EP2410131A3 - Rotor einer Turbomaschine - Google Patents

Rotor einer Turbomaschine Download PDF

Info

Publication number
EP2410131A3
EP2410131A3 EP11161987.0A EP11161987A EP2410131A3 EP 2410131 A3 EP2410131 A3 EP 2410131A3 EP 11161987 A EP11161987 A EP 11161987A EP 2410131 A3 EP2410131 A3 EP 2410131A3
Authority
EP
European Patent Office
Prior art keywords
rotor
coupling element
blades
immediately adjacent
blade
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.)
Granted
Application number
EP11161987.0A
Other languages
English (en)
French (fr)
Other versions
EP2410131B1 (de
EP2410131A2 (de
Inventor
Tilmann Dr. Raible
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
MAN Energy Solutions SE
Original Assignee
MAN Diesel and Turbo SE
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by MAN Diesel and Turbo SE filed Critical MAN Diesel and Turbo SE
Publication of EP2410131A2 publication Critical patent/EP2410131A2/de
Publication of EP2410131A3 publication Critical patent/EP2410131A3/de
Application granted granted Critical
Publication of EP2410131B1 publication Critical patent/EP2410131B1/de
Not-in-force legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/70—Shape
    • F05D2250/73—Shape asymmetric

Abstract

Rotor einer Turbomaschine, mit einem Rotorgrundkörper und mehreren Laufschaufeln, wobei jede Laufschaufel ein Schaufelblatt (11) und ein Koppelelementsegment(10, 10', 10") aufweist, Erfindungsgemäß ist das Koppelelementsegment (10, 10', 10") einer jeden Laufschaufel an einer ersten Seite (16) und an einer gegenüberliegenden zweiten Seite (17) derart konturiert ist, dass an der ersten Seite und an der zweiten Seite eine sich im wesentlichen in Axialrichtung erstreckende radial äußere Kante (18, 19) und eine sich im wesentlichen in Axialrichtung erstreckende radial innere Kante (20, 21) des jeweiligen Koppelelementsegments jeweils zwei durch eine Trennlinie (26, 27) voneinander getrennte Flächen begrenzen, wobei an mindestens einer Umfangsposition des Rotors zwischen zwei unmittelbar benachbarten Laufschaufeln die an unmittelbar benachbarten Seiten (16, 17) der Koppelelementsegmente (10', 10") ausgebildeten Trennlinien (26, 27) in etwa annähernd parallel zu der über die Schaufelfüße definierten Montagerichtung der Laufschaufeln am Rotorgrundkörper verlaufen, wohingegen an jeder anderen Umfangsposition zwischen zwei unmittelbar benachbarten Laufschaufeln die an unmittelbar benachbarten Seiten der Koppelelementsegmente (10, 10', 10") ausgebildeten Trennlinien (26, 27) zur Montagerichtung schräggestellt sind. (Fig. 1)
EP11161987.0A 2010-07-12 2011-04-12 Rotor einer Turbomaschine Not-in-force EP2410131B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102010031213A DE102010031213A1 (de) 2010-07-12 2010-07-12 Rotor einer Turbomaschine

Publications (3)

Publication Number Publication Date
EP2410131A2 EP2410131A2 (de) 2012-01-25
EP2410131A3 true EP2410131A3 (de) 2017-08-02
EP2410131B1 EP2410131B1 (de) 2018-08-15

Family

ID=43901478

Family Applications (1)

Application Number Title Priority Date Filing Date
EP11161987.0A Not-in-force EP2410131B1 (de) 2010-07-12 2011-04-12 Rotor einer Turbomaschine

Country Status (5)

