JP2003278502A5 - - Google Patents
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- Publication number
- JP2003278502A5 JP2003278502A5 JP2002298169A JP2002298169A JP2003278502A5 JP 2003278502 A5 JP2003278502 A5 JP 2003278502A5 JP 2002298169 A JP2002298169 A JP 2002298169A JP 2002298169 A JP2002298169 A JP 2002298169A JP 2003278502 A5 JP2003278502 A5 JP 2003278502A5
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- JP
- Japan
- 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.)
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Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/976,564 US6843928B2 (en) | 2001-10-12 | 2001-10-12 | Method for removing metal cladding from airfoil substrate |
US09/976564 | 2001-10-12 |
Publications (3)
Publication Number | Publication Date |
---|---|
JP2003278502A JP2003278502A (ja) | 2003-10-02 |
JP2003278502A5 true JP2003278502A5 (ja) | 2005-11-04 |
JP4184031B2 JP4184031B2 (ja) | 2008-11-19 |
Family
ID=25524230
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2002298169A Expired - Fee Related JP4184031B2 (ja) | 2001-10-12 | 2002-10-11 | 翼形部基体から金属クラッドを除去するための方法 |
Country Status (7)
Country | Link |
---|---|
US (1) | US6843928B2 (ja) |
EP (1) | EP1302562B1 (ja) |
JP (1) | JP4184031B2 (ja) |
BR (1) | BR0204152B1 (ja) |
CA (1) | CA2406430C (ja) |
DE (1) | DE60219116T2 (ja) |
SG (1) | SG107616A1 (ja) |
Families Citing this family (49)
Publication number | Priority date | Publication date | Assignee | Title |
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US7094033B2 (en) * | 2004-01-21 | 2006-08-22 | General Electric Company | Methods and apparatus for assembling gas turbine engines |
US7754091B2 (en) * | 2004-08-31 | 2010-07-13 | World Properties, Inc. | Custom lamp from finished EL panel |
US7637721B2 (en) * | 2005-07-29 | 2009-12-29 | General Electric Company | Methods and apparatus for producing wind energy with reduced wind turbine noise |
DE102006061916A1 (de) * | 2006-12-21 | 2008-06-26 | Rolls-Royce Deutschland Ltd & Co Kg | Fanschaufel für ein Gasturbinentriebwerk |
US20080169270A1 (en) * | 2007-01-17 | 2008-07-17 | United Technologies Corporation | Method of removing a case layer from a metal alloy |
US20080210059A1 (en) * | 2007-01-30 | 2008-09-04 | Robert Adams | Graphite / titanium hammer |
US7736130B2 (en) * | 2007-07-23 | 2010-06-15 | General Electric Company | Airfoil and method for protecting airfoil leading edge |
US8236190B2 (en) * | 2008-06-13 | 2012-08-07 | United Technologies Corporation | Recast removal method |
US20110097213A1 (en) * | 2009-03-24 | 2011-04-28 | Peretti Michael W | Composite airfoils having leading edge protection made using high temperature additive manufacturing methods |
US8662834B2 (en) * | 2009-06-30 | 2014-03-04 | General Electric Company | Method for reducing tip rub loading |
CA2766534C (en) * | 2009-06-30 | 2017-12-12 | General Electric Company | Rotor blade and method for reducing tip rub loading |
US8657570B2 (en) * | 2009-06-30 | 2014-02-25 | General Electric Company | Rotor blade with reduced rub loading |
US8419374B2 (en) * | 2009-08-14 | 2013-04-16 | Hamilton Sundstrand Corporation | Gas turbine engine composite blade |
US20110052405A1 (en) * | 2009-09-02 | 2011-03-03 | United Technologies Corporation | Composite airfoil with locally reinforced tip region |
US9528382B2 (en) * | 2009-11-10 | 2016-12-27 | General Electric Company | Airfoil heat shield |
FR2954200B1 (fr) * | 2009-12-23 | 2012-03-02 | Snecma | Procede de realisation d'un renfort metallique d'aube de turbomachine |
DE102010006384A1 (de) * | 2010-01-29 | 2011-08-04 | Lufthansa Technik AG, 22335 | Reparaturverfahren für ein Verbundbauteil für ein Luftfahrzeug, Verbundbauteil für ein Luftfahrzeug und Einrichtung zur Reparatur eines Verbundbauteiles für ein Luftfahrzeug |
