Method to produce high corrosion and wear resistant cast iron components by water jet surface activation, nitrocarburization and thermal spray coating
US-2024084430-A1 · Mar 14, 2024 · US
US9683281B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9683281-B2 |
| Application number | US-201514683820-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 10, 2015 |
| Priority date | Apr 10, 2015 |
| Publication date | Jun 20, 2017 |
| Grant date | Jun 20, 2017 |
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A method of forming a thermal barrier coating on a metal part includes laser cleaning a surface of the metal part to remove undesirable oxides and residues from the surface of the part. It further includes depositing an aluminum containing bondcoat on the part and thermally interdiffusing the bondcoat and the part with a heat treatment. Laser cleaning a surface of the bondcoat to remove oxides and debris from the surface forms an alpha aluminum oxide layer on the bondcoat. A ceramic topcoat is then deposited on the alpha aluminum oxide layer at a temperature above 1800° F. (982° C.).
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The invention claimed is: 1. A method of forming a thermal barrier coating on a metal part comprising: laser cleaning a surface of the metal part to remove undesirable oxides and residues from the surface of the part; depositing an aluminum containing bondcoat on the part; thermally interdiffusing the aluminum containing bondcoat and the part with a heat treatment; laser cleaning a surface of the aluminum containing bondcoat to remove oxides and debris from the surface of the bondcoat and form an alpha aluminum oxide layer on the bondcoat; preheating the surface of the aluminum containing bondcoat above 1800° F. (982° C.); and depositing a ceramic topcoat on the alpha aluminum oxide layer on the bondcoat. 2. The method of claim 1 wherein the metal part comprises a nickel based, cobalt based, iron based superalloy or mixtures thereof. 3. The method of claim 1 wherein laser cleaning comprises exposing the surface to a laser focused on the surface of the metal part or on the surface of the aluminum containing bondcoat. 4. The method of claim 3 wherein the laser comprises a YAG (yttrium aluminum garnet), UV (ultraviolet), eximer, CO 2 (carbon dioxide), fiber, or disc laser. 5. The method of claim 1 wherien the aluminum containing bondcoat comprises MCrAlY wherein M is Ni, Co, Fe, Pt, Hf, Si, Fe-base, Ni-base, or Co-base alloys, or mixtures thereof. 6. The method of claim 1 wherein depositing the aluminum containing bondcoat comprises low pressure plasma spray (LPPS), high velocity oxy fuel (HVOF) spray, cathodic arc deposition, or chemical vapor deposition. 7. The method of claim 6 wherein depositing the ceramic topcoat comprises electron beam physical vapor deposition (EBPVD). 8. The method of claim 1 wherein the ceramic topcoat comprises yttria stabilized zirconia, gadolinia zirconia, ceria stabilized zirconia, or mixtures thereof.
with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer · CPC title
in an atmosphere of particular gases · CPC title
Aluminium or alloys thereof · CPC title
by means of bombardment with energetic particles or radiation · CPC title
in a liquid, e.g. underwater · CPC title
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