JP2012102732A5 - - Google Patents
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- Publication number
- JP2012102732A5 JP2012102732A5 JP2011243087A JP2011243087A JP2012102732A5 JP 2012102732 A5 JP2012102732 A5 JP 2012102732A5 JP 2011243087 A JP2011243087 A JP 2011243087A JP 2011243087 A JP2011243087 A JP 2011243087A JP 2012102732 A5 JP2012102732 A5 JP 2012102732A5
- Authority
- JP
- Japan
- Prior art keywords
- grooves
- substrate
- coating
- component
- recessed
- 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
- 239000000758 substrate Substances 0.000 claims 18
- 239000011248 coating agent Substances 0.000 claims 17
- 238000000576 coating method Methods 0.000 claims 17
- 238000000034 method Methods 0.000 claims 10
- 238000000151 deposition Methods 0.000 claims 6
- 239000007921 spray Substances 0.000 claims 4
- 238000001816 cooling Methods 0.000 claims 3
- 239000012530 fluid Substances 0.000 claims 3
- 238000010286 high velocity air fuel Methods 0.000 claims 3
- 238000005498 polishing Methods 0.000 claims 3
- 230000008021 deposition Effects 0.000 claims 2
- 238000010285 flame spraying Methods 0.000 claims 2
- 238000007749 high velocity oxygen fuel spraying Methods 0.000 claims 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 claims 1
- 238000005266 casting Methods 0.000 claims 1
- 239000000945 filler Substances 0.000 claims 1
- 239000000446 fuel Substances 0.000 claims 1
- 238000004519 manufacturing process Methods 0.000 claims 1
- 239000002184 metal Substances 0.000 claims 1
- 229910052760 oxygen Inorganic materials 0.000 claims 1
- 239000001301 oxygen Substances 0.000 claims 1
- 239000012720 thermal barrier coating Substances 0.000 claims 1
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US12/943,624 US8387245B2 (en) | 2010-11-10 | 2010-11-10 | Components with re-entrant shaped cooling channels and methods of manufacture |
| US12/943,624 | 2010-11-10 |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2012102732A JP2012102732A (ja) | 2012-05-31 |
| JP2012102732A5 true JP2012102732A5 (enExample) | 2014-12-18 |
| JP5941266B2 JP5941266B2 (ja) | 2016-06-29 |
Family
ID=45990481
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2011243087A Active JP5941266B2 (ja) | 2010-11-10 | 2011-11-07 | 窪み形状の冷却チャネルを備える構成部品および製造方法 |
Country Status (5)
| Country | Link |
|---|---|
| US (2) | US8387245B2 (enExample) |
| JP (1) | JP5941266B2 (enExample) |
| CN (1) | CN102536332B (enExample) |
| DE (1) | DE102011055246B4 (enExample) |
| FR (1) | FR2967168B1 (enExample) |
Families Citing this family (41)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8905713B2 (en) | 2010-05-28 | 2014-12-09 | General Electric Company | Articles which include chevron film cooling holes, and related processes |
| US9249491B2 (en) * | 2010-11-10 | 2016-02-02 | General Electric Company | Components with re-entrant shaped cooling channels and methods of manufacture |
| US8673397B2 (en) | 2010-11-10 | 2014-03-18 | General Electric Company | Methods of fabricating and coating a component |
| US8387245B2 (en) * | 2010-11-10 | 2013-03-05 | General Electric Company | Components with re-entrant shaped cooling channels and methods of manufacture |
| US20120148769A1 (en) | 2010-12-13 | 2012-06-14 | General Electric Company | Method of fabricating a component using a two-layer structural coating |
| US8601691B2 (en) | 2011-04-27 | 2013-12-10 | General Electric Company | Component and methods of fabricating a coated component using multiple types of fillers |
| US20120317984A1 (en) * | 2011-06-16 | 2012-12-20 | Dierberger James A | Cell structure thermal barrier coating |
| US9216491B2 (en) | 2011-06-24 | 2015-12-22 | General Electric Company | Components with cooling channels and methods of manufacture |
| US9327384B2 (en) | 2011-06-24 | 2016-05-03 | General Electric Company | Components with cooling channels and methods of manufacture |
| US9206696B2 (en) | 2011-08-16 | 2015-12-08 | General Electric Company | Components with cooling channels and methods of manufacture |
| US9260191B2 (en) * | 2011-08-26 | 2016-02-16 | Hs Marston Aerospace Ltd. | Heat exhanger apparatus including heat transfer surfaces |
| US20130086784A1 (en) | 2011-10-06 | 2013-04-11 | General Electric Company | Repair methods for cooled components |
| US9249670B2 (en) | 2011-12-15 | 2016-02-02 | General Electric Company | Components with microchannel cooling |
