EP1939402A3 - Aube de soufflante en matériau composite pour un moteur à turbine à gaz - Google Patents

Aube de soufflante en matériau composite pour un moteur à turbine à gaz Download PDF

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Publication number
EP1939402A3
EP1939402A3 EP07024380A EP07024380A EP1939402A3 EP 1939402 A3 EP1939402 A3 EP 1939402A3 EP 07024380 A EP07024380 A EP 07024380A EP 07024380 A EP07024380 A EP 07024380A EP 1939402 A3 EP1939402 A3 EP 1939402A3
Authority
EP
European Patent Office
Prior art keywords
gas turbine
turbine engine
fan blade
composite fan
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.)
Withdrawn
Application number
EP07024380A
Other languages
German (de)
English (en)
Other versions
EP1939402A2 (fr
Inventor
Karl Schreiber
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 Deutschland Ltd and Co KG
Original Assignee
Rolls Royce Deutschland Ltd and Co KG
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 Deutschland Ltd and Co KG filed Critical Rolls Royce Deutschland Ltd and Co KG
Publication of EP1939402A2 publication Critical patent/EP1939402A2/fr
Publication of EP1939402A3 publication Critical patent/EP1939402A3/fr
Withdrawn legal-status Critical Current

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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • 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
    • F05D2240/00—Components
    • F05D2240/20—Rotors
    • F05D2240/30—Characteristics of rotor blades, i.e. of any element transforming dynamic fluid energy to or from rotational energy and being attached to a rotor

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)
EP07024380A 2006-12-21 2007-12-17 Aube de soufflante en matériau composite pour un moteur à turbine à gaz Withdrawn EP1939402A3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102006061916A DE102006061916A1 (de) 2006-12-21 2006-12-21 Fanschaufel für ein Gasturbinentriebwerk

Publications (2)

Publication Number Publication Date
EP1939402A2 EP1939402A2 (fr) 2008-07-02
EP1939402A3 true EP1939402A3 (fr) 2010-05-05

Family

ID=39203238

Family Applications (1)

Application Number Title Priority Date Filing Date
EP07024380A Withdrawn EP1939402A3 (fr) 2006-12-21 2007-12-17 Aube de soufflante en matériau composite pour un moteur à turbine à gaz

Country Status (3)

Country Link
US (1) US8251664B2 (fr)
EP (1) EP1939402A3 (fr)
DE (1) DE102006061916A1 (fr)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008058913A1 (de) 2008-11-25 2010-05-27 Rolls-Royce Deutschland Ltd & Co Kg Verfahren zur Herstellung hybrider Bauteile für Fluggasturbinen
FR2943102B1 (fr) * 2009-03-12 2014-05-02 Snecma Aube en materiau composite comportant un dispositif d'amortissement.
US8585368B2 (en) * 2009-04-16 2013-11-19 United Technologies Corporation Hybrid structure airfoil
US20120021243A1 (en) * 2010-07-23 2012-01-26 General Electric Company Components with bonded edges
CH705171A1 (de) 2011-06-21 2012-12-31 Alstom Technology Ltd Turbinenschaufel mit einem Schaufelblatt aus Verbundwerkstoff und Verfahren zum Herstellen davon.
US9121294B2 (en) * 2011-12-20 2015-09-01 General Electric Company Fan blade with composite core and wavy wall trailing edge cladding
EP2679776A1 (fr) 2012-06-28 2014-01-01 Alstom Technology Ltd Système de refroidissement et procédé pour turbine à flux axial
EP2870364B1 (fr) * 2012-07-03 2018-11-28 GKN Aerospace Sweden AB Structure de support pour un moteur de turbine à gaz
DE102012015137A1 (de) * 2012-07-30 2014-02-13 Rolls-Royce Deutschland Ltd & Co Kg Niedermodulige Gasturbinenverdichterschaufel
DE102012015135A1 (de) 2012-07-30 2014-02-13 Rolls-Royce Deutschland Ltd & Co Kg Verdichterschaufel einer Gasturbine sowie Verfahren zu deren Herstellung
US9121287B2 (en) * 2012-09-12 2015-09-01 United Technologies Corporation Hollow fan blade with honeycomb filler
EP2746428B1 (fr) 2012-12-20 2017-09-13 General Electric Technology GmbH Revêtement de composants de turbine
CN105518256A (zh) * 2013-05-29 2016-04-20 通用电气公司 复合物翼形件金属补片
FR3012515B1 (fr) * 2013-10-31 2018-02-09 Safran Aube composite de turbomachine
CN106460865B (zh) 2014-05-05 2019-04-12 霍顿公司 复合物风扇
FR3041684B1 (fr) * 2015-09-28 2021-12-10 Snecma Aube comprenant un bouclier de bord d'attaque et procede de fabrication de l'aube
US11542820B2 (en) * 2017-12-06 2023-01-03 General Electric Company Turbomachinery blade and method of fabricating
US11073027B2 (en) 2018-05-17 2021-07-27 Raytheon Technologies Corporation Mold tool and methods for airfoil bonding
US11136888B2 (en) * 2018-10-18 2021-10-05 Raytheon Technologies Corporation Rotor assembly with active damping for gas turbine engines
CN110439623B (zh) * 2019-08-14 2024-05-14 上海两擎机电科技合伙企业(有限合伙) 飞机发动机风扇叶片用金属包边、加工工装及加工方法

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3762835A (en) * 1971-07-02 1973-10-02 Gen Electric Foreign object damage protection for compressor blades and other structures and related methods
DE4411679C1 (de) * 1994-04-05 1994-12-01 Mtu Muenchen Gmbh Schaufelblatt in Faserverbundbauweise mit Schutzprofil
US5672417A (en) * 1995-03-29 1997-09-30 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine blade made of composite material
EP1596