Applying cold spray erosion protection to an airfoil
US-2019329906-A1 · Oct 31, 2019 · US
US12140386B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12140386-B2 |
| Application number | US-202217903993-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 6, 2022 |
| Priority date | Jul 7, 2021 |
| Publication date | Nov 12, 2024 |
| Grant date | Nov 12, 2024 |
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The heat-dissipating substrate structure includes a base layer and a cold spray coating layer. The cold spray coating layer is formed on a surface of the base layer. The cold spray coating layer is a film formed on the surface of the base layer by spraying a solid-phase metal powder and a high-pressure compressed gas onto the base layer. The solid-phase metal powder at least includes a film-forming powder with an apparent density of 3 to 4 g/cm 3 and a median particle diameter (D50) of 30 μm or less. A maximum depth of a bottom of the cold spray coating layer embedded in the base layer is less than 60 μm. A cooler contains an internal cooling fin joined to the base layer. An internal coolant passage is defined between the base layer, the internal cooling fin, and an interior of the cooler.
Opening claim text (preview).
What is claimed is: 1. A heat-dissipating substrate structure, comprising: a base layer made of a metal; and a cold spray coating layer formed on a top surface of the base layer; wherein the cold spray coating layer is a film formed on the top surface of the base layer by spraying a solid-phase metal powder and a high-pressure compressed gas with a pressure of 4 to 6 Mpa onto the base layer; wherein the solid-phase metal powder at least includes a film-forming powder with an apparent density of 3 to 4 g/cm 3 and a median particle diameter (D50) of 30 μm or less; wherein a maximum depth of a bottom of the cold spray coating layer embedded in the base layer is less than 60 μm; wherein at least one internal cooling fin is joined to a bottom surface of the base layer, and at least one internal coolant passage is defined between the base layer and the at least one internal cooling fin. 2. The heat-dissipating substrate structure according to claim 1 , wherein a predetermined ratio between a thickness of the base layer and a thickness of the cold spray coating layer ranges from 10:1 to 30:1. 3. The heat-dissipating substrate structure according to claim 2 , wherein the thickness of the base layer is from 1 mm to 3 mm. 4. The heat-dissipating substrate structure according to claim 1 , wherein the at least one internal cooling fin is joined to the bottom surface of the base layer by brazing, adhesive bonding, or solid-state welding. 5. The heat-dissipating substrate structure according to claim 1 , wherein the cold spray coating layer is a cold spray copper layer. 6. The heat-dissipating substrate structure according to claim 1 , wherein the base layer is an aluminum substrate.
by flowing liquids, e.g. forced water cooling · CPC title
Metallic materials (H10W40/254, H10W40/257, H10W40/255, H10W40/251, H10W40/253 take precedence) · CPC title
having a laminate or multilayered structure, e.g. direct bond copper [DBC] ceramic substrates · CPC title
of conductive package substrates serving as an interconnection, e.g. of metal plates (manufacture or treatment of leadframes H10W70/04) · CPC title
from aluminium or aluminium alloys · CPC title
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