DE60128645D1 - Rotor-Schaufelblatt-Zusammenbau - Google Patents
Rotor-Schaufelblatt-ZusammenbauInfo
- Publication number
- DE60128645D1 DE60128645D1 DE60128645T DE60128645T DE60128645D1 DE 60128645 D1 DE60128645 D1 DE 60128645D1 DE 60128645 T DE60128645 T DE 60128645T DE 60128645 T DE60128645 T DE 60128645T DE 60128645 D1 DE60128645 D1 DE 60128645D1
- Authority
- DE
- Germany
- Prior art keywords
- rotor
- blade
- assembly
- 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.)
- Expired - Lifetime
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US746255 | 1996-11-07 | ||
US09/746,255 US6439851B1 (en) | 2000-12-21 | 2000-12-21 | Reduced stress rotor blade and disk assembly |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60128645D1 true DE60128645D1 (de) | 2007-07-12 |
DE60128645T2 DE60128645T2 (de) | 2007-09-20 |
Family
ID=25000063
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60138579T Expired - Lifetime DE60138579D1 (de) | 2000-12-21 | 2001-12-19 | Beschaufelte Rotoranordnung |
DE60128645T Expired - Lifetime DE60128645T2 (de) | 2000-12-21 | 2001-12-19 | Rotor-Schaufelblatt-Zusammenbau |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60138579T Expired - Lifetime DE60138579D1 (de) | 2000-12-21 | 2001-12-19 | Beschaufelte Rotoranordnung |
Country Status (4)
Country | Link |
---|---|
US (1) | US6439851B1 (de) |
EP (2) | EP1813771B1 (de) |
JP (1) | JP4101508B2 (de) |
DE (2) | DE60138579D1 (de) |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6769877B2 (en) | 2002-10-18 | 2004-08-03 | General Electric Company | Undercut leading edge for compressor blades and related method |
US6902376B2 (en) * | 2002-12-26 | 2005-06-07 | General Electric Company | Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge |
US7121803B2 (en) * | 2002-12-26 | 2006-10-17 | General Electric Company | Compressor blade with dovetail slotted to reduce stress on the airfoil leading edge |
GB0302116D0 (en) * | 2003-01-30 | 2003-03-05 | Rolls Royce Plc | A rotor |
SE526255C2 (sv) * | 2003-03-14 | 2005-08-09 | Sandvik Intellectual Property | Verktyg och indexerbart skär för finsvarvning av rotationssymmetriska spår i arbetsstycken |
US7156621B2 (en) * | 2004-05-14 | 2007-01-02 | Pratt & Whitney Canada Corp. | Blade fixing relief mismatch |
JP4869616B2 (ja) * | 2005-04-01 | 2012-02-08 | 株式会社日立製作所 | 蒸気タービン動翼と蒸気タービンロータ及びそれを用いた蒸気タービン並びにその発電プラント |
US20060251522A1 (en) * | 2005-05-05 | 2006-11-09 | Matheny Alfred P | Curved blade and vane attachment |
WO2006124617A2 (en) * | 2005-05-12 | 2006-11-23 | General Electric Company | BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION (9FA+e, STAGE 1) |
WO2006124618A1 (en) * | 2005-05-12 | 2006-11-23 | General Electric Company | BLADE/DISK DOVETAIL BACKCUT FOR BLADE/DISK STRESS REDUCTION (6FA AND 6FA+e, STAGE 1) |
EP1882084A4 (de) * | 2005-05-12 | 2013-06-26 | Gen Electric | Stutzung der zinken einer schaufel oder einer scheibe zur reduktion der belastung der schaufel bzw. der scheibe (9fa+e, stufe 2) |
JP4870754B2 (ja) * | 2005-05-12 | 2012-02-08 | ゼネラル・エレクトリック・カンパニイ | 動翼/ディスク(7FA+e、第2段)の応力を低減するための動翼/ディスクダブテールバックカット |
WO2006124615A1 (en) * | 2005-05-16 | 2006-11-23 | General Electric Company | Blade/disk dovetail backcut for blade/disk stress reduction (7fa+e, stage 1) |
GB0521242D0 (en) * | 2005-10-19 | 2005-11-23 | Rolls Royce Plc | A blade mounting |
FR2900989B1 (fr) * | 2006-05-12 | 2008-07-11 | Snecma Sa | Ensemble pour compresseur de moteur d'aeronef comprenant des aubes a attache marteau a pied incline |
EP2019913A4 (de) * | 2006-05-12 | 2011-06-01 | Gen Electric | Schaufel/scheiben-schwalbenschwanzhinterschnitt für schaufel/scheiben-spannungsreduzierung (6fa+e, stufe 2) |
US7476085B2 (en) * | 2006-05-12 | 2009-01-13 | General Electric Company | Blade/disk dovetail backcut for blade/disk stress reduction (6FA+E, stage2) |
US20080101938A1 (en) * | 2006-10-26 | 2008-05-01 | General Electric | Blade/disk dovetail backcut for blade/disk stress reduction (7FA, stage 1) |
US20080101937A1 (en) * | 2006-10-26 | 2008-05-01 | General Electric | Blade/disk dovetail backcut for blade/disk stress reduction (9FA, stage 1) |