| US9435208B2 (en) * | 2012-04-17 | 2016-09-06 | General Electric Company | Components with microchannel cooling |
| US9243503B2 (en) * | 2012-05-23 | 2016-01-26 | General Electric Company | Components with microchannel cooled platforms and fillets and methods of manufacture |
| DE102013109116A1 (de) * | 2012-08-27 | 2014-03-27 | General Electric Company (N.D.Ges.D. Staates New York) | Bauteil mit Kühlkanälen und Verfahren zur Herstellung |
| US8974859B2 (en) * | 2012-09-26 | 2015-03-10 | General Electric Company | Micro-channel coating deposition system and method for using the same |
| US9238265B2 (en) | 2012-09-27 | 2016-01-19 | General Electric Company | Backstrike protection during machining of cooling features |
| US20140116660A1 (en) * | 2012-10-31 | 2014-05-01 | General Electric Company | Components with asymmetric cooling channels and methods of manufacture |
| DE102013111874A1 (de) * | 2012-11-06 | 2014-05-08 | General Electric Company | Bauteil mit hinterschnitten geformten Kühlkanälen und Herstellungsverfahren dazu |
| US20140137408A1 (en) * | 2012-11-16 | 2014-05-22 | General Electric Company | Methods of fabricating and coating turbine components |
| US9297267B2 (en) | 2012-12-10 | 2016-03-29 | General Electric Company | System and method for removing heat from a turbine |
| US20160032766A1 (en) | 2013-03-14 | 2016-02-04 | General Electric Company | Components with micro cooled laser deposited material layer and methods of manufacture |
| US20140302278A1 (en) | 2013-04-09 | 2014-10-09 | General Electric Company | Components with double sided cooling features and methods of manufacture |
| EP2860358A1 (en) * | 2013-10-10 | 2015-04-15 | Alstom Technology Ltd | Arrangement for cooling a component in the hot gas path of a gas turbine |
| US9278462B2 (en) | 2013-11-20 | 2016-03-08 | General Electric Company | Backstrike protection during machining of cooling features |
| US9803939B2 (en) | 2013-11-22 | 2017-10-31 | General Electric Company | Methods for the formation and shaping of cooling channels, and related articles of manufacture |
| US9476306B2 (en) | 2013-11-26 | 2016-10-25 | General Electric Company | Components with multi-layered cooling features and methods of manufacture |
| US9897006B2 (en) * | 2015-06-15 | 2018-02-20 | General Electric Company | Hot gas path component cooling system having a particle collection chamber |
| US9828915B2 (en) * | 2015-06-15 | 2017-11-28 | General Electric Company | Hot gas path component having near wall cooling features |
| US9938899B2 (en) | 2015-06-15 | 2018-04-10 | General Electric Company | Hot gas path component having cast-in features for near wall cooling |
| US9970302B2 (en) | 2015-06-15 | 2018-05-15 | General Electric Company | Hot gas path component trailing edge having near wall cooling features |
| US10030537B2 (en) * | 2015-10-12 | 2018-07-24 | General Electric Company | Turbine nozzle with inner band and outer band cooling |
| US10731472B2 (en) * | 2016-05-10 | 2020-08-04 | General Electric Company | Airfoil with cooling circuit |
| US10458259B2 (en) | 2016-05-12 | 2019-10-29 | General Electric Company | Engine component wall with a cooling circuit |
| US10612389B2 (en) | 2016-08-16 | 2020-04-07 | General Electric Company | Engine component with porous section |
| US10508551B2 (en) | 2016-08-16 | 2019-12-17 | General Electric Company | Engine component with porous trench |
| US10767489B2 (en) | 2016-08-16 | 2020-09-08 | General Electric Company | Component for a turbine engine with a hole |
| US20180128177A1 (en) * | 2016-11-07 | 2018-05-10 | General Electric Company | Method for forming a hole in an engine component |
| EP3674518A1 (en) * | 2018-12-27 | 2020-07-01 | Siemens Aktiengesellschaft | Coolable component for a streaming engine and corresponding manufacturing method |
| CN113202566B (zh) * | 2021-04-19 | 2022-12-02 | 中国航发湖南动力机械研究所 | 涡轮导向叶片及燃气涡轮发动机 |
Family Cites Families (63)
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| US4042162A (en) * | 1975-07-11 | 1977-08-16 | General Motors Corporation | Airfoil fabrication |
| US5075966A (en) * | 1990-09-04 | 1991-12-31 | General Electric Company | Method for fabricating a hollow component for a rocket engine |
| US5640767A (en) * | 1995-01-03 | 1997-06-24 | Gen Electric | Method for making a double-wall airfoil |
| US5626462A (en) | 1995-01-03 | 1997-05-06 | General Electric Company | Double-wall airfoil |
