JP2007177789A5 - - Google Patents
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- Publication number
- JP2007177789A5 JP2007177789A5 JP2006342206A JP2006342206A JP2007177789A5 JP 2007177789 A5 JP2007177789 A5 JP 2007177789A5 JP 2006342206 A JP2006342206 A JP 2006342206A JP 2006342206 A JP2006342206 A JP 2006342206A JP 2007177789 A5 JP2007177789 A5 JP 2007177789A5
- Authority
- JP
- Japan
- Prior art keywords
- nozzle segment
- coating
- weight
- nozzle
- resistant coating
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000000034 method Methods 0.000 claims 11
- 239000011248 coating agent Substances 0.000 claims 10
- 238000000576 coating method Methods 0.000 claims 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims 4
- 230000007613 environmental effect Effects 0.000 claims 4
- 238000000151 deposition Methods 0.000 claims 3
- 230000003647 oxidation Effects 0.000 claims 3
- 238000007254 oxidation reaction Methods 0.000 claims 3
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims 2
- QCWXUUIWCKQGHC-UHFFFAOYSA-N Zirconium Chemical compound [Zr] QCWXUUIWCKQGHC-UHFFFAOYSA-N 0.000 claims 2
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims 2
- 229910052782 aluminium Inorganic materials 0.000 claims 2
- 229910052796 boron Inorganic materials 0.000 claims 2
- 229910052799 carbon Inorganic materials 0.000 claims 2
- 229910052804 chromium Inorganic materials 0.000 claims 2
- 239000011651 chromium Substances 0.000 claims 2
- 239000010941 cobalt Substances 0.000 claims 2
- 229910017052 cobalt Inorganic materials 0.000 claims 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 claims 2
- 239000007789 gas Substances 0.000 claims 2
- 229910052735 hafnium Inorganic materials 0.000 claims 2
- VBJZVLUMGGDVMO-UHFFFAOYSA-N hafnium atom Chemical compound [Hf] VBJZVLUMGGDVMO-UHFFFAOYSA-N 0.000 claims 2
- 239000000203 mixture Substances 0.000 claims 2
- 229910052759 nickel Inorganic materials 0.000 claims 2
- 239000000843 powder Substances 0.000 claims 2
- 229910052715 tantalum Inorganic materials 0.000 claims 2
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 claims 2
- 229910052726 zirconium Inorganic materials 0.000 claims 2
- 229910000951 Aluminide Inorganic materials 0.000 claims 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims 1
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 claims 1
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims 1
- 238000000429 assembly Methods 0.000 claims 1
- 230000000712 assembly Effects 0.000 claims 1
- 238000005266 casting Methods 0.000 claims 1
- 238000010276 construction Methods 0.000 claims 1
- 238000001816 cooling Methods 0.000 claims 1
- 230000008021 deposition Effects 0.000 claims 1
- 238000009792 diffusion process Methods 0.000 claims 1
- 238000005553 drilling Methods 0.000 claims 1
- 238000009499 grossing Methods 0.000 claims 1
- 239000012535 impurity Substances 0.000 claims 1
- 239000011261 inert gas Substances 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
- 229910052750 molybdenum Inorganic materials 0.000 claims 1
- 239000011733 molybdenum Substances 0.000 claims 1
- 229910052758 niobium Inorganic materials 0.000 claims 1
- 239000010955 niobium Substances 0.000 claims 1
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims 1
- 229910052763 palladium Inorganic materials 0.000 claims 1
- KDLHZDBZIXYQEI-UHFFFAOYSA-N palladium Substances [Pd] KDLHZDBZIXYQEI-UHFFFAOYSA-N 0.000 claims 1
- 239000002245 particle Substances 0.000 claims 1
- 238000007750 plasma spraying Methods 0.000 claims 1
- 238000005498 polishing Methods 0.000 claims 1
- 229910052702 rhenium Inorganic materials 0.000 claims 1
- WUAPFZMCVAUBPE-UHFFFAOYSA-N rhenium atom Chemical compound [Re] WUAPFZMCVAUBPE-UHFFFAOYSA-N 0.000 claims 1
- 238000005480 shot peening Methods 0.000 claims 1
- 229910052710 silicon Inorganic materials 0.000 claims 1
- 239000010703 silicon Substances 0.000 claims 1
- 229910000601 superalloy Inorganic materials 0.000 claims 1
- 230000003746 surface roughness Effects 0.000 claims 1
- 239000012720 thermal barrier coating Substances 0.000 claims 1
- 238000007751 thermal spraying Methods 0.000 claims 1
- 239000010936 titanium Substances 0.000 claims 1
- 229910052719 titanium Inorganic materials 0.000 claims 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 claims 1
- 229910052721 tungsten Inorganic materials 0.000 claims 1
