PL2670953T3 - Stopka łopatki,odpowiednia łopatka, tarcza wirnika i zespół maszyny przepływowej - Google Patents
Stopka łopatki,odpowiednia łopatka, tarcza wirnika i zespół maszyny przepływowejInfo
- Publication number
- PL2670953T3 PL2670953T3 PL12734898T PL12734898T PL2670953T3 PL 2670953 T3 PL2670953 T3 PL 2670953T3 PL 12734898 T PL12734898 T PL 12734898T PL 12734898 T PL12734898 T PL 12734898T PL 2670953 T3 PL2670953 T3 PL 2670953T3
- Authority
- PL
- Poland
- Prior art keywords
- blade
- rotor disc
- turbomachine assembly
- blade root
- root
- Prior art date
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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
- F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
-
- 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
- F01D5/3023—Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP11174019A EP2546465A1 (en) | 2011-07-14 | 2011-07-14 | Blade root, corresponding blade, rotor disc, and turbomachine assembly |
EP12734898.5A EP2670953B1 (en) | 2011-07-14 | 2012-07-05 | Blade root, corresponding blade, rotor disc, and turbomachine assembly |
PCT/EP2012/063105 WO2013007587A1 (en) | 2011-07-14 | 2012-07-05 | Blade root, corresponding blade, rotor disc, and turbomachine assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
PL2670953T3 true PL2670953T3 (pl) | 2015-08-31 |
Family
ID=44583835
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PL12734898T PL2670953T3 (pl) | 2011-07-14 | 2012-07-05 | Stopka łopatki,odpowiednia łopatka, tarcza wirnika i zespół maszyny przepływowej |
Country Status (7)
Country | Link |
---|---|
US (1) | US10287898B2 (pl) |
EP (2) | EP2546465A1 (pl) |
CN (1) | CN103649467B (pl) |
ES (1) | ES2537006T3 (pl) |
PL (1) | PL2670953T3 (pl) |
RU (1) | RU2612675C2 (pl) |
WO (1) | WO2013007587A1 (pl) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3018849B1 (fr) * | 2014-03-24 | 2018-03-16 | Safran Aircraft Engines | Piece de revolution pour un rotor de turbomachine |
GB201416505D0 (en) | 2014-09-18 | 2014-11-05 | Rolls Royce Plc | Gas turbine engine |
EP3015652A1 (de) | 2014-10-28 | 2016-05-04 | Siemens Aktiengesellschaft | Laufschaufel für eine Turbine |
EP3093441B1 (en) * | 2015-05-12 | 2019-07-10 | Ansaldo Energia Switzerland AG | Turbo engine rotor comprising a blade-shaft connection, and blade for said rotor |
EP3098388A1 (de) * | 2015-05-28 | 2016-11-30 | Siemens Aktiengesellschaft | Laufschaufel für eine gasturbine |
EP3293362B1 (en) * | 2015-08-21 | 2020-07-22 | Mitsubishi Heavy Industries Compressor Corporation | Steam turbine |
CN106934087B (zh) * | 2015-12-31 | 2021-01-15 | 上海汽轮机厂有限公司 | 透平机械的叶片根部和转子轮槽的型线的优化设计方法 |
US10683765B2 (en) * | 2017-02-14 | 2020-06-16 | General Electric Company | Turbine blades having shank features and methods of fabricating the same |
US10895160B1 (en) * | 2017-04-07 | 2021-01-19 | Glenn B. Sinclair | Stress relief via unblended edge radii in blade attachments in gas turbines |
CN107143380B (zh) * | 2017-05-27 | 2019-04-02 | 中国航发湖南动力机械研究所 | 燃气涡轮盘榫槽设计方法、燃气涡轮盘及航空发动机 |
EP3425162A1 (de) * | 2017-07-07 | 2019-01-09 | Siemens Aktiengesellschaft | Turbinenschaufel und befestigungsausnehmung für eine strömungsmaschine, sowie deren herstellungsverfahren |
JP7385992B2 (ja) * | 2018-12-28 | 2023-11-24 | 川崎重工業株式会社 | 回転体の動翼およびディスク |
FR3091552B1 (fr) * | 2019-01-09 | 2021-05-21 | Safran Aircraft Engines | Alvéole de disque de rotor destiné à recevoir une aube de turbomachine |
FR3091553B1 (fr) * | 2019-01-09 | 2021-04-02 | Safran Aircraft Engines | Aube destinée à être montée sur un disque de rotor d’une turbomachine |
DE102019207620A1 (de) * | 2019-05-24 | 2020-11-26 | MTU Aero Engines AG | Laufschaufel mit Schaufelfußkontur mit in einem konkaven Konturabschnitt vorgesehenem Geradenabschnitt |
US11203944B2 (en) * | 2019-09-05 | 2021-12-21 | Raytheon Technologies Corporation | Flared fan hub slot |
DE102019219403A1 (de) * | 2019-12-12 | 2021-06-17 | MTU Aero Engines AG | Rotor für eine Strömungsmaschine und Strömungsmaschine |
USD946527S1 (en) | 2020-09-04 | 2022-03-22 | Siemens Energy Global GmbH & Co. KG | Turbine blade |
USD949793S1 (en) | 2020-09-04 | 2022-04-26 | Siemens Energy Global GmbH & Co. KG | Turbine blade |
USD949794S1 (en) | 2020-09-04 | 2022-04-26 | Siemens Energy Global GmbH & Co. KG | Turbine blade |