| JP3529191B2 (ja) | 1995-04-26 | 2004-05-24 | 日本精工株式会社 | 保持器付自動調心ころ軸受と保持器付自動調心ころ軸受用保持器の製造方法 |
| US5875549A (en) * | 1997-03-17 | 1999-03-02 | Siemens Westinghouse Power Corporation | Method of forming internal passages within articles and articles formed by same |
| DE19737845C2 (de) | 1997-08-29 | 1999-12-02 | Siemens Ag | Verfahren zum Herstellen einer Gasturbinenschaufel, sowie nach dem Verfahren hergestellte Gasturbinenschaufel |
| GB2343486B (en) * | 1998-06-19 | 2000-09-20 | Rolls Royce Plc | Improvemnts in or relating to cooling systems for gas turbine engine airfoil |
| US6321449B2 (en) | 1998-11-12 | 2001-11-27 | General Electric Company | Method of forming hollow channels within a component |
| US6214248B1 (en) * | 1998-11-12 | 2001-04-10 | General Electric Company | Method of forming hollow channels within a component |
| US6086328A (en) * | 1998-12-21 | 2000-07-11 | General Electric Company | Tapered tip turbine blade |
| US6234755B1 (en) | 1999-10-04 | 2001-05-22 | General Electric Company | Method for improving the cooling effectiveness of a gaseous coolant stream, and related articles of manufacture |
| DE10024302A1 (de) | 2000-05-17 | 2001-11-22 | Alstom Power Nv | Verfahren zur Herstellung eines thermisch belasteten Gussteils |
| US6368060B1 (en) | 2000-05-23 | 2002-04-09 | General Electric Company | Shaped cooling hole for an airfoil |
| US6375425B1 (en) * | 2000-11-06 | 2002-04-23 | General Electric Company | Transpiration cooling in thermal barrier coating |
| US6617003B1 (en) | 2000-11-06 | 2003-09-09 | General Electric Company | Directly cooled thermal barrier coating system |
| US6478537B2 (en) * | 2001-02-16 | 2002-11-12 | Siemens Westinghouse Power Corporation | Pre-segmented squealer tip for turbine blades |
| US6551061B2 (en) | 2001-03-27 | 2003-04-22 | General Electric Company | Process for forming micro cooling channels inside a thermal barrier coating system without masking material |
| US6851627B2 (en) * | 2001-07-31 | 2005-02-08 | Flow International Corporation | Multiple segment high pressure fluidjet nozzle and method of making the nozzle |
| US6602053B2 (en) | 2001-08-02 | 2003-08-05 | Siemens Westinghouse Power Corporation | Cooling structure and method of manufacturing the same |
| EP1295970A1 (en) | 2001-09-22 | 2003-03-26 | ALSTOM (Switzerland) Ltd | MCrAlY type alloy coating |
| EP1295969A1 (en) | 2001-09-22 | 2003-03-26 | ALSTOM (Switzerland) Ltd | Method of growing a MCrAIY-coating and an article coated with the MCrAIY-coating |
| US6726444B2 (en) * | 2002-03-18 | 2004-04-27 | General Electric Company | Hybrid high temperature articles and method of making |
| US6921014B2 (en) | 2002-05-07 | 2005-07-26 | General Electric Company | Method for forming a channel on the surface of a metal substrate |
| EP1387040B1 (en) | 2002-08-02 | 2006-12-06 | ALSTOM Technology Ltd | Method of protecting partial areas of a component |
| EP1462613A1 (de) | 2003-03-26 | 2004-09-29 | Siemens Aktiengesellschaft | Kühlbares Schichtsystem |
| US6981906B2 (en) * | 2003-06-23 | 2006-01-03 | Flow International Corporation | Methods and apparatus for milling grooves with abrasive fluidjets |
| US7351290B2 (en) | 2003-07-17 | 2008-04-01 | General Electric Company | Robotic pen |
| US6905302B2 (en) | 2003-09-17 | 2005-06-14 | General Electric Company | Network cooled coated wall |
| US7186167B2 (en) | 2004-04-15 | 2007-03-06 | United Technologies Corporation | Suspended abrasive waterjet hole drilling system and method |
| US7302990B2 (en) * | 2004-05-06 | 2007-12-04 | General Electric Company | Method of forming concavities in the surface of a metal component, and related processes and articles |
| US7186091B2 (en) * | 2004-11-09 | 2007-03-06 | General Electric Company | Methods and apparatus for cooling gas turbine engine components |
| US7247002B2 (en) * | 2004-12-02 | 2007-07-24 | Siemens Power Generation, Inc. | Lamellate CMC structure with interlock to metallic support structure |
| EP1828544B1 (de) * | 2004-12-24 | 2011-06-22 | Alstom Technology Ltd | Verfahren zur herstellung eines bauteils mit eingebettetem kanal sowie bauteil |
| EP1712739A1 (de) * | 2005-04-12 | 2006-10-18 | Siemens Aktiengesellschaft | Bauteil mit Filmkühlloch |
| US7625180B1 (en) | 2006-11-16 | 2009-12-01 | Florida Turbine Technologies, Inc. | Turbine blade with near-wall multi-metering and diffusion cooling circuit |
