EP2511479A3 - Annulus filler system - Google Patents

Annulus filler system Download PDF

Info

Publication number
EP2511479A3
EP2511479A3 EP12160837.6A EP12160837A EP2511479A3 EP 2511479 A3 EP2511479 A3 EP 2511479A3 EP 12160837 A EP12160837 A EP 12160837A EP 2511479 A3 EP2511479 A3 EP 2511479A3
Authority
EP
European Patent Office
Prior art keywords
foot
disc
filler
groove
rim
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
EP12160837.6A
Other languages
German (de)
French (fr)
Other versions
EP2511479B1 (en
EP2511479A2 (en
Inventor
Dale Evans
Ian Care
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of EP2511479A2 publication Critical patent/EP2511479A2/en
Publication of EP2511479A3 publication Critical patent/EP2511479A3/en
Application granted granted Critical
Publication of EP2511479B1 publication Critical patent/EP2511479B1/en
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
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • F01D11/006Sealing the gap between rotor blades or blades and rotor
    • F01D11/008Sealing the gap between rotor blades or blades and rotor by spacer elements between the blades, e.g. independent interblade platforms
    • 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
    • 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
    • F01D5/3092Protective layers between blade root and rotor disc surfaces, e.g. anti-friction layers
    • 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
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

An annulus filler system bridges the gap between two adjacent blades attached to a rim of the rotor disc of a gas turbine engine. The system includes an annulus filler having a lid which extends between the adjacent blades and defines an airflow surface for air being drawn through the engine. The filler also has a support body extending beneath the lid and terminating in an elongate foot which, in use, extends along a groove provided in the rim of the disc. The groove has a neck which prevents withdrawal of the foot through the neck in a radially outward direction of the disc. The system further includes a sleeve which, after installation of the filler, is slidably locatable into a gap between the foot and sides of the groove. The foot is formed of composite material and the sleeve provides a galvanic isolation layer preventing galvanic corrosion between the foot and the disc.
EP12160837.6A 2011-04-14 2012-03-22 Annulus filler system Active EP2511479B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB1106276.7A GB201106276D0 (en) 2011-04-14 2011-04-14 Annulus filler system

Publications (3)

Publication Number Publication Date
EP2511479A2 EP2511479A2 (en) 2012-10-17
EP2511479A3 true EP2511479A3 (en) 2017-04-19
EP2511479B1 EP2511479B1 (en) 2018-01-24

Family

ID=44123053

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12160837.6A Active EP2511479B1 (en) 2011-04-14 2012-03-22 Annulus filler system

Country Status (3)

Country Link
US (1) US20120263596A1 (en)
EP (1) EP2511479B1 (en)
GB (1) GB201106276D0 (en)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201314540D0 (en) * 2013-08-14 2013-09-25 Rolls Royce Plc Annulus filler
US10458428B2 (en) * 2013-09-09 2019-10-29 United Technologies Corporation Fan blades and manufacture methods
US10487843B2 (en) * 2013-09-09 2019-11-26 United Technologies Corporation Fan blades and manufacture methods
US10533435B2 (en) * 2013-12-13 2020-01-14 United Technologies Corporation Fan blade platform spacer mounting
US10156151B2 (en) 2014-10-23 2018-12-18 Rolls-Royce North American Technologies Inc. Composite annulus filler
US20170101878A1 (en) * 2015-10-08 2017-04-13 General Electric Company Low modulus insert for a component of a gas turbine engine
US10605117B2 (en) * 2015-10-08 2020-03-31 General Electric Company Fan platform for a gas turbine engine
US10557350B2 (en) * 2017-03-30 2020-02-11 General Electric Company I beam blade platform
US10746031B2 (en) 2017-07-18 2020-08-18 Rolls-Royce Corporation Annulus filler
US11078839B2 (en) 2018-01-22 2021-08-03 Rolls-Royce Corporation Composite nosecone
US11359500B2 (en) * 2018-10-18 2022-06-14 Raytheon Technologies Corporation Rotor assembly with structural platforms for gas turbine engines
US11209084B2 (en) * 2019-05-30 2021-12-28 The Boeing Company Seal, aircraft including the seal, and methods therefor
US11421538B2 (en) 2020-05-12 2022-08-23 Rolls-Royce Corporation Composite aerofoils
US11506083B2 (en) 2020-06-03 2022-11-22 Rolls-Royce Corporalion Composite liners for turbofan engines
CN113833691A (en) * 2020-06-08 2021-12-24 中国航发商用航空发动机有限责任公司 Fan assembly and turbofan engine
US12012857B2 (en) 2022-10-14 2024-06-18 Rtx Corporation Platform for an airfoil of a gas turbine engine
US12049833B1 (en) * 2023-05-26 2024-07-30 General Electric Company Rotor disks with disk post inserts and methods of assembling the same

