Integrated heat shield
US-9556795-B2 · Jan 31, 2017 · US
US2016003157A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016003157-A1 |
| Application number | US-201514790907-A |
| Country | US |
| Kind code | A1 |
| Filing date | Jul 2, 2015 |
| Priority date | Jul 3, 2014 |
| Publication date | Jan 7, 2016 |
| Grant date | — |
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A tube assembly is additive manufactured as one unitary piece and has a first tube that co-extends with and is surrounded by a second tube. An annular void may be defined by and located between the first and second tubes for insulating a fluid flowing through the first tube. The void may be sealed and under a negative atmospheric pressure for enhancing insulating properties.
Opening claim text (preview).
What is claimed is: 1 . A tube assembly comprising: an additive manufactured first tube; and an additive manufactured second tube connected to the first tube and manufactured as one unitary piece. 2 . The tube assembly set forth in claim 1 , wherein the first tube is surrounded by and substantially co-extends with the second tube. 3 . The tube assembly set forth in claim 1 , wherein the first tube is substantially concentric to the second tube. 4 . The tube assembly set forth in claim 2 further comprising: an additive manufactured third tube co-extending with the first tube and surrounded by the second tube with the second tube spaced radially outward from the first and third tubes. 5 . The tube assembly set forth in claim 4 , wherein the third tube is manufactured as one unitary piece to the first and second tubes. 6 . The tube assembly set forth in claim 2 , wherein the first and second tubes co-extend along a centerline having at least one bend. 7 . The tube assembly set forth in claim 2 , wherein a generally annular void is defined by and between the first and second tubes. 8 . The tube assembly set forth in claim 7 , wherein the void is sealed for thermally insulating the first tube. 9 . The tube assembly set forth in claim 8 , wherein the void is under a negative atmospheric pressure. 10 . The tube assembly set forth in claim 9 further comprising: a pressure maintenance feature attached to the second tube for maintaining the negative atmospheric pressure in the void. 11 . The tube assembly set forth in claim 7 further comprising: an additive manufactured support structure engaged between the first and second tubes. 12 . The tube assembly set forth in claim 11 , wherein the support structure is in the void. 13 . The tube assembly set forth in claim 6 , wherein the tube assembly is part of a fuel nozzle for a gas turbine engine. 14 . A tube assembly comprising: a first tube for flowing a fluid; a second tube surrounding and spaced radially outward from the first tube with an insulating void defined between the first and second tubes; a support structure engaged between the first and second tubes; and wherein the tube assembly is additive manufactured as one unitary piece. 15 . The tube assembly set forth in claim 14 , wherein the void is sealed and under a negative atmospheric pressure for thermally insulating the fluid. 16 . The tube assembly set forth in claim 14 , wherein the support structure is a plurality of pylons spaced from one-another in the void. 17 . The tube assembly set forth in claim 14 , wherein the support structure is a honeycomb engaged to the first and second tubes in the void. 18 . The tube assembly set forth in claim 14 , wherein the support structure is girder-like and engaged to the first and second tubes in the void. 19 . A method of manufacturing a tube assembly comprising the steps of: electronically modeling the tube assembly having a first tube co-extending and surrounded by a second tube; and additive manufacturing the tube assembly as one unitary piece. 20 . The method of manufacturing the tube assembly set forth in claim 18 , wherein the tube assembly is modeled into a plurality of slices each slice having a portion of the first and second tubes, and a first slice of the plurality of slices is manufactured before proceeding to the manufacture of a next successive slice of the plurality of slices.
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Direct deposition of metal particles, e.g. direct metal deposition [DMD] or laser engineered net shaping [LENS] · CPC title
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