Cooling assemblies having porous three dimensional surfaces

Patent metadata

Field	Value
Publication number	US-9803938-B2
Application number	US-201313935800-A
Country	US
Kind code	B2
Filing date	Jul 5, 2013
Priority date	Jul 5, 2013
Publication date	Oct 31, 2017
Grant date	Oct 31, 2017

Abstract

Cooling assemblies including a porous three dimensional surface such as a heat sink are disclosed. In one embodiment, a cooling assembly includes a heat transfer substrate having a surface, a thermally conductive fin extending from the surface, a metal mesh bonded to a surface of the thermally conductive fin, and sintered metal particles bonded to the metal mesh and the surface of the thermally conductive fin. The metal mesh defines a macro-level porosity, and the sintered metal particles define a micro-level porosity. In another embodiment, a cooling assembly includes a heat transfer substrate having a surface, a thermally conductive fin extending from the surface of the heat transfer substrate, and sintered metal particles bonded to the surface of the thermally conductive fin. An average diameter of the sintered metal particles increases from a base of the thermally conductive fin to a top of the thermally conductive fin.

First claim

What is claimed is:

1. A cooling assembly comprising:
a heat transfer substrate having a surface;
a thermally conductive fin comprising one or more surfaces, the thermally conductive fin extending from the surface of the heat transfer substrate;
a metal mesh that is diffusion bonded to each of the one or more surfaces of the thermally conductive fin, the metal mesh conforming entirely to each of the one or more surfaces of the thermally conductive fin and defining a macro-porosity; and
sintered metal particles that are at least one of sintered and diffusion bonded to the surfaces of the thermally conductive fin to form a layer of sintered metal particles, wherein:
the sintered metal particles define a micro-level porosity; and
an average diameter of the sintered metal particles increases from a base of the thermally conductive fin to a top of the thermally conductive fin.

2. The cooling assembly of claim 1 , wherein the thermally conductive fin is an individual thermally conductive fin of an array of thermally conductive fins extending from the surface of the heat transfer substrate, and the layer of sintered metal particles is bonded to each thermally conductive fin of the array of thermally conductive fins.

3. The cooling assembly of claim 2 , wherein the layer of sintered metal particles is bonded to the surface of the heat transfer substrate between adjacent thermally conductive fins of the array of thermally conductive fins.

4. The cooling assembly of claim 1 , wherein the heat transfer substrate, the thermally conductive fin, and the sintered metal particles are made of copper.

5. The cooling assembly of claim 1 , wherein the sintered metal particles have an average diameter between about 40 μm and about 150 μm.

6. The cooling assembly of claim 1 , further comprising an impingement jet assembly comprising a fluid inlet channel fluidly coupled to an array of orifices provided in a jet plate, wherein the jet plate is offset from the heat transfer substrate.

7. A cooling assembly comprising:
a heat transfer substrate having a surface;
an array of thermally conductive fins comprising one or more surfaces, the array of thermally conductive fins being integrally formed with and extending from the surface of the heat transfer substrate; and
a metal mesh that is diffusion bonded to the surfaces of the array of thermally conductive fins and a surface of the heat transfer substrate between adjacent thermally conductive fins of the array of thermally conductive fins, the metal mesh conforming entirely to each of the one or more surfaces of the array of thermally conductive fins and defining a macro-porosity.

8. The cooling assembly of claim 7 , wherein the heat transfer substrate, the array of thermally conductive fins, and the metal mesh are made of copper.

9. The cooling assembly of claim 7 , wherein the metal mesh is at least 50% porous.

10. The cooling assembly of claim 7 , further comprising an impingement jet assembly comprising a fluid inlet channel fluidly coupled to an array of orifices provided in a jet plate, wherein the jet plate is offset from the heat transfer substrate.

11. A cooling assembly comprising:
a heat transfer substrate having a surface;
a thermally conductive fin comprising one or more surfaces, the thermally conductive fin extending from the surface of the heat transfer substrate;
a metal mesh bonded to each of the one or more surfaces of the thermally conductive fin, the metal mesh conforming entirely to each of the one or more surfaces of the thermally conductive fin and defining a macro-level porosity; and
sintered metal particles that are at least one of sintered and diffusion bonded to the metal mesh and the surfaces of the thermally conductive fin to form a layer of sintered metal particles, the sintered metal particles defining a micro-level porosity, wherein an average diameter of the sintered metal particles increases from a base of the thermally conductive fin to a top of the thermally conductive fin.

12. The cooling assembly of claim 11 , wherein the metal mesh and the layer of sintered metal particles are disposed on at least a portion of the surface of the heat transfer substrate.

13. The cooling assembly of claim 11 , wherein the thermally conductive fin is an individual thermally conductive fin of an array of thermally conductive fins extending from the surface of the heat transfer substrate, and the metal mesh and the layer of sintered metal particles are bonded to each thermally conductive fin of the array of thermally conductive fins.

14. The cooling assembly of claim 13 , wherein the metal mesh and the layer of sintered metal particles are bonded to the surface of the heat transfer substrate between adjacent thermally conductive fins of the array of thermally conductive fins.

15. The cooling assembly of claim 11 , wherein the metal mesh is bonded to the each of the one or more surfaces of the thermally conductive fin by diffusion bonding.

16. The cooling assembly of claim 11 , wherein the heat transfer substrate, the thermally conductive fin, the metal mesh, and the sintered metal particles are made of copper.

17. The cooling assembly of claim 11 , wherein the sintered metal particles have an average diameter between about 40 μm and about 150 μm.

18. The cooling assembly of claim 11 , further comprising an impingement jet assembly comprising a fluid inlet channel fluidly coupled to an array of orifices provided in a jet plate, wherein the jet plate is offset from the heat transfer substrate.

19. The cooling assembly of claim 1 , wherein the layer of sintered metal particles are at least one of diffusion sintered and diffusion bonded to a top surface and peripheral surfaces of the thermally conductive fin and the layer of sintered metal particles comprises a thickness that is constant along the peripheral and top surfaces of the fin.

20. The cooling assembly of claim 19 , wherein the thickness of the layer of sintered metal particles is about 0.25 mm.

21. The cooling assembly of claim 2 , wherein layers of sintered metal particles on opposing surfaces of two adjacent thermally conductive fins of the array of thermally conductive fins are spaced apart from one another.

Assignees

• Toyota Motor Eng & Mfg North America Inc

Inventors

• Joshi Shailesh N

Classifications

• H10W40/475

  using jet impingement (H10W40/776 takes precedence) · CPC title

• H10W40/257

  having a heterogeneous or anisotropic structure, e.g. powder or fibres in a matrix, wire mesh or porous structures (H10W40/254, H10W40/251 take precedence) · CPC title

• H10W40/037

  Assembling together parts thereof · CPC title

• F28F1/122

  and being formed of wires · CPC title

• F28F13/003

  by using permeable mass, perforated or porous materials (F28F13/18 takes precedence) · CPC title