Wind turbine blade
US-2015233345-A1 · Aug 20, 2015 · US
US11020955B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-11020955-B2 |
| Application number | US-201916704831-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 5, 2019 |
| Priority date | Dec 16, 2013 |
| Publication date | Jun 1, 2021 |
| Grant date | Jun 1, 2021 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method of method of forming or repairing a superalloy article having a columnar or equiaxed or directionally solidified or amorphous or single crystal microstructure includes emitting a plurality of laser beams from selected fibers of a diode laser fiber array corresponding to a pattern of a layer of the article onto a powder bed of the superalloy to form a melt pool; and controlling a temperature gradient and a solidification velocity of the melt pool to form the columnar or single crystal microstructure.
Opening claim text (preview).
What is claimed is: 1. A superalloy article or repair formed by a method comprising the steps of: emitting a plurality of laser beams, from first selected fibers of a diode laser fiber array, corresponding to a pattern of a first layer of the article onto a powder bed of a superalloy to form a first melt pool; distributing additional powder across the first layer; emitting a plurality of laser beams, from second selected fibers of the diode laser fiber array, corresponding to a pattern of a second layer of the article onto the powder bed to form a second melt pool over the first layer; and controlling a temperature gradient and a solidification velocity of the first and second melt pools such that each of the first and second layers has a columnar or equiaxed or directionally solidified or amorphous or single crystal microstructure, the controlling comprising controlling a decay rate of a laser energy of each of the plurality of laser beams to control a cooling period of the melt pool. 2. A superalloy article or repair according to claim 1 , wherein the columnar microstructure is dendritic. 3. A superalloy article or repair according to claim 1 , wherein grains of the microstructure have a size of 10 μm-100 μm. 4. A superalloy article or repair according to claim 1 , wherein the superalloy is a CoCrMo material. 5. A superalloy article or repair according to claim 1 , wherein the superalloy is a Ni-based superalloy. 6. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and solidification velocity comprises decreasing the laser energy at 10 W/s to provide a 1 s cooling period. 7. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and solidification velocity comprises decreasing the laser energy at 1 W/s to provide a 10 s cooling period. 8. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and solidification velocity comprises decreasing the laser energy at 0.1 W/s to provide a 100 s cooling period. 9. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and solidification velocity comprises heating a substrate that supports the powder bed and/or heating a prior layer of the article formed by solidification of a prior melt pool. 10. A superalloy article or repair according to claim 9 , wherein heating the substrate comprises heating the substrate to a temperature below the melting temperature of the substrate. 11. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and the solidification velocity comprises controlling at least one of a duration of each laser beam, a pulse energy of each diode laser, a pulse width of each diode laser, an average output power of each diode laser, an energy distribution of each laser beam, power density of each laser beam, a rate of reduction of the power of each laser beam, and/or a distance of ends of the fibers from the powder bed. 12. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and a solidification velocity comprises emitting laser beams from fibers at least adjacent to the pattern of the layer and heating the powder adjacent to the powder of the layer to control a cooling rate of the melted powder. 13. A superalloy article or repair according to claim 12 , wherein heating the powder adjacent to the powder of the layer comprises heating the powder at least one of prior to and/or during and/or after simultaneous melting of the powder of the pattern of the layer. 14. A superalloy article or repair according to claim 12 , wherein a power density of the laser beams heating the powder adjacent the pattern is in a range of from about 100 W/cm 2 to about 100,000 W/cm 2 . 15. A superalloy article or repair according to claim 1 , further comprising: moving the selected fibers and the powder bed relative to each other; and controlling the laser beams of the selected fibers during relative movement. 16. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and the solidification velocity to form the columnar or single crystal microstructure comprises controlling a cooling rate of each layer in two dimensions. 17. A superalloy article or repair according to claim 16 , wherein controlling the cooling rate of each layer in two dimensions comprises controlling a cooling rate of a layer that forms a surface layer of the article or repair to have at least one of a predetermined surface roughness and density. 18. A superalloy article or repair according to claim 1 , wherein controlling the temperature gradient and the solidification velocity comprises decreasing an output of each of the plurality of laser beams asymptotically towards a set value to control a cooling period of the melt pool. 19. A superalloy article or repair according to claim 1 , wherein the superalloy article is a turbine component. 20. A superalloy article or repair according to claim 19 , wherein the turbine component is an airfoil.
Two or more · CPC title
characterised by the configuration of the radiation means · CPC title
characterised by the type, e.g. laser or electron beam · CPC title
to achieve specific product aspects, e.g. surface smoothness, density, porosity or hollow structures · CPC title
Temperature or temperature gradient, e.g. temperature of the melt pool · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.