 wherein said face sheets are graphite reinforced aluminum.

7. A hybrid structural material according to claim 6 wherein said face sheets are pitch-based graphite fibers in an aluminum matrix.

8. A hybrid structural material according to claim 1 wherein said frame is a monolithic aluminum alloy.

9. A hybrid structural material according to claim 1 wherein said frame is bonded to said face sheets by diffusion.

10. A hybrid structural material according to claim 1 wherein said frame is integral with said face sheets.

11. A hybrid structural material according to claim 1 wherein said frame has multiple ribs.

12. A hybrid structural material according to claim 11 wherein said ribs provide only a structural connection between said face sheets.

13. A hybrid structural material according to claim 1 wherein said core material is in slight compression to assure physical contact between said face sheets and said core material.

14. A hybrid structural material for mounting electronic components and transferring heat generated by the electronic components and combining high thermal conductivity and mechanical properties independently selected to be compatible with adjacent electronic components, said hybrid structural material comprising:

a non-structural, high thermal conductivity core material chosen from the group consisting of highly ordered pyrolytic graphite, compression annealed pyrolytic graphite, and synthetic diamond, having an in-plane isotropic thermal conductivity greater than 750 W/m-K, and defining the thermal conductivity of said hybrid structural material;

a pair of face sheets forming opposing surfaces of said hybrid structural material and helping to define the mechanical properties of said hybrid structural material, the first of said face sheets disposed on one side of said core material and the second of said face sheets disposed on the opposite side of said core material to create a face sheet-core material-face sheet sandwich construction;

a first interface between said first face sheet and said core material allowing physical contact between said first face sheet and said core material and sallowing said first face sheet to slide over said core material on heating and cooling;

a second interface between said second face sheet and said core material allowing physical contact between said second face sheet and said core material and allowing said second face sheet to slide over said core material on heating and cooling; and

a frame substantially surrounding said core material and bonded to said face sheets for helping to define the mechanical properties of said hybrid structural material.

15. A hybrid structural material according to claim 14 wherein said core material is compression annealed pyrolytic graphite.

16. A hybrid structural material according to claim 14 wherein said face sheets are graphite reinforced aluminum.

17. A hybrid structural material according to claim 16 wherein said face sheets are pitch-based graphite fibers in an aluminum matrix.

18. A hybrid structural material according to claim 14 wherein said frame is a monolithic aluminum alloy.

19. A hybrid structural material according to claim 14 wherein said frame is bonded to said face sheets by diffusion.

20. A hybrid structural material according to claim 14 wherein said frame has multiple ribs.

21. A hybrid structural material according to claim 14 wherein said core material is in slight compression to assure physical contact between said face sheets and said core material at said first and second interfaces.