JP2002155702A5 - - Google Patents

Download PDF

Info

Publication number
JP2002155702A5
JP2002155702A5 JP2001225350A JP2001225350A JP2002155702A5 JP 2002155702 A5 JP2002155702 A5 JP 2002155702A5 JP 2001225350 A JP2001225350 A JP 2001225350A JP 2001225350 A JP2001225350 A JP 2001225350A JP 2002155702 A5 JP2002155702 A5 JP 2002155702A5
Authority
JP
Japan
Prior art keywords
airfoil
band
compressive stress
tip
depth
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.)
Pending
Application number
JP2001225350A
Other languages
English (en)
Japanese (ja)
Other versions
JP2002155702A (ja
Filing date
Publication date
Priority claimed from US09/627,143 external-priority patent/US6672838B1/en
Application filed filed Critical
Publication of JP2002155702A publication Critical patent/JP2002155702A/ja
Publication of JP2002155702A5 publication Critical patent/JP2002155702A5/ja
Pending legal-status Critical Current

Links

JP2001225350A 2000-07-27 2001-07-26 圧縮下にある一体の端部バンドを備える金属製物品及びその製造方法 Pending JP2002155702A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/627,143 US6672838B1 (en) 2000-07-27 2000-07-27 Method for making a metallic article with integral end band under compression
US09/627143 2000-07-27

Publications (2)

Publication Number Publication Date
JP2002155702A JP2002155702A (ja) 2002-05-31
JP2002155702A5 true JP2002155702A5 (enExample) 2008-09-11

Family

ID=24513365

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2001225350A Pending JP2002155702A (ja) 2000-07-27 2001-07-26 圧縮下にある一体の端部バンドを備える金属製物品及びその製造方法

Country Status (11)

Country Link
US (2) US6672838B1 (enExample)
EP (1) EP1175956B1 (enExample)
JP (1) JP2002155702A (enExample)
CN (1) CN100519055C (enExample)
BR (1) BR0103027B1 (enExample)
CA (1) CA2353265C (enExample)
DE (1) DE60114943T2 (enExample)
MX (1) MXPA01007587A (enExample)
MY (1) MY129152A (enExample)
RU (1) RU2281402C2 (enExample)
SG (1) SG101992A1 (enExample)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10245396A1 (de) * 2002-09-28 2004-04-15 Mtu Aero Engines Gmbh Vorrichtung und Verfahren zur Oberflächenbearbeitung von Werkstücken
FR2871399B1 (fr) * 2004-06-15 2006-09-22 Snecma Moteurs Sa Procede de reparation d'un element d'aube
US7229253B2 (en) 2004-11-30 2007-06-12 General Electric Company Fatigue-resistant components and method therefor
US7384244B2 (en) * 2004-12-16 2008-06-10 General Electric Company Fatigue-resistant components and method therefor
JPWO2006117847A1 (ja) * 2005-04-27 2008-12-18 株式会社日立製作所 マイクロガスタービン
US7217099B2 (en) * 2005-05-24 2007-05-15 General Electric Company Coated forward stub shaft dovetail slot
US20060280612A1 (en) * 2005-06-09 2006-12-14 Prevey Paul S Iii Metallic article with integral end band under compression
US7805972B2 (en) * 2005-10-12 2010-10-05 Surface Technology Holdings Ltd. Integrally bladed rotating turbo machinery and method and apparatus for achieving the same
US8024846B2 (en) * 2006-01-27 2011-09-27 General Electric Company Preparation of an article surface having a surface compressive texture
US20070281088A1 (en) * 2006-06-02 2007-12-06 United Technologies Corporation Low plasticity burnishing of coated titanium parts
US7530792B2 (en) * 2006-06-30 2009-05-12 General Electric Company Component of variable thickness having residual compressive stresses therein, and method therefor
KR20080012744A (ko) * 2006-08-03 2008-02-12 유나이티드 테크놀로지스 코포레이션 부식 코팅되는 부품의 코팅전 버니싱
US8079120B2 (en) * 2006-12-30 2011-12-20 General Electric Company Method for determining initial burnishing parameters
US8051565B2 (en) * 2006-12-30 2011-11-08 General Electric Company Method for increasing fatigue notch capability of airfoils
GB0704426D0 (en) * 2007-03-08 2007-04-18 Rolls Royce Plc Aerofoil members for a turbomachine
ES2343397B1 (es) * 2008-03-07 2011-06-13 GAMESA INNOVATION & TECHNOLOGY, S.L. Una pala de aerogenerador.
US8539659B2 (en) * 2008-04-23 2013-09-24 United Technologies Corporation Method of repairing an article
US8753065B2 (en) 2012-09-27 2014-06-17 United Technologies Corporation Method for setting a gear ratio of a fan drive gear system of a gas turbine engine
CN114292994A (zh) * 2021-12-30 2022-04-08 西北工业大学 一种薄壁叶片低塑性滚压强化方法