- 239000010937 tungsten Substances 0.000 claims 1
- 229910052727 yttrium Inorganic materials 0.000 claims 1
- VWQVUPCCIRVNHF-UHFFFAOYSA-N yttrium atom Chemical compound [Y] VWQVUPCCIRVNHF-UHFFFAOYSA-N 0.000 claims 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US11/306,221 US7341427B2 (en) | 2005-12-20 | 2005-12-20 | Gas turbine nozzle segment and process therefor |
| US11/306,221 | 2005-12-20 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2007177789A JP2007177789A (ja) | 2007-07-12 |
| JP2007177789A5 true JP2007177789A5 (enExample) | 2010-02-04 |
| JP4748600B2 JP4748600B2 (ja) | 2011-08-17 |
Family
ID=37846143
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2006342206A Expired - Fee Related JP4748600B2 (ja) | 2005-12-20 | 2006-12-20 | ガスタービン用ノズルセグメント及びその製造方法 |
Country Status (4)
| Country | Link |
|---|---|
| US (1) | US7341427B2 (enExample) |
| EP (1) | EP1803896B1 (enExample) |
| JP (1) | JP4748600B2 (enExample) |
| DE (1) | DE602006007532D1 (enExample) |
Families Citing this family (38)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102005062303A1 (de) * | 2005-12-24 | 2007-06-28 | Rolls-Royce Deutschland Ltd & Co Kg | Verfahren und Anordnung zur Fertigbearbeitung von aus einem spröden Werkstoff gegossenen Schaufeln für ein Gasturbinentriebwerk |
| WO2007106065A1 (en) * | 2006-02-24 | 2007-09-20 | Aeromet Technologies, Inc. | Roughened coatings for gas turbine engine components |
| EP1985803A1 (de) * | 2007-04-23 | 2008-10-29 | Siemens Aktiengesellschaft | Verfahren zum Herstellen von beschichteten Turbinenlaufschaufeln |
| JP4591722B2 (ja) * | 2008-01-24 | 2010-12-01 | 信越化学工業株式会社 | セラミックス溶射部材の製造方法 |
| US20090274562A1 (en) * | 2008-05-02 | 2009-11-05 | United Technologies Corporation | Coated turbine-stage nozzle segments |
| US8157515B2 (en) * | 2008-08-01 | 2012-04-17 | General Electric Company | Split doublet power nozzle and related method |
| US8192850B2 (en) * | 2008-08-20 | 2012-06-05 | Siemens Energy, Inc. | Combustion turbine component having bond coating and associated methods |
| US8047771B2 (en) * | 2008-11-17 | 2011-11-01 | Honeywell International Inc. | Turbine nozzles and methods of manufacturing the same |
| US20100126014A1 (en) * | 2008-11-26 | 2010-05-27 | General Electric Company | Repair method for tbc coated turbine components |
| JP5210850B2 (ja) * | 2008-12-19 | 2013-06-12 | 三菱重工業株式会社 | ガスタービン翼、及びガスタービン |
| US8366386B2 (en) * | 2009-01-27 | 2013-02-05 | United Technologies Corporation | Method and assembly for gas turbine engine airfoils with protective coating |
| FR2941963B1 (fr) * | 2009-02-10 | 2011-03-04 | Snecma | Methode de fabrication d'une barriere thermique recouvrant un substrat metallique en superalliage et piece thermomecanique resultant de cette methode de fabrication |
| US20110052406A1 (en) * | 2009-08-25 | 2011-03-03 | General Electric Company | Airfoil and process for depositing an erosion-resistant coating on the airfoil |
| US20110150666A1 (en) * | 2009-12-18 | 2011-06-23 | Brian Thomas Hazel | Turbine blade |
| US10337404B2 (en) * | 2010-03-08 | 2019-07-02 | General Electric Company | Preferential cooling of gas turbine nozzles |
| RU2523185C2 (ru) * | 2010-03-23 | 2014-07-20 | Сименс Акциенгезелльшафт | Металлическое покрытие со связующим веществом с высокой температурой перехода гамма/гамма' и деталь |
| JP5147886B2 (ja) * | 2010-03-29 | 2013-02-20 | 株式会社日立製作所 | 圧縮機 |
| JP2012072705A (ja) * | 2010-09-29 | 2012-04-12 | Hitachi Ltd | ガスタービン翼の製造方法 |
| US8828214B2 (en) * | 2010-12-30 | 2014-09-09 | Rolls-Royce Corporation | System, method, and apparatus for leaching cast components |
| FR2980485B1 (fr) * | 2011-09-28 | 2014-07-04 | Snecma | Alliage a base de nickel |
| US8967973B2 (en) | 2011-10-26 | 2015-03-03 | General Electric Company | Turbine bucket platform shaping for gas temperature control and related method |
| EP2901022B1 (en) * | 2012-09-28 | 2019-04-24 | United Technologies Corporation | Turbine engine vane arrangement having a plurality of interconnected vane arrangement segments |
| WO2014076407A1 (fr) * | 2012-11-13 | 2014-05-22 | Snecma | Preforme et module d'aubes monobloc pour un carter intermediaire de turbomachine |
| US9702252B2 (en) | 2012-12-19 | 2017-07-11 | Honeywell International Inc. | Turbine nozzles with slip joints and methods for the production thereof |