US20110194941A1 (en) * | 2010-02-05 | 2011-08-11 | United Technologies Corporation | Co-cured sheath for composite blade |
US9157327B2 (en) * | 2010-02-26 | 2015-10-13 | United Technologies Corporation | Hybrid metal fan blade |
US9650897B2 (en) | 2010-02-26 | 2017-05-16 | United Technologies Corporation | Hybrid metal fan blade |
JP5614131B2 (ja) * | 2010-07-01 | 2014-10-29 | 株式会社Ihi | ファン動翼及びファン |
GB201011228D0 (en) | 2010-07-05 | 2010-08-18 | Rolls Royce Plc | A composite turbomachine blade |
WO2012008452A1 (ja) * | 2010-07-15 | 2012-01-19 | 株式会社Ihi | ファン動翼、及び、ファン |
US8449784B2 (en) * | 2010-12-21 | 2013-05-28 | United Technologies Corporation | Method for securing a sheath to a blade |
FR2970197B1 (fr) | 2011-01-11 | 2013-12-20 | Snecma | Procede de desolidarisation/solidarisation par induction d'une piece mecanique magnetique collee a une piece mecanique. |
CH705171A1 (de) * | 2011-06-21 | 2012-12-31 | Alstom Technology Ltd | Turbinenschaufel mit einem Schaufelblatt aus Verbundwerkstoff und Verfahren zum Herstellen davon. |
US9121294B2 (en) * | 2011-12-20 | 2015-09-01 | General Electric Company | Fan blade with composite core and wavy wall trailing edge cladding |
JP2013155723A (ja) * | 2012-01-31 | 2013-08-15 | Mitsubishi Heavy Ind Ltd | 風車回転翼及びこれを備えた風力発電装置 |
US9752441B2 (en) | 2012-01-31 | 2017-09-05 | United Technologies Corporation | Gas turbine rotary blade with tip insert |
FR2991710B1 (fr) * | 2012-06-06 | 2018-06-01 | Safran Aircraft Engines | Aube de turbomachine comportant un insert recouvrant le bord de fuite |
SG11201408363XA (en) * | 2012-06-21 | 2015-01-29 | United Technologies Corp | Hybrid metal fan blade |
US20140064937A1 (en) * | 2012-06-29 | 2014-03-06 | General Electric Company | Fan blade brush tip |
US10385703B2 (en) * | 2013-03-08 | 2019-08-20 | United Technologies Corporation | Fan blades with protective sheaths and galvanic shields |
US20140259667A1 (en) * | 2013-03-13 | 2014-09-18 | James Witt | System, kit and method for surface repair and reconditioning of industrial sized fan blades such as incorporated into a cooling tower |
WO2014204573A1 (en) * | 2013-06-17 | 2014-12-24 | United Technologies Corporation | Composite airfoil bonded to a metallic root |
WO2015034612A1 (en) * | 2013-09-09 | 2015-03-12 | United Technologies Corporation | Fan blades and manufacture methods |
US10487843B2 (en) * | 2013-09-09 | 2019-11-26 | United Technologies Corporation | Fan blades and manufacture methods |
WO2015041841A1 (en) | 2013-09-17 | 2015-03-26 | United Technologies Corporation | Aluminum airfoil with titanium coating |
JP6278191B2 (ja) * | 2014-04-07 | 2018-02-14 | 株式会社Ihi | 複合材翼及び複合材翼の製造方法 |
FR3025127B1 (fr) * | 2014-08-28 | 2017-03-17 | Snecma | Reparation d'un assemblage comprenant un corps principal et un renfort |
US10465703B2 (en) | 2016-04-11 | 2019-11-05 | United Technologies Corporation | Airfoil |
WO2018146862A1 (ja) * | 2017-02-08 | 2018-08-16 | 株式会社Ihi | ファンブレード |
GB201702698D0 (en) * | 2017-02-20 | 2017-04-05 | Rolls Royce Plc | Fan |
US20190368361A1 (en) * | 2018-06-05 | 2019-12-05 | General Electric Company | Non-symmetric fan blade tip cladding |
CN109185226B (zh) * | 2018-10-24 | 2024-06-11 | 佛山市启正电气有限公司 | 吊扇及其扇叶 |
US20200157953A1 (en) * | 2018-11-20 | 2020-05-21 | General Electric Company | Composite fan blade with abrasive tip |
US11136673B2 (en) * | 2019-02-08 | 2021-10-05 | The Boeing Company | Method of surface micro-texturing with a subtractive agent |
US11142830B2 (en) | 2019-02-08 | 2021-10-12 | The Boeing Company | Method of surface micro-texturing with a subtractive agent |
US11441545B2 (en) * | 2020-02-25 | 2022-09-13 | General Electric Company | Tungsten-based erosion-resistant leading edge protection cap for rotor blades |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4006999A (en) | 1975-07-17 | 1977-02-08 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Leading edge protection for composite blades |