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB302657A (en) * 1927-12-19 1929-03-07 Gen Electric Improvements in and relating to turbine blades
GB1127157A (en) * 1966-06-13 1968-09-11 Orenda Ltd Method for improving the fatigue resistance of turbine blades
US4839245A (en) * 1985-09-30 1989-06-13 Union Carbide Corporation Zirconium nitride coated article and method for making same
SU1600899A1 (ru) * 1988-02-22 1990-10-23 Винницкий политехнический институт Способ изготовлени лопаток
DE4309176C2 (de) * 1993-03-22 1995-10-19 Siemens Ag Verfahren zum Festwalzen eines Bauteils
US5476363A (en) * 1993-10-15 1995-12-19 Charles E. Sohl Method and apparatus for reducing stress on the tips of turbine or compressor blades
US6215097B1 (en) * 1994-12-22 2001-04-10 General Electric Company On the fly laser shock peening
US5591009A (en) * 1995-01-17 1997-01-07 General Electric Company Laser shock peened gas turbine engine fan blade edges
US5620307A (en) 1995-03-06 1997-04-15 General Electric Company Laser shock peened gas turbine engine blade tip
US5531570A (en) * 1995-03-06 1996-07-02 General Electric Company Distortion control for laser shock peened gas turbine engine compressor blade edges
IL117347A (en) * 1995-03-06 1999-10-28 Gen Electric Laser shock peened gas turbine engine compressor airfoil edges
US5735044A (en) * 1995-12-12 1998-04-07 General Electric Company Laser shock peening for gas turbine engine weld repair
JP3728006B2 (ja) * 1996-03-29 2005-12-21 ゼネラル・エレクトリック・カンパニイ ガスタービン機関のファンの羽根
US5826453A (en) 1996-12-05 1998-10-27 Lambda Research, Inc. Burnishing method and apparatus for providing a layer of compressive residual stress in the surface of a workpiece
US6005219A (en) * 1997-12-18 1999-12-21 General Electric Company Ripstop laser shock peening
US5932120A (en) * 1997-12-18 1999-08-03 General Electric Company Laser shock peening using low energy laser
US5951790A (en) * 1998-06-26 1999-09-14 General Electric Company Method of monitoring and controlling laser shock peening using an in plane deflection test coupon
JP2000087897A (ja) * 1998-09-08 2000-03-28 Hitachi Ltd ガスタービンの圧縮機翼およびガスタービン

Similar Documents

Publication Publication Date Title
JP2002155702A5 (enExample)
EP1557229A3 (en) Apparatus and method for reducing operating stress in a turbine blade and the like
WO2006101644A3 (en) Ultrasonic blade with terminal end balance features
EP1634665A3 (en) Composite core for use in precision investment casting
EP1207212A3 (en) Nickel alloy composition
WO2006060434A3 (en) Weldable, crack-resistant co-based alloy
WO2008015643A3 (en) Nickel-based brazing alloy and method for brazing
WO2005007909A3 (en) Cobalt alloys, methods of making cobalt alloys, and implants and articles of manufacture made therefrom
WO2005079506A3 (en) Systemic immune activation method using nucleic acid-lipid complexes
EP1108495A3 (en) Welding material and a method of producing welded joint
RU2001121022A (ru) Металлическое изделие с выполненной за одно целое концевой полосой под сжатием и способ его изготовления
EP0816637A3 (en) Gas turbine guide vane
WO2005106061A3 (de) Eisen-chrom-aluminium-legierung
CA2353265A1 (en) Metallic article with integral end band under compression and method for making
WO2004081247A3 (de) Eisen-chrom-aluminium-legierung
WO2005018867A3 (fr) Procédé de brasage d'un alliage ti-al
CN105298547A (zh) 排气涡轮增压器的涡轮以及相关生产方法
EP1070863A3 (de) Walze bestehend aus einem Metallkern und einer weichen elastomeren Beschichtung sowie Verfahren zum Aufbringen dieser Schicht auf eine Walze
CN201269241Y (zh) 一种双金属铆钉
EP0870849A3 (en) Tool for glass molding operations and method of manufacture thereof
EP1306458A3 (en) 12Cr alloy steel for a turbine rotor
WO2000021746A8 (fr) Procede d'obtention de pieces metalliques minces, legeres et rigides
WO2006102034A3 (en) Co-based wire and method for saw tip manufacture and repair
JP2003226945A5 (enExample)
JP2006242320A5 (enExample)