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
US2019054533A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2019054533-A1 |
| Application number | US-201816169290-A |
| Country | US |
| Kind code | A1 |
| Filing date | Oct 24, 2018 |
| Priority date | Nov 1, 2012 |
| Publication date | Feb 21, 2019 |
| Grant date | — |
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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.
Opening claim text (preview).
What is claimed is: 1 . An additive manufacturing apparatus, comprising: a pulsed-laser generating system; and a controller configured to: apply 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; form 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; and apply 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. 2 . The additive manufacturing apparatus 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 . The additive manufacturing apparatus of claim 1 , 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, and the at least one microstructural defect is chosen from the group consisting of microcracks and porosity. 4 . The additive manufacturing apparatus of claim 1 , wherein the powder material is a metallic powder material. 5 . The additive manufacturing apparatus of claim 4 , wherein the metallic powder material is a metal material prone to microcracking resulting from rapid solidification and localized heating. 6 . The additive manufacturing apparatus of claim 1 , 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.
Scanning parameters, e.g. hatch distance or scanning strategy · CPC title
pulsed; frequency modulated · CPC title
characterised by the type, e.g. laser or electron beam · CPC title
Processes of additive manufacturing · CPC title
Data acquisition or data processing for additive manufacturing · CPC title
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