DE102021120876A1 (de) * | 2021-08-11 | 2023-02-16 | MTU Aero Engines AG | Schaufelfussaufnahme zum aufnehmen einer laufschaufel |
CN113915163A (zh) * | 2021-10-12 | 2022-01-11 | 浙江意动科技股份有限公司 | 一种压气机转子叶片连接结构 |
FR3128245A1 (fr) * | 2021-10-19 | 2023-04-21 | Safran Aircraft Engines | Procede de fabrication d’une piece de rotor de turbomachine comprenant des portions arrondies optimisees et piece de turbomachine correspondante |
JP7163523B1 (ja) * | 2022-03-24 | 2022-10-31 | 三菱重工業株式会社 | タービン動翼、タービン動翼組立体、ガスタービン及びガスタービンの補修方法 |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2343225A (en) | 1940-01-18 | 1944-02-29 | Youngstown Sheet And Tube Co | Method of applying protective coatings for metal |
US4191509A (en) * | 1977-12-27 | 1980-03-04 | United Technologies Corporation | Rotor blade attachment |
GB2030657B (en) * | 1978-09-30 | 1982-08-11 | Rolls Royce | Blade for gas turbine engine |
CH655547B (pl) | 1981-11-10 | 1986-04-30 | ||
JPS59113206A (ja) | 1982-12-20 | 1984-06-29 | Hitachi Ltd | タ−ボ機械のブレ−ド取付構造 |
GB2238581B (en) * | 1989-11-30 | 1994-01-12 | Rolls Royce Plc | Improved attachment of a gas turbine engine blade to a turbine rotor disc |
US5141401A (en) * | 1990-09-27 | 1992-08-25 | General Electric Company | Stress-relieved rotor blade attachment slot |
DE4435268A1 (de) | 1994-10-01 | 1996-04-04 | Abb Management Ag | Beschaufelter Rotor einer Turbomaschine |
US5474423A (en) | 1994-10-12 | 1995-12-12 | General Electric Co. | Bucket and wheel dovetail design for turbine rotors |
DE19728085A1 (de) * | 1997-07-02 | 1999-01-07 | Asea Brown Boveri | Fügeverbindung zwischen zwei Fügepartnern sowie deren Verwendung |
US6033185A (en) * | 1998-09-28 | 2000-03-07 | General Electric Company | Stress relieved dovetail |
US6183202B1 (en) | 1999-04-30 | 2001-02-06 | General Electric Company | Stress relieved blade support |
US6592330B2 (en) * | 2001-08-30 | 2003-07-15 | General Electric Company | Method and apparatus for non-parallel turbine dovetail-faces |
GB2380770B (en) * | 2001-10-13 | 2005-09-07 | Rolls Royce Plc | Indentor arrangement |
US6652237B2 (en) | 2001-10-15 | 2003-11-25 | General Electric Company | Bucket and wheel dovetail design for turbine rotors |
DE10357134A1 (de) * | 2003-12-06 | 2005-06-30 | Alstom Technology Ltd | Rotor für einen Verdichter |
JP4918806B2 (ja) | 2006-04-06 | 2012-04-18 | 株式会社日立製作所 | タービンロータ及びタービン動翼 |
US7594799B2 (en) | 2006-09-13 | 2009-09-29 | General Electric Company | Undercut fillet radius for blade dovetails |
GB2442449B (en) * | 2006-10-04 | 2008-06-11 | Rolls Royce Plc | Forming firtree profiles |
FR2911632B1 (fr) | 2007-01-18 | 2009-08-21 | Snecma Sa | Disque de rotor de soufflante de turbomachine |
US8038404B2 (en) * | 2007-07-16 | 2011-10-18 | Nuovo Pignone Holdings, S.P.A. | Steam turbine and rotating blade |
US20100068062A1 (en) | 2008-09-12 | 2010-03-18 | General Electric Company | Turbine bucket with dovetail seal and related method |
UA47583U (uk) | 2009-09-11 | 2010-02-10 | Украинская Инженерно-Педагогическая Академия | Багатоопорне хвостове з'єднання робочої лопатки турбіни з гарантованим контактом по всіх опорах |
US8834123B2 (en) | 2009-12-29 | 2014-09-16 | Rolls-Royce Corporation | Turbomachinery component |
CN102102545B (zh) | 2011-03-22 | 2013-11-27 | 东方电气集团东方汽轮机有限公司 | 半转速核电大承载枞树型叶根及轮槽结构 |
-
2011
- 2011-07-14 EP EP11174019A patent/EP2546465A1/en not_active Withdrawn
-
2012
- 2012-07-05 WO PCT/EP2012/063105 patent/WO2013007587A1/en active Application Filing
- 2012-07-05 US US14/232,661 patent/US10287898B2/en active Active
- 2012-07-05 CN CN201280034883.7A patent/CN103649467B/zh active Active
- 2012-07-05 EP EP12734898.5A patent/EP2670953B1/en active Active
- 2012-07-05 PL PL12734898T patent/PL2670953T3/pl unknown
- 2012-07-05 RU RU2014105457A patent/RU2612675C2/ru active
- 2012-07-05 ES ES12734898.5T patent/ES2537006T3/es active Active
Also Published As
Publication number | Publication date |
---|---|
EP2546465A1 (en) | 2013-01-16 |
US10287898B2 (en) | 2019-05-14 |
RU2014105457A (ru) | 2015-08-20 |
RU2612675C2 (ru) | 2017-03-13 |
EP2670953B1 (en) | 2015-03-04 |
ES2537006T3 (es) | 2015-06-01 |
US20140140852A1 (en) | 2014-05-22 |
CN103649467B (zh) | 2015-11-25 |
WO2013007587A1 (en) | 2013-01-17 |
CN103649467A (zh) | 2014-03-19 |
EP2670953A1 (en) | 2013-12-11 |
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