DE2705225C2 (de) * | 1976-06-07 | 1983-03-24 | Nobuo Tokyo Nishida | Ornamentteil für Uhren usw. |
USRE31605E (en) * | 1979-06-20 | 1984-06-19 | United Technologies Corporation | Method and apparatus for electrochemically finishing airfoil edges |
US4353780A (en) | 1980-10-01 | 1982-10-12 | United Technologies Corporation | Chemical milling of high tungsten content superalloys |
US4411730A (en) | 1980-10-01 | 1983-10-25 | United Technologies Corporation | Selective chemical milling of recast surfaces |
US4339282A (en) * | 1981-06-03 | 1982-07-13 | United Technologies Corporation | Method and composition for removing aluminide coatings from nickel superalloys |
US4534823A (en) | 1983-12-05 | 1985-08-13 | United Technologies Corporation | Chemical milling IN-100 nickel superalloy |
US4563239A (en) | 1984-10-16 | 1986-01-07 | United Technologies Corporation | Chemical milling using an inert particulate and moving vessel |
US4900398A (en) | 1989-06-19 | 1990-02-13 | General Motors Corporation | Chemical milling of titanium |
US5126005A (en) | 1990-08-31 | 1992-06-30 | The Boeing Company | Process for eliminating pits during chemical milling |
US5102499A (en) | 1991-01-07 | 1992-04-07 | United Technologies Corporation | Hydrogen embrittlement reduction in chemical milling |
US5100500A (en) | 1991-02-08 | 1992-03-31 | Aluminum Company Of America | Milling solution and method |
US5215624A (en) | 1991-02-08 | 1993-06-01 | Aluminum Company Of America | Milling solution and method |
US5248386A (en) | 1991-02-08 | 1993-09-28 | Aluminum Company Of America | Milling solution and method |
US5197191A (en) | 1991-03-04 | 1993-03-30 | General Electric Company | Repair of airfoil edges |
GB9116332D0 (en) * | 1991-07-29 | 1991-09-11 | Diffusion Alloys Ltd | Refurbishing of corroded superalloy or heat resistant steel parts and parts so refurbished |
GB2293631B (en) | 1994-09-30 | 1998-09-09 | Gen Electric | Composite fan blade trailing edge reinforcement |
US5705082A (en) * | 1995-01-26 | 1998-01-06 | Chromalloy Gas Turbine Corporation | Roughening of metal surfaces |
US5655883A (en) | 1995-09-25 | 1997-08-12 | General Electric Company | Hybrid blade for a gas turbine |
US5695659A (en) * | 1995-11-27 | 1997-12-09 | United Technologies Corporation | Process for removing a protective coating from a surface of an airfoil |
US5685917A (en) * | 1995-12-26 | 1997-11-11 | General Electric Company | Method for cleaning cracks and surfaces of airfoils |
JPH11107780A (ja) * | 1997-10-02 | 1999-04-20 | Toshiba Corp | ガスタービン部品のコーティングの除去方法 |
US5944909A (en) | 1998-02-02 | 1999-08-31 | General Electric Company | Method for chemically stripping a cobalt-base substrate |
US5960249A (en) * | 1998-03-06 | 1999-09-28 | General Electric Company | Method of forming high-temperature components and components formed thereby |
US6833328B1 (en) | 2000-06-09 | 2004-12-21 | General Electric Company | Method for removing a coating from a substrate, and related compositions |
US6413051B1 (en) | 2000-10-30 | 2002-07-02 | General Electric Company | Article including a composite laminated end portion with a discrete end barrier and method for making and repairing |
-
2001
- 2001-10-12 US US09/976,564 patent/US6843928B2/en not_active Expired - Lifetime
-
2002
- 2002-10-03 CA CA002406430A patent/CA2406430C/en not_active Expired - Fee Related
- 2002-10-10 SG SG200206208A patent/SG107616A1/en unknown
- 2002-10-10 DE DE60219116T patent/DE60219116T2/de not_active Expired - Lifetime
- 2002-10-10 EP EP02257058A patent/EP1302562B1/en not_active Expired - Fee Related
- 2002-10-11 JP JP2002298169A patent/JP4184031B2/ja not_active Expired - Fee Related
- 2002-10-11 BR BRPI0204152-9A patent/BR0204152B1/pt not_active IP Right Cessation