EP1698758A3 - Axial getrennter Rotor-Schluss - Google Patents

Axial getrennter Rotor-Schluss Download PDF

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Publication number
EP1698758A3
EP1698758A3 EP20060110011 EP06110011A EP1698758A3 EP 1698758 A3 EP1698758 A3 EP 1698758A3 EP 20060110011 EP20060110011 EP 20060110011 EP 06110011 A EP06110011 A EP 06110011A EP 1698758 A3 EP1698758 A3 EP 1698758A3
Authority
EP
European Patent Office
Prior art keywords
rotor
halves
blades
forces
rotor end
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
EP20060110011
Other languages
English (en)
French (fr)
Other versions
EP1698758B1 (de
EP1698758A2 (de
Inventor
René Bachofner
Wolfgang Kappis
Kurt Rubischon
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.)
General Electric Technology GmbH
Original Assignee
Alstom Technology AG
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 Alstom Technology AG filed Critical Alstom Technology AG
Publication of EP1698758A2 publication Critical patent/EP1698758A2/de
Publication of EP1698758A3 publication Critical patent/EP1698758A3/de
Application granted granted Critical
Publication of EP1698758B1 publication Critical patent/EP1698758B1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3023Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses
    • F01D5/303Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot
    • F01D5/3038Fixing blades to rotors; Blade roots ; Blade spacers of radial insertion type, e.g. in individual recesses in a circumferential slot the slot having inwardly directed abutment faces on both sides
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/30Retaining components in desired mutual position

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

Ein Rotor-Schluss (1) für einen Rotor einer thermischen Turbomaschine mit zumindest einer Umfangsnut (3), in der Stauchschaufeln, Zwischenstücke und zwei Schlussschaufeln (4), zwischen denen ein Restspalt gebildet ist, montiert sind, wobei der Rotor-Schluss (1) zwei Schlusshälften (9, 9) und einen Keil (7) aufweist, ist dadurch gekennzeichnet, dass eine Klammer (8) in dem Restspalt angeordnet ist, welche die Kräfte der beiden Schlusshälften (9, 9) und zweier zwischen den Schlusshälften (9, 9) angeordneter und mit dem Keil (7) verspannten Beilagehälften (5, 6) aufnimmt. Hierdurch werden die Nachteile des Standes der Technik vermieden und ein Rotor-Schluss zur Verfügung gestellt, welcher keine Axialkräfte auf den Rotor und keine Kräfte in Umfangsrichtung auf benachbare Schaufeln ausübt, so dass ein Auftreten störender Rotorvibrationen und Verklemmung von benachbarten Schaufeln wirksam vermieden wird. Ferner wird ein entsprechendes Montageverfahren angegeben.
EP06110011.1A 2005-02-23 2006-02-16 Axial getrennter Rotor-Schluss Active EP1698758B1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH3222005 2005-02-23

Publications (3)

Publication Number Publication Date
EP1698758A2 EP1698758A2 (de) 2006-09-06
EP1698758A3 true EP1698758A3 (de) 2013-03-27
EP1698758B1 EP1698758B1 (de) 2015-11-11

Family

ID=34974750

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06110011.1A Active EP1698758B1 (de) 2005-02-23 2006-02-16 Axial getrennter Rotor-Schluss

Country Status (2)

Country Link
US (1) US7338258B2 (de)
EP (1) EP1698758B1 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2045444B1 (de) 2007-10-01 2015-11-18 Alstom Technology Ltd Laufschaufel, Verfahren zur Herstellung einer Laufschaufel, sowie Verdichter mit einer solchen Laufschaufel
US8162615B2 (en) * 2009-03-17 2012-04-24 United Technologies Corporation Split disk assembly for a gas turbine engine
CH702204A1 (de) * 2009-11-10 2011-05-13 Alstom Technology Ltd Rotor für eine axial durchströmte turbomaschine sowie gasturbine für solchen rotor.
US8545184B2 (en) * 2010-01-05 2013-10-01 General Electric Company Locking spacer assembly
US8517688B2 (en) * 2010-09-21 2013-08-27 General Electric Company Rotor assembly for use in turbine engines and methods for assembling same
EP3159483A1 (de) * 2015-10-22 2017-04-26 Siemens Aktiengesellschaft Schaufelträger zur befestigung von laufschaufeln einer thermischen strömungsmaschine
US10465699B2 (en) * 2017-01-26 2019-11-05 DOOSAN Heavy Industries Construction Co., LTD Compressor blade locking mechanism in disk with tangential groove
CN108791817B (zh) * 2018-06-26 2021-07-20 深圳市飞翼创新有限公司 一种具有低阻力性能的飞行器螺旋桨及其组装方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH349624A (de) * 1957-03-05 1960-10-31 Oerlikon Maschf Axiale Strömungsmaschine
DE1751819B1 (de) * 1968-07-26 1971-01-21 Sulzer Ag Läufer für Str¦mungsmaschinen
EP1215367A2 (de) * 2000-12-16 2002-06-19 ALSTOM Power N.V. Fixiervorrichtung für eine Beschaufelung einer Strömungsmaschine
EP1457642A2 (de) * 2003-03-11 2004-09-15 Alstom Technology Ltd Vorrichtung zur Schaufelbefestigung an einem Rotor

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
NL56668C (de) 1940-06-12
US2406703A (en) * 1944-06-08 1946-08-27 Allis Chalmers Mfg Co Turbine blade locking apparatus
FR974989A (fr) 1948-09-17 1951-02-28 Verrou pour l'aubage des rotors en forme de tambour de compresseurs axiaux et de turbines à vapeur ou à gaz
US3252687A (en) * 1965-02-01 1966-05-24 Gen Motors Corp Rotor blade locking
EP1028231B1 (de) 1999-02-12 2003-09-03 ALSTOM (Switzerland) Ltd Befestigung von Laufschaufeln einer Strömungsmachine

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH349624A (de) * 1957-03-05 1960-10-31 Oerlikon Maschf Axiale Strömungsmaschine
DE1751819B1 (de) * 1968-07-26 1971-01-21 Sulzer Ag Läufer für Str¦mungsmaschinen
EP1215367A2 (de) * 2000-12-16 2002-06-19 ALSTOM Power N.V. Fixiervorrichtung für eine Beschaufelung einer Strömungsmaschine
EP1457642A2 (de) * 2003-03-11 2004-09-15 Alstom Technology Ltd Vorrichtung zur Schaufelbefestigung an einem Rotor

Also Published As

Publication number Publication date
US7338258B2 (en) 2008-03-04
US20060188373A1 (en) 2006-08-24
EP1698758B1 (de) 2015-11-11
EP1698758A2 (de) 2006-09-06

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