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3317988A (en) * 1962-12-14 1967-05-09 Bbc Brown Boveri & Cie Method for fastening blades into turbine rotors
GB2171151A (en) * 1985-02-20 1986-08-20 Rolls Royce Rotors for gas turbine engines
WO1992004480A1 (en) * 1990-09-04 1992-03-19 Tampella Telatek Oy A coating, and a coating method, for a steam turbine and adjoining steel surfaces
DE19859477A1 (en) * 1998-12-22 2000-06-29 Mtu Muenchen Gmbh Wear protection layer
EP2154334A2 (en) * 2008-08-13 2010-02-17 Rolls-Royce plc Annulus filler between turbine blades

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US3114045A (en) * 1956-08-20 1963-12-10 Thorn Electrical Ind Ltd Photo-conductive translucent electroluminescent device and method of manufacture
US3647316A (en) * 1970-04-28 1972-03-07 Curtiss Wright Corp Variable permeability and oxidation-resistant airfoil
DE2108176A1 (en) * 1971-02-20 1972-08-31 Motoren Turbinen Union Fastening of ceramic turbine blades
US4169694A (en) * 1977-07-20 1979-10-02 Electric Power Research Institute, Inc. Ceramic rotor blade having root with double curvature
US4207029A (en) * 1978-06-12 1980-06-10 Avco Corporation Turbine rotor assembly of ceramic blades to metallic disc
US4820126A (en) * 1988-02-22 1989-04-11 Westinghouse Electric Corp. Turbomachine rotor assembly having reduced stress concentrations
US5314309A (en) * 1990-05-25 1994-05-24 Anthony Blakeley Turbine blade with metallic attachment and method of making the same
US5118257A (en) * 1990-05-25 1992-06-02 Sundstrand Corporation Boot attachment for composite turbine blade, turbine blade and method of making turbine blade
US5160243A (en) * 1991-01-15 1992-11-03 General Electric Company Turbine blade wear protection system with multilayer shim
US5240375A (en) * 1992-01-10 1993-08-31 General Electric Company Wear protection system for turbine engine rotor and blade
US6132175A (en) 1997-05-29 2000-10-17 Alliedsignal, Inc. Compliant sleeve for ceramic turbine blades
US6468613B1 (en) * 1997-08-21 2002-10-22 Toray Industries, Inc. Light metal/CFRP structural member
US6290466B1 (en) * 1999-09-17 2001-09-18 General Electric Company Composite blade root attachment
US6431835B1 (en) * 2000-10-17 2002-08-13 Honeywell International, Inc. Fan blade compliant shim
US7094033B2 (en) * 2004-01-21 2006-08-22 General Electric Company Methods and apparatus for assembling gas turbine engines
US7329101B2 (en) * 2004-12-29 2008-02-12 General Electric Company Ceramic composite with integrated compliance/wear layer
FR2890126B1 (en) * 2005-08-26 2010-10-29 Snecma ASSEMBLY AND METHOD FOR THE FOOT ASSEMBLY OF A TURBOMACHINE, BLOWER, COMPRESSOR AND TURBOMACHINE BLADE COMPRISING SUCH AN ASSEMBLY
US7435056B2 (en) * 2006-02-28 2008-10-14 Honeywell International Inc. Leading edge erosion protection for composite stator vanes
US7429165B2 (en) * 2006-06-14 2008-09-30 General Electric Company Hybrid blade for a steam turbine
FR2918702B1 (en) * 2007-07-13 2009-10-16 Snecma Sa CLINKING FOR TURBOMACHINE BLADE
FR2918703B1 (en) * 2007-07-13 2009-10-16 Snecma Sa ROTOR ASSEMBLY OF TURBOMACHINE
US20090176110A1 (en) * 2008-01-08 2009-07-09 General Electric Company Erosion and corrosion-resistant coating system and process therefor
US20100226783A1 (en) * 2009-03-06 2010-09-09 General Electric Company Erosion and Corrosion Resistant Turbine Compressor Airfoil and Method of Making the Same
US8282356B2 (en) * 2009-11-03 2012-10-09 General Electric Company Apparatus and method for reducing wear in disk lugs
US8834126B2 (en) * 2011-06-30 2014-09-16 United Technologies Corporation Fan blade protection system

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3317988A (en) * 1962-12-14 1967-05-09 Bbc Brown Boveri & Cie Method for fastening blades into turbine rotors
GB2171151A (en) * 1985-02-20 1986-08-20 Rolls Royce Rotors for gas turbine engines
WO1992004480A1 (en) * 1990-09-04 1992-03-19 Tampella Telatek Oy A coating, and a coating method, for a steam turbine and adjoining steel surfaces
DE19859477A1 (en) * 1998-12-22 2000-06-29 Mtu Muenchen Gmbh Wear protection layer
EP2154334A2 (en) * 2008-08-13 2010-02-17 Rolls-Royce plc Annulus filler between turbine blades

Also Published As

Publication number Publication date
EP2511479B1 (en) 2018-01-24
US20120263596A1 (en) 2012-10-18
EP2511479A2 (en) 2012-10-17
GB201106276D0 (en) 2011-05-25

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