| US7879203B2 (en) | 2006-12-11 | 2011-02-01 | General Electric Company | Method and apparatus for cathodic arc ion plasma deposition |
| US7766617B1 (en) * | 2007-03-06 | 2010-08-03 | Florida Turbine Technologies, Inc. | Transpiration cooled turbine airfoil |
| US7900458B2 (en) | 2007-05-29 | 2011-03-08 | Siemens Energy, Inc. | Turbine airfoils with near surface cooling passages and method of making same |
| US8857055B2 (en) | 2010-01-29 | 2014-10-14 | General Electric Company | Process and system for forming shaped air holes |
| US8905713B2 (en) | 2010-05-28 | 2014-12-09 | General Electric Company | Articles which include chevron film cooling holes, and related processes |
| US8673397B2 (en) | 2010-11-10 | 2014-03-18 | General Electric Company | Methods of fabricating and coating a component |
| US9249491B2 (en) * | 2010-11-10 | 2016-02-02 | General Electric Company | Components with re-entrant shaped cooling channels and methods of manufacture |
| US8387245B2 (en) * | 2010-11-10 | 2013-03-05 | General Electric Company | Components with re-entrant shaped cooling channels and methods of manufacture |
| US8727727B2 (en) * | 2010-12-10 | 2014-05-20 | General Electric Company | Components with cooling channels and methods of manufacture |
| US20120148769A1 (en) * | 2010-12-13 | 2012-06-14 | General Electric Company | Method of fabricating a component using a two-layer structural coating |
| US8753071B2 (en) * | 2010-12-22 | 2014-06-17 | General Electric Company | Cooling channel systems for high-temperature components covered by coatings, and related processes |
| US8533949B2 (en) * | 2011-02-14 | 2013-09-17 | General Electric Company | Methods of manufacture for components with cooling channels |
| US20120243995A1 (en) * | 2011-03-21 | 2012-09-27 | General Electric Company | Components with cooling channels formed in coating and methods of manufacture |
| US8601691B2 (en) * | 2011-04-27 | 2013-12-10 | General Electric Company | Component and methods of fabricating a coated component using multiple types of fillers |
| US9216491B2 (en) * | 2011-06-24 | 2015-12-22 | General Electric Company | Components with cooling channels and methods of manufacture |
| US9327384B2 (en) * | 2011-06-24 | 2016-05-03 | General Electric Company | Components with cooling channels and methods of manufacture |
| US9206696B2 (en) * | 2011-08-16 | 2015-12-08 | General Electric Company | Components with cooling channels and methods of manufacture |
| US9249672B2 (en) * | 2011-09-23 | 2016-02-02 | General Electric Company | Components with cooling channels and methods of manufacture |
| US20130078418A1 (en) * | 2011-09-23 | 2013-03-28 | General Electric Company | Components with cooling channels and methods of manufacture |
| US20130086784A1 (en) * | 2011-10-06 | 2013-04-11 | General Electric Company | Repair methods for cooled components |
| US20130101761A1 (en) * | 2011-10-21 | 2013-04-25 | General Electric Company | Components with laser cladding and methods of manufacture |
| US9435208B2 (en) * | 2012-04-17 | 2016-09-06 | General Electric Company | Components with microchannel cooling |
| US9243503B2 (en) * | 2012-05-23 | 2016-01-26 | General Electric Company | Components with microchannel cooled platforms and fillets and methods of manufacture |
| US8974859B2 (en) * | 2012-09-26 | 2015-03-10 | General Electric Company | Micro-channel coating deposition system and method for using the same |
| US9200521B2 (en) * | 2012-10-30 | 2015-12-01 | General Electric Company | Components with micro cooled coating layer and methods of manufacture |
| US20140116660A1 (en) * | 2012-10-31 | 2014-05-01 | General Electric Company | Components with asymmetric cooling channels and methods of manufacture |
| US20140302278A1 (en) * | 2013-04-09 | 2014-10-09 | General Electric Company | Components with double sided cooling features and methods of manufacture |
-
2010
- 2010-11-10 US US12/943,624 patent/US8387245B2/en active Active
-
2011
- 2011-11-07 JP JP2011243087A patent/JP5941266B2/ja active Active
- 2011-11-09 FR FR1160220A patent/FR2967168B1/fr not_active Expired - Fee Related
- 2011-11-10 CN CN201110373806.1A patent/CN102536332B/zh not_active Expired - Fee Related
- 2011-11-10 DE DE102011055246.4A patent/DE102011055246B4/de active Active
-
2013
- 2013-01-30 US US13/753,828 patent/US20130140007A1/en not_active Abandoned
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