Country Link
US (1) US8974186B2 (de)
EP (1) EP2410131B1 (de)
JP (1) JP5274625B2 (de)
CN (1) CN102330572B (de)
DE (1) DE102010031213A1 (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2869338T3 (es) * 2011-10-07 2021-10-25 MTU Aero Engines AG Anillo de refuerzo de una paleta para una turbomaquinaria
US9347326B2 (en) * 2012-11-02 2016-05-24 General Electric Company Integral cover bucket assembly
CN107615506B (zh) * 2015-05-08 2021-01-22 株式会社理光 光电转换元件
EP3297780B1 (de) 2015-05-20 2024-04-17 MAN Energy Solutions SE Verfahren zum herstellen eines rotors einer strömungsmaschine
IT201900017171A1 (it) * 2019-09-25 2021-03-25 Ge Avio Srl Protezioni delle punte delle pale di turbina desintonizzate
CN114382555A (zh) * 2020-10-16 2022-04-22 中国航发商用航空发动机有限责任公司 导叶缘板、导叶、涡轮导向器及导叶缘板的设计方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5001830A (en) * 1989-10-23 1991-03-26 Westinghouse Electric Corp. Method for assembling side entry control stage blades in a steam turbine
JPH0791206A (ja) * 1993-09-24 1995-04-04 Mitsubishi Heavy Ind Ltd 回転機械動翼のダンパ構造
JPH09209703A (ja) * 1996-01-31 1997-08-12 Mitsubishi Heavy Ind Ltd インテグラルシュラウド翼
JP2007064074A (ja) * 2005-08-30 2007-03-15 Toshiba Corp 軸流タービン

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL108437C (de) 1960-05-09 1900-01-01
DE1159965B (de) 1961-08-10 1963-12-27 Bbc Brown Boveri & Cie Einrichtung zur Schwingungsdaempfung an einem Turbinen- oder Verdichter-Schaufelkranz
AT242717B (de) 1961-08-10 1965-10-11 Bbc Brown Boveri & Cie Deckbandbeschauflung für Turbinen oder Verdichter
US3923420A (en) * 1973-04-30 1975-12-02 Gen Electric Blade platform with friction damping interlock
GB2072760A (en) 1980-03-29 1981-10-07 Rolls Royce Shrouded turbine rotor blade
US4400915A (en) 1980-06-02 1983-08-30 United Technologies Corporation Fixture for restoring a face on the shroud of a rotor blade
DE4015206C1 (de) 1990-05-11 1991-10-17 Mtu Muenchen Gmbh
DE10012381A1 (de) 2000-03-14 2001-09-20 Man Turbomasch Ag Ghh Borsig Schaufelschloss und Verfahren zur Herstellung eines Schaufelschlosses
US6910854B2 (en) * 2002-10-08 2005-06-28 United Technologies Corporation Leak resistant vane cluster
JP4335771B2 (ja) * 2004-09-16 2009-09-30 株式会社日立製作所 タービン動翼及びタービン設備
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
EP1961918A1 (de) 2007-02-21 2008-08-27 ABB Turbo Systems AG Turbinenrad
DE102009029587A1 (de) * 2009-09-18 2011-03-24 Man Diesel & Turbo Se Rotor einer Turbomaschine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5001830A (en) * 1989-10-23 1991-03-26 Westinghouse Electric Corp. Method for assembling side entry control stage blades in a steam turbine
JPH0791206A (ja) * 1993-09-24 1995-04-04 Mitsubishi Heavy Ind Ltd 回転機械動翼のダンパ構造
JPH09209703A (ja) * 1996-01-31 1997-08-12 Mitsubishi Heavy Ind Ltd インテグラルシュラウド翼
JP2007064074A (ja) * 2005-08-30 2007-03-15 Toshiba Corp 軸流タービン

Also Published As

Publication number Publication date
JP2012021529A (ja) 2012-02-02
EP2410131B1 (de) 2018-08-15
CN102330572A (zh) 2012-01-25
DE102010031213A1 (de) 2012-01-12
CN102330572B (zh) 2014-07-09
JP5274625B2 (ja) 2013-08-28
US8974186B2 (en) 2015-03-10
US20120009067A1 (en) 2012-01-12
EP2410131A2 (de) 2012-01-25

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