Method of manufacturing turbine airfoil and tip component thereof using ceramic core with witness feature
US-10702958-B2 · Jul 7, 2020 · US
US11498121B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11498121-B2 |
| Application number | US-202016816447-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 12, 2020 |
| Priority date | Mar 14, 2019 |
| Publication date | Nov 15, 2022 |
| Grant date | Nov 15, 2022 |
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Methods for creating a cast component, along with the resulting cast components, are provided. The method may include heating a mold having a cavity therein; supplying a first molten metal material into the cavity of the mold such that the first molten metal material is directed to a first portion of the cavity of the mold; supplying a second molten metal material into the cavity of the mold such that the second molten metal material is directed to a second portion of the cavity of the mold, wherein the first molten metal material is compositionally different than the second molten metal material; and thereafter, allowing the first molten metal material and the second molten metal material to form the cast component.
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What is claimed is: 1. A method of creating a cast component, the method comprising: heating a mold having a cavity therein under controlled conditions such that a first portion of the cavity has a first controlled thermal condition and a second portion of the cavity has a second controlled thermal condition that is different than the first controlled thermal condition; thereafter, supplying a first molten metal material into the cavity of the mold such that the first molten metal material is directed to the first portion of the cavity of the mold; supplying a second molten metal material into the cavity of the mold such that the second molten metal material is directed to the second portion of the cavity of the mold, wherein the first molten metal material is compositionally different than the second molten metal material; and thereafter, allowing the first molten metal material and the second molten metal material to form the cast component by cooling and solidifying the first molten metal material and the second molten metal material; wherein the mold is heated such that the first portion has an initial first portion temperature and the second portion has an initial second portion temperature that is different than the initial first portion temperature, and wherein the second portion of the mold is surrounded by an insulating material and wherein the first portion of the mold is not in contact with the insulating material. 2. The method of claim 1 , wherein the insulating material is a powder of ceramic material. 3. The method of claim 1 , wherein the first portion of the mold is exposed. 4. The method of claim 1 , wherein the first molten metal material is an alloy or a superalloy, and wherein the second molten metal material is an alloy or a superalloy. 5. The method of claim 1 , wherein the first molten metal material and the second molten metal material mix together within the mold to form a transition zone within the cast component in a transition area between the first portion and the second portion. 6. The method of claim 1 , wherein the mold is rotatable around an axis, and wherein the method further comprises: rotating the mold around the axis while supplying the first molten metal material into the cavity such that the first molten metal material flows radially outwardly within the cavity. 7. The method of claim 1 , wherein the initial first portion temperature is greater than the initial second portion temperature. 8. The method of claim 1 , wherein the cast component has a first section corresponding to the first portion of the mold and having a first average grain size therein, and wherein the cast component has a second section corresponding to the second portion of the mold and having a second average grain size therein; wherein the first average grain size is greater than the second average grain size. 9. The method of claim 1 , wherein the cast component has a first section corresponding to the first portion of the mold and having a first average grain size therein, and wherein the cast component has a second section corresponding to the second portion of the mold and having a second average grain size therein; wherein the first average grain size has a higher average aspect ratio than the second average grain size. 10. The method of claim 9 , wherein the first section comprises a single crystal. 11. The method of claim 9 , wherein a ceramic core is included within the cavity located in the first section. 12. The method of claim 1 , further comprising: cooling an outer edge of the first portion of the cavity of the mold. 13. The method of claim 1 , wherein the mold is constructed from ceramic material. 14. A method of creating a cast component, the method comprising: heating a mold having a cavity therein under controlled conditions such that a first portion of the cavity has a first thermal condition and a second portion of the cavity has a second thermal condition that is different than the first thermal condition; supplying a first molten metal material into the cavity of the mold such that the first molten metal material is directed to the first portion of the cavity of the mold; supplying a second molten metal material into the cavity of the mold such that the second molten metal material is directed to the second portion of the cavity of the mold; and thereafter, allowing the first molten metal material and the second molten metal material to form the cast component comprising a first section comprising a first metal material and having first grains with a first average grain size and a second section comprising a second metal material and having second grains with a second average grain size, wherein the first metal material has a different composition than the second metal material, and wherein a transition zone is provided between the first section and the second section, the transition zone having third grains with a third average grain size, wherein the third average grain size is less than the first average grain size, and wherein the third average grain size is greater than the second average grain size.
Casting heavy metals with high melting point, i.e. 1000 - 1600 degrees C, e.g. Co 1490 degrees C, Ni 1450 degrees C, Mn 1240 degrees C, Cu 1083 degrees C · CPC title
for making compound objects cast of two or more different metals, e.g. for making rolls for rolling mills (casting compound ingots B22D7/02) · CPC title
Influencing the temperature of the metal, e.g. by heating or cooling the mould · CPC title
Grain size · CPC title
Superalloys · CPC title
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