US20080101939A1 (en) * | 2006-10-26 | 2008-05-01 | General Electric | Blade/disk dovetail backcut for blade/disk stress reduction (7FA, stage 2) |
US7927069B2 (en) * | 2006-11-13 | 2011-04-19 | United Technologies Corporation | Hoop seal with partial slot geometry |
US20130333173A1 (en) * | 2012-06-15 | 2013-12-19 | Mitsubishi Heavy Industries, Ltd. | Blade root spring insertion jig and insertion method of blade root spring |
US9366145B2 (en) * | 2012-08-24 | 2016-06-14 | United Technologies Corporation | Turbine engine rotor assembly |
US9739159B2 (en) | 2013-10-09 | 2017-08-22 | General Electric Company | Method and system for relieving turbine rotor blade dovetail stress |
JP5726261B2 (ja) * | 2013-10-18 | 2015-05-27 | 三菱重工業株式会社 | 軸流圧縮機用動翼および軸流圧縮機 |
US10260350B2 (en) * | 2014-09-05 | 2019-04-16 | United Technologies Corporation | Gas turbine engine airfoil structure |
FR3026429B1 (fr) * | 2014-09-30 | 2016-12-09 | Snecma | Aube mobile de turbomachine, comprenant un ergot engageant une entaille de blocage d'un disque de rotor |
US9896947B2 (en) * | 2014-12-15 | 2018-02-20 | United Technologies Corporation | Turbine airfoil attachment with multi-radial serration profile |
EP3034798B1 (de) * | 2014-12-18 | 2018-03-07 | Ansaldo Energia Switzerland AG | Gasturbinenschaufel |
US10371163B2 (en) | 2016-02-02 | 2019-08-06 | General Electric Company | Load absorption systems and methods |
US20170356297A1 (en) * | 2016-06-13 | 2017-12-14 | General Electric Company | Lockwire Tab Backcut For Blade Stress Reduction (9E.04) |
KR102176954B1 (ko) * | 2017-09-14 | 2020-11-10 | 두산중공업 주식회사 | 가스 터빈용 압축기 로터 디스크 |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2807436A (en) * | 1952-03-25 | 1957-09-24 | Gen Motors Corp | Turbine wheel and bucket assembly |
DE1070335B (de) * | 1955-06-24 | |||
AT287741B (de) * | 1968-10-28 | 1971-02-10 | Elin Union Ag | Sicherung für in profilierten axialen Nuten eines Turbinenrotors gehaltene Laufschaufeln gegen eine Axialverschiebung |
US4169694A (en) * | 1977-07-20 | 1979-10-02 | Electric Power Research Institute, Inc. | Ceramic rotor blade having root with double curvature |
JPS57186004A (en) * | 1981-05-13 | 1982-11-16 | Hitachi Ltd | Structure of rotor for turbo-machine |
US4480957A (en) * | 1983-04-14 | 1984-11-06 | General Electric Company | Dynamic response modification and stress reduction in dovetail and blade assembly |
US5259728A (en) * | 1992-05-08 | 1993-11-09 | General Electric Company | Bladed disk assembly |
FR2725239B1 (fr) * | 1994-09-30 | 1996-11-22 | Gec Alsthom Electromec | Disposition pour l'ecretement des pointes de contrainte dans l'ancrage d'une ailette de turbine, comportant une racine dite en "pied-sapin" |
KR20000022064A (ko) * | 1996-06-21 | 2000-04-25 | 칼 하인쯔 호르닝어 | 홈내에 삽입될 수 있는 블레이드를 갖는 터보 머신용 회전자 및회전자용 블레이드 |
DE19705323A1 (de) * | 1997-02-12 | 1998-08-27 | Siemens Ag | Reduzierung von lokalen Spannungen in Schaufelfußnuten |
US6183202B1 (en) * | 1999-04-30 | 2001-02-06 | General Electric Company | Stress relieved blade support |
-
2000
- 2000-12-21 US US09/746,255 patent/US6439851B1/en not_active Expired - Lifetime
-
2001
- 2001-12-19 DE DE60138579T patent/DE60138579D1/de not_active Expired - Lifetime
- 2001-12-19 EP EP07009913A patent/EP1813771B1/de not_active Expired - Lifetime
- 2001-12-19 EP EP01310608A patent/EP1219782B1/de not_active Expired - Lifetime
- 2001-12-19 DE DE60128645T patent/DE60128645T2/de not_active Expired - Lifetime
- 2001-12-20 JP JP2001386954A patent/JP4101508B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
US6439851B1 (en) | 2002-08-27 |
EP1219782A3 (de) | 2003-10-08 |
EP1813771B1 (de) | 2009-04-29 |
EP1813771A2 (de) | 2007-08-01 |
US20020081205A1 (en) | 2002-06-27 |
JP4101508B2 (ja) | 2008-06-18 |
DE60138579D1 (de) | 2009-06-10 |
EP1219782A2 (de) | 2002-07-03 |
JP2002201910A (ja) | 2002-07-19 |
EP1813771A3 (de) | 2008-02-20 |
EP1219782B1 (de) | 2007-05-30 |
DE60128645T2 (de) | 2007-09-20 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |