Flow body for a gas turbine, gas turbine, method for manufacturing a flow body for a gas turbine, and method for repairing a flow body of a gas turbine
US-2024376825-A1 · Nov 14, 2024 · US
US10124408B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10124408-B2 |
| Application number | US-201314440154-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 1, 2013 |
| Priority date | Nov 1, 2012 |
| Publication date | Nov 13, 2018 |
| Grant date | Nov 13, 2018 |
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A method and apparatus for fabricating an object. The method and apparatus entail applying a pulsed laser energy to a first quantity of a powder material on a substrate so as to fuse particles of the powder material into a first layer on the substrate, and then forming at least one additional layer on the first layer by applying a pulsed laser energy to at least a second quantity of the powder material on the first layer so as to fuse particles of the powder material into the at least one additional layer on the first layer. The pulsed laser energy is applied in a controlled manner such that solidification dynamics of the first and second quantities of the powder material are altered to promote at least one microstructural characteristic of the first and additional layer.
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What is claimed is: 1. An additive manufacturing method of fabricating an object, the method comprising: applying a pulsed laser energy to a first quantity of a powder material on a substrate to fuse particles of the powder material into a first layer on the substrate; forming at least one additional layer on the first layer by applying a pulsed laser energy to at least a second quantity of the powder material on the first layer to fuse particles of the powder material into the at least one additional layer on the first layer; applying the pulsed laser energy in a controlled manner such that solidification dynamics of the first and second quantities of the powder material are altered to promote at least one microstructural characteristic of the object comprising the first layer and the at least one additional layer, wherein the controlled manner of applying the pulsed laser energy reduces at least one microstructural defect in the first layer and the at least one additional layer, the at least one microstructural defect consisting of microcracks; cooling the first and second quantities of powder at a rate of at least 2.0×10^7 Kelvin/second, wherein the cooled first and second quantities of powder form a metallic glass having a disordered atomic-scale structure, the metallic glass comprising; an alloy of at least two elements; a first element comprising between 45-70 atomic percent iron; and one or more glass to crystalline transition regions, the one or more glass to crystalline transition regions forming at temperatures in the range between about 410° C. to about 500° C. 2. The additive manufacturing method of claim 1 , wherein the controlled manner of applying the pulsed laser energy causes the first and second quantities of the powder material to fully melt. 3. An additive manufacturing method of fabricating an object, the method comprising: applying a pulsed laser energy to a first quantity of a powder material on a substrate to fuse particles of the powder material into a first layer on the substrate; forming at least one additional layer on the first layer by applying a pulsed laser energy to at least a second quantity of the powder material on the first layer to fuse particles of the powder material into the at least one additional layer on the first layer; and applying the pulsed laser energy in a controlled manner such that solidification dynamics of the first and second quantities of the powder material are altered to promote at least one microstructural characteristic of the object comprising the first layer and the at least one additional layer, wherein the powder material is a metallic powder material, wherein the controlled manner of applying the pulsed laser energy causes the pulsed laser energy to have a global energy density that causes the object to be free of microcracks and porosity, wherein the global energy density is calculated with the equation: Global Energy Density= P avg /vs, where P avg is laser peak power multiplied by duty cycle, v is scan velocity, and s is hatch spacing, and wherein the controlled manner of applying the pulsed laser energy causes the global energy density to be between about 20 to about 60 J/mm 2 . 4. The additive manufacturing method of claim 3 , wherein the metallic powder material is a metal material prone to microcracking resulting from rapid solidification and localized heating. 5. The additive manufacturing method of claim 4 , wherein the controlled manner of applying the pulsed laser energy causes the pulse frequency vary between about 20 KHz to about 50 KHz, wherein the controlled manner of applying the pulsed laser energy causes the laser average power to be between about 165 W to about 350 W, wherein the controlled manner of applying the pulsed laser energy causes the duty cycle to be between about 0.5 to about 0.7, wherein the scan velocity is between about 100 mm/s to about 200 mm/s, and wherein the hatch spacing is between about 0.04 mm to about 0.1 mm. 6. The additive manufacturing method of claim 3 , wherein the metal material is selected from the group consisting of aluminum, nickel, titanium, copper, refractory metals, and alloys thereof. 7. The additive manufacturing method of claim 6 , wherein the aluminum alloy is chosen from the group consisting of 6000 and 7000 aluminum alloy series and mixtures thereof. 8. The additive manufacturing method of claim 3 , wherein the controlled manner of applying the pulsed laser energy varies the pulse frequency to be between about 20 KHz to about 50 KHz. 9. The additive manufacturing method of claim 3 , wherein the controlled manner of applying the pulsed laser energy varies the laser peak power to be between about 100 W to about 500 W. 10. The additive manufacturing method of claim 3 , wherein the controlled manner of applying the pulsed laser energy varies the duty cycle to be between about 0.5 to about 0.7. 11. The additive manufacturing method of claim 3 , wherein the scan velocity is about 100 mm/s to about 2000 mm/s and the hatch spacing is about 0.04 mm to about 0.1 mm. 12. An additive manufacturing method of fabricating an object, the method comprising: applying a pulsed laser energy to a first quantity of a powder material on a substrate to fuse particles of the powder material into a first layer on the substrate; forming at least one additional layer on the first layer by applying a pulsed laser energy to at least a second quantity of the powder material on the first layer to fuse particles of the powder material into the at least one additional layer on the first layer; applying the pulsed laser energy in a controlled manner such that solidification dynamics of the first and second quantities of the powder material are altered to promote at least one microstructural characteristic of the object comprising the first layer and the at least one additional layer, wherein the controlled manner of applying the pulsed laser energy reduces at least one microstructural defect in the first layer and the at least one additional layer, wherein the controlled manner of applying the pulsed laser energy causes the pulse frequency to be between about 20 KHz to about 50 KHz, wherein the controlled manner of applying the pulsed laser energy causes the laser average power to be between about 165 W to about 350 W, wherein the controlled manner of applying the pulsed laser energy causes the duty cycle to be between about 0.5 to about 0.7, wherein the scan velocity is between about 100 mm/s to about 200 mm/s, and wherein the hatch spacing is between about 0.04 mm to about 0.1 mm.
pulsed; frequency modulated · CPC title
Scanning parameters, e.g. hatch distance or scanning strategy · CPC title
characterised by the type, e.g. laser or electron beam · CPC title
Apparatus for additive manufacturing; Details thereof or accessories therefor · CPC title
for controlling or regulating additive manufacturing processes · CPC title
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