WO2010097277A3 - Method for attaching or producing a closed cover strip for the blading of a turbine stage and blading - Google Patents

Method for attaching or producing a closed cover strip for the blading of a turbine stage and blading Download PDF

Info

Publication number
WO2010097277A3
WO2010097277A3 PCT/EP2010/051366 EP2010051366W WO2010097277A3 WO 2010097277 A3 WO2010097277 A3 WO 2010097277A3 EP 2010051366 W EP2010051366 W EP 2010051366W WO 2010097277 A3 WO2010097277 A3 WO 2010097277A3
Authority
WO
WIPO (PCT)
Prior art keywords
blading
attaching
producing
closed cover
turbine stage
Prior art date
Application number
PCT/EP2010/051366
Other languages
German (de)
French (fr)
Other versions
WO2010097277A2 (en
Inventor
Christoph Ebert
Detlef Haje
Albert Langkamp
Markus Mantei
Original Assignee
Siemens Aktiengesellschaft
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 Siemens Aktiengesellschaft filed Critical Siemens Aktiengesellschaft
Priority to EP10702677A priority Critical patent/EP2401477A2/en
Publication of WO2010097277A2 publication Critical patent/WO2010097277A2/en
Publication of WO2010097277A3 publication Critical patent/WO2010097277A3/en

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
    • F01D5/34Rotor-blade aggregates of unitary construction, e.g. formed of sheet laminae
    • 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
    • F01D5/12Blades
    • F01D5/22Blade-to-blade connections, e.g. for damping vibrations
    • F01D5/225Blade-to-blade connections, e.g. for damping vibrations by shrouding
    • 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
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282Selecting composite materials, e.g. blades with reinforcing filaments
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00Components
    • F05B2240/20Rotors
    • F05B2240/33Shrouds which are part of or which are rotating with the rotor
    • 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
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/31Application in turbines in steam turbines
    • 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
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • 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
    • F05D2230/00Manufacture
    • F05D2230/60Assembly methods

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Ceramic Engineering (AREA)
  • Composite Materials (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The invention relates to a method for attaching or producing a closed cover strip (1) to or on the free front ends (2) of neighbouring blades (3) of the blading of a turbine stage, according to which a strip consisting of a fibrous material is wound onto the free front ends (2) of the blades (3), a matrix material is infiltrated into the fibrous material of the wound strip and the resultant fibre composite material is cured. The invention also relates to two other methods for attaching/producing a closed cover strip (1) to or on the front free ends (2) of neighbouring blades (3) of the blading of a turbine stage and to blading for a turbine, having a plurality of neighbouring blades (3), said blades (3) being made from a fibrous material.
PCT/EP2010/051366 2009-02-25 2010-02-04 Method for attaching or producing a closed cover strip the blading of a turbine stage and blading for a turbine stage of a turbine WO2010097277A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP10702677A EP2401477A2 (en) 2009-02-25 2010-02-04 Method for attaching or producing an annular shroud for a turbine rotor and turbine rotor

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102009010613.8 2009-02-25
DE200910010613 DE102009010613A1 (en) 2009-02-25 2009-02-25 A method for attaching or producing a closed shroud for a rotor blading a turbine stage and blading a turbine stage for a turbine

Publications (2)

Publication Number Publication Date
WO2010097277A2 WO2010097277A2 (en) 2010-09-02
WO2010097277A3 true WO2010097277A3 (en) 2011-06-23

Family

ID=42371723

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2010/051366 WO2010097277A2 (en) 2009-02-25 2010-02-04 Method for attaching or producing a closed cover strip the blading of a turbine stage and blading for a turbine stage of a turbine

Country Status (3)

Country Link
EP (1) EP2401477A2 (en)
DE (1) DE102009010613A1 (en)
WO (1) WO2010097277A2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102009036018A1 (en) * 2009-08-04 2011-02-17 Siemens Aktiengesellschaft Thermoplastic final stage blade
US9151166B2 (en) 2010-06-07 2015-10-06 Rolls-Royce North American Technologies, Inc. Composite gas turbine engine component
EP2431571B1 (en) 2010-09-16 2013-06-05 Techspace Aero S.A. Assembly of a blade and a composite support by secure fixing

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB835177A (en) * 1957-06-14 1960-05-18 Burton Albert Avery Vibration damping shroud for gas turbine engines
GB1244349A (en) * 1968-01-29 1971-08-25 Gen Electric Improvements in composite bladed rotors
US4017209A (en) * 1975-12-15 1977-04-12 United Technologies Corporation Turbine rotor construction
DE3523518A1 (en) * 1984-07-07 1986-02-06 Rolls-Royce Ltd., London RING SHAPED BUCKET BODY WITH AN INTEGRAL BUCKET RING AND METHOD FOR PRODUCING THE SAME
DE10304529B3 (en) * 2003-02-04 2004-05-27 E & T Energietechnik Gmbh Axial steam or gas turbine for energy plant has ring fitted around radial outer ends of turbine blades for damping blade vibration
EP1788197A1 (en) * 2005-11-21 2007-05-23 Siemens Aktiengesellschaft Turbine blade for a steam turbine
DE102006025883A1 (en) * 2006-06-02 2007-12-06 Mtu Aero Engines Gmbh Integral bladed gas turbine rotor for gas turbine aircraft engine, has shrouding band designed as closed ring, and resting against outside sections of rotor blades in resting condition and in operation of rotor by compression stress

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3977728A (en) * 1974-12-30 1976-08-31 General Electric Company Wheel
US6223524B1 (en) * 1998-01-23 2001-05-01 Diversitech, Inc. Shrouds for gas turbine engines and methods for making the same
GB2427658B (en) * 2005-06-30 2007-08-22 Rolls Royce Plc Organic matrix composite integrally bladed rotor

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB835177A (en) * 1957-06-14 1960-05-18 Burton Albert Avery Vibration damping shroud for gas turbine engines
GB1244349A (en) * 1968-01-29 1971-08-25 Gen Electric Improvements in composite bladed rotors
US4017209A (en) * 1975-12-15 1977-04-12 United Technologies Corporation Turbine rotor construction
DE3523518A1 (en) * 1984-07-07 1986-02-06 Rolls-Royce Ltd., London RING SHAPED BUCKET BODY WITH AN INTEGRAL BUCKET RING AND METHOD FOR PRODUCING THE SAME
DE10304529B3 (en) * 2003-02-04 2004-05-27 E & T Energietechnik Gmbh Axial steam or gas turbine for energy plant has ring fitted around radial outer ends of turbine blades for damping blade vibration
EP1788197A1 (en) * 2005-11-21 2007-05-23 Siemens Aktiengesellschaft Turbine blade for a steam turbine
DE102006025883A1 (en) * 2006-06-02 2007-12-06 Mtu Aero Engines Gmbh Integral bladed gas turbine rotor for gas turbine aircraft engine, has shrouding band designed as closed ring, and resting against outside sections of rotor blades in resting condition and in operation of rotor by compression stress

Also Published As

Publication number Publication date
DE102009010613A1 (en) 2010-09-02
WO2010097277A2 (en) 2010-09-02
EP2401477A2 (en) 2012-01-04

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