| RU2627997C2 (ru) * | 2012-12-20 | 2017-08-14 | Сименс Акциенгезелльшафт | СОПЛОВОЙ СЕГМЕНТ ДЛЯ ГАЗОВОЙ ТУРБИНЫ, ПОКРЫТЫЙ ПОКРЫТИЕМ MCrAlY И НАКЛАДКАМИ ТБП |
| JP6045389B2 (ja) * | 2013-02-18 | 2016-12-14 | 三菱重工業株式会社 | タービンノズル及びその製造方法 |
| US10822980B2 (en) * | 2013-04-11 | 2020-11-03 | Raytheon Technologies Corporation | Gas turbine engine stress isolation scallop |
| US10266926B2 (en) | 2013-04-23 | 2019-04-23 | General Electric Company | Cast nickel-base alloys including iron |
| US10731482B2 (en) * | 2015-12-04 | 2020-08-04 | Raytheon Technologies Corporation | Enhanced adhesion thermal barrier coating |
| US20170307311A1 (en) * | 2016-04-26 | 2017-10-26 | United Technologies Corporation | Simple Heat Exchanger Using Super Alloy Materials for Challenging Applications |
| CN108004498A (zh) * | 2017-12-29 | 2018-05-08 | 上海英佛曼纳米科技股份有限公司 | 一种具有抗高温结瘤抗氧化耐腐蚀耐磨损涂层的高温热轧钢炉辊 |
| GB202002451D0 (en) * | 2020-02-21 | 2020-04-08 | Rolls Royce Plc | Article and method of manufacturing the same |
| US11512596B2 (en) * | 2021-03-25 | 2022-11-29 | Raytheon Technologies Corporation | Vane arc segment with flange having step |
| US11624289B2 (en) * | 2021-04-21 | 2023-04-11 | Rolls-Royce Corporation | Barrier layer and surface preparation thereof |
| EP4105449A1 (en) | 2021-06-18 | 2022-12-21 | Raytheon Technologies Corporation | Hybrid bonded configuration for blade outer airseal (boas) |
| US20230147399A1 (en) * | 2021-06-18 | 2023-05-11 | Raytheon Technologies Corporation | Joining individual turbine vanes with field assisted sintering technology (fast) |
| EP4105450A1 (en) | 2021-06-18 | 2022-12-21 | Raytheon Technologies Corporation | Passive clearance control (apcc) system produced by field assisted sintering technology (fast) |
| EP4105440A1 (en) | 2021-06-18 | 2022-12-21 | Raytheon Technologies Corporation | Hybrid superalloy article and method of manufacture thereof |
Family Cites Families (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5316866A (en) * | 1991-09-09 | 1994-05-31 | General Electric Company | Strengthened protective coatings for superalloys |
| US5236745A (en) * | 1991-09-13 | 1993-08-17 | General Electric Company | Method for increasing the cyclic spallation life of a thermal barrier coating |
| US5248240A (en) * | 1993-02-08 | 1993-09-28 | General Electric Company | Turbine stator vane assembly |
| US5636439A (en) * | 1995-05-22 | 1997-06-10 | General Electric Co. | Methods for coating and securing multi-vane nozzle segments |
| US5771577A (en) * | 1996-05-17 | 1998-06-30 | General Electric Company | Method for making a fluid cooled article with protective coating |
| US6444057B1 (en) * | 1999-05-26 | 2002-09-03 | General Electric Company | Compositions and single-crystal articles of hafnium-modified and/or zirconium-modified nickel-base superalloys |
| EP1097779B1 (en) * | 1999-11-03 | 2005-10-05 | ALSTOM Technology Ltd | Method for coating and welding stator of a gas turbine |
| US6375425B1 (en) * | 2000-11-06 | 2002-04-23 | General Electric Company | Transpiration cooling in thermal barrier coating |
| US6560870B2 (en) * | 2001-05-08 | 2003-05-13 | General Electric Company | Method for applying diffusion aluminide coating on a selective area of a turbine engine component |
| US6966956B2 (en) * | 2001-05-30 | 2005-11-22 | National Institute For Materials Science | Ni-based single crystal super alloy |
| FR2830874B1 (fr) * | 2001-10-16 | 2004-01-16 | Snecma Moteurs | Procede de protection par aluminisation de pieces metalliques de turbomachines munies de trous et cavites |
| US6905559B2 (en) * | 2002-12-06 | 2005-06-14 | General Electric Company | Nickel-base superalloy composition and its use in single-crystal articles |
| US6932568B2 (en) * | 2003-02-27 | 2005-08-23 | General Electric Company | Turbine nozzle segment cantilevered mount |
| US7343676B2 (en) * | 2004-01-29 | 2008-03-18 | United Technologies Corporation | Method of restoring dimensions of an airfoil and preform for performing same |
-
2005
- 2005-12-20 US US11/306,221 patent/US7341427B2/en not_active Expired - Fee Related
-
2006
- 2006-12-18 EP EP06126418A patent/EP1803896B1/en not_active Not-in-force
- 2006-12-18 DE DE602006007532T patent/DE602006007532D1/de active Active
- 2006-12-20 JP JP2006342206A patent/JP4748600B2/ja not_active Expired - Fee Related
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