Methods for the repair of gas turbine engine components using additive manufacturing techniques
US-9174312-B2 · Nov 3, 2015 · US
US2016376996A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016376996-A1 |
| Application number | US-201514749791-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jun 25, 2015 |
| Priority date | Jun 25, 2015 |
| Publication date | Dec 29, 2016 |
| Grant date | — |
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A method for producing a device having at least one internal feature includes manufacturing an internal volume of the internal features out of a first material, disposing the internal volume in a parent material that has a higher melting point than the first material, causing the internal volume to melt within the parent material, and allowing at least a portion of the first material to diffuse into the parent material, thereby leaving behind the at least one internal feature within the parent material.
Opening claim text (preview).
What is claimed is: 1 . A method for producing a device having at least one internal feature, comprising: manufacturing an internal volume of the internal features out of a first material; disposing the internal volume in a parent material that has a higher melting point than the first material; causing the internal volume to melt within the parent material; and allowing at least a portion of the first material to diffuse into the parent material, thereby leaving behind the at least one internal feature within the parent material. 2 . The method of claim 1 , wherein the internal feature is a flow channel, the internal volume is a flow volume, and the first material is a channel material. 3 . The method of claim 2 , wherein causing the flow volume to melt includes subjecting the channel material and the parent material to at least one of cold isostatic pressing or hot isostatic pressing. 4 . The method of claim 2 , wherein manufacturing the flow volume includes additively manufacturing the flow volume. 5 . The method of claim 4 , further comprising smoothing an exterior surface of the additively manufactured flow volume. 6 . The method of claim 2 , wherein the parent material includes a powder. 7 . The method of claim 6 , wherein the powder includes at least one of a metal powder, an alloy powder, a composite powder, or a ceramic powder. 8 . The method of claim 7 , further comprising fusing the powder together after or during melting the channel material within the powder. 9 . The method of claim 2 , wherein the parent material includes at least one of a metal, metal alloy, a composite material, or a ceramic. 10 . The method of claim 9 , wherein the channel material can include at least one of BNi-2, BNi-6, NB 30, NB 150, Bni-3, MBF-60, MBF-80, DF-3, Ni—Cr—B—Si, Haynes 230 doped with B, Al, Al+SiO 2 , B 2 O 3 , or Oxynitride glass. 11 . The method of claim 2 , wherein manufacturing the flow volume includes forming the flow volume such the flow channel defines at least part of a fuel flow circuit. 12 . The method of claim 11 , further comprising shaping the parent material into a fuel nozzle for a turbomachine. 13 . A flow device, comprising: a parent material defining a flow channel; and a channel material diffused into the parent material through a wall that defines the flow channel. 14 . The flow device of claim 13 , wherein the channel material is only partially diffused into the parent material from the flow channel such that there is a portion of the parent material that includes the channel material and a portion of the parent material that does not include the channel material. 15 . The flow device of claim 13 , wherein a diffusion gradient exists such that an amount of channel material becomes greater closer to the wall that defines the flow channel. 16 . The flow device of claim 13 , wherein the flow device is a fuel nozzle and the flow channel is one or more fuel circuits. 17 . The flow device of claim 13 , wherein the parent material includes at least one of a metal, metal alloy, a composite material, or a ceramic. 18 . The flow device of claim 13 , wherein the channel material includes at least one of BNi-2, BNi-6, NB 30, NB 150, Bni-3, MBF-60, MBF-80, DF-3, Ni—Cr—B—Si, Haynes 230 doped with B, Al, Al+SiO 2 , B 2 O 3 , or Oxynitride glass. 19 . The flow device of claim 18 , wherein the wall that defines the flow channel includes a mirror finish. 20 . A method for creating a smooth finish in a flow channel of an additively manufactured fuel nozzle, comprising: manufacturing a three dimensional flow volume of the flow channel out of a channel material such that the flow volume includes a smooth outer surface; disposing the flow volume in a parent material, wherein the parent material that has a higher melting point than the channel material; causing the flow volume to melt within the parent material; and allowing at least a portion of the channel material to diffuse into the parent material, thereby leaving behind the flow channel within the parent material, wherein the flow channel includes a wall having a smoothness substantially similar to the smooth outer surface of the flow volume.
with deposition of material · CPC title
Products made by additive manufacturing · CPC title
Special casting characterised by the nature of the product (B22D15/02, B22D17/16, B22D19/00 take precedence; casting stereotype plates B41D3/00) · CPC title
by sintering · CPC title
Fuel supply systems · CPC title
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