JP2004308660A5 - - Google Patents
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- Publication number
- JP2004308660A5 JP2004308660A5 JP2004112684A JP2004112684A JP2004308660A5 JP 2004308660 A5 JP2004308660 A5 JP 2004308660A5 JP 2004112684 A JP2004112684 A JP 2004112684A JP 2004112684 A JP2004112684 A JP 2004112684A JP 2004308660 A5 JP2004308660 A5 JP 2004308660A5
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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.)
- Pending
Links
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US10/409,392 US6908285B2 (en) | 2003-04-08 | 2003-04-08 | Methods and apparatus for assembling rotatable machines |
Publications (2)
Publication Number | Publication Date |
---|---|
JP2004308660A JP2004308660A (ja) | 2004-11-04 |
JP2004308660A5 true JP2004308660A5 (ja) | 2007-05-31 |
Family
ID=32869193
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2004112684A Pending JP2004308660A (ja) | 2003-04-08 | 2004-04-07 | 回転機械を組立てるための方法及び装置 |
Country Status (4)
Country | Link |
---|---|
US (1) | US6908285B2 (ja) |
EP (1) | EP1467063A1 (ja) |
JP (1) | JP2004308660A (ja) |
CN (1) | CN100406678C (ja) |
Families Citing this family (22)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6898547B1 (en) | 2000-09-11 | 2005-05-24 | Axiam, Incorporated | Rotor assembly system and method |
GB0325215D0 (en) * | 2003-10-29 | 2003-12-03 | Rolls Royce Plc | Design of vanes for exposure to vibratory loading |
US7090464B2 (en) * | 2004-07-13 | 2006-08-15 | General Electric Company | Methods and apparatus for assembling rotatable machines |
US8180596B2 (en) * | 2004-07-13 | 2012-05-15 | General Electric Company | Methods and apparatus for assembling rotatable machines |
US7287958B2 (en) * | 2005-01-10 | 2007-10-30 | General Electric Company | Methods and apparatus for assembling rotatable machines |
US7572101B2 (en) * | 2005-02-22 | 2009-08-11 | General Electric Company | Methods and apparatus for assembling rotatable machines |
FR2886012B1 (fr) * | 2005-05-23 | 2007-07-06 | Snecma Moteurs Sa | Procede de calibrage en masse de pieces destinees a etre montees en peripherie d'un rotor |
GB0601837D0 (en) | 2006-01-31 | 2006-03-08 | Rolls Royce Plc | An aerofoil assembly and a method of manufacturing an aerofoil assembly |
US7497662B2 (en) * | 2006-07-31 | 2009-03-03 | General Electric Company | Methods and systems for assembling rotatable machines |
US7539594B2 (en) * | 2006-09-26 | 2009-05-26 | Axiam, Incorporated | Method and apparatus for geometric rotor stacking and balancing |
US8142161B2 (en) * | 2007-09-20 | 2012-03-27 | General Electric Company | Replaceable staking insert |
US7792600B2 (en) * | 2007-12-31 | 2010-09-07 | General Electric Company | System and a method for assembling a rotor stack |
US9157723B2 (en) | 2009-01-30 | 2015-10-13 | Axiam, Inc. | Absolute diameter measurement arm |
US8219353B2 (en) | 2009-01-30 | 2012-07-10 | Axiam, Inc. | Absolute diameter measurement arm |
DE102009016123B4 (de) * | 2009-04-03 | 2014-07-17 | Schenck Rotec Gmbh | Verfahren zum Zusammenbau und Bestimmen der Unwucht von Rotoren |
US8069707B2 (en) * | 2009-08-05 | 2011-12-06 | General Electric Company | Methods and apparatus for determining moment weight of rotating machine components |
GB201009216D0 (en) * | 2010-06-02 | 2010-07-21 | Rolls Royce Plc | Rotationally balancing a rotating part |
US9404367B2 (en) * | 2012-11-21 | 2016-08-02 | Solar Turbines Incorporated | Gas turbine engine compressor rotor assembly and balancing system |
US10710705B2 (en) * | 2017-06-28 | 2020-07-14 | General Electric Company | Open rotor and airfoil therefor |
FR3073045B1 (fr) * | 2017-10-26 | 2019-11-22 | Safran Aircraft Engines | Procede d'equilibrage d'un ensemble d'aubes |
US10816429B2 (en) * | 2018-12-07 | 2020-10-27 | Raytheon Technologies Corporation | Determining a moment weight of a component based on measured surface geometry/solid model of the component |
CN113323920B (zh) * | 2021-01-18 | 2023-05-09 | 中国民用航空飞行学院 | 一种发动机风扇叶片更换及风扇转子静态再平衡调整方法 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2140816A1 (de) * | 1971-08-14 | 1973-03-01 | Motoren Turbinen Union | Rotor fuer stroemungsmaschinen |
US3888601A (en) | 1974-05-23 | 1975-06-10 | Gen Electric | Turbomachine with balancing means |
US4213736A (en) | 1978-06-05 | 1980-07-22 | Innerspace Corporation | Turbomachinery and method of operation |
JPS5525555A (en) | 1978-08-12 | 1980-02-23 | Hitachi Ltd | Impeller |
GB2054058B (en) | 1979-06-16 | 1983-04-20 | Rolls Royce | Reducing rotor noise |
US4602412A (en) * | 1982-12-02 | 1986-07-29 | Westinghouse Electric Corp. | Method for assembling in a circular array turbine blades each with an integral shroud |
US4767272A (en) | 1987-10-14 | 1988-08-30 | United Technologies Corporation | Method for reducing blade tip variation of a bladed rotor |
US4971641A (en) * | 1988-11-14 | 1990-11-20 | General Electric Company | Method of making counterrotating aircraft propeller blades |
GB2245661B (en) | 1990-07-03 | 1993-12-15 | Rolls Royce Plc | Turbine balancing system |
ITTO980490A1 (it) | 1998-06-05 | 1999-12-05 | Magneti Marelli Climat Srl | Procedimento per l'assemblaggio di un elettroventilatore. |
US6290466B1 (en) | 1999-09-17 | 2001-09-18 | General Electric Company | Composite blade root attachment |
FR2842571B1 (fr) | 2002-07-17 | 2004-10-15 | Snecma Moteurs | Procede de repartition d'aubes de rotor de turbomachine |
-
2003
- 2003-04-08 US US10/409,392 patent/US6908285B2/en not_active Expired - Fee Related
-
2004
- 2004-04-07 JP JP2004112684A patent/JP2004308660A/ja active Pending
- 2004-04-08 CN CNB2004100325283A patent/CN100406678C/zh not_active Expired - Fee Related
- 2004-04-08 EP EP04252137A patent/EP1467063A1/en not_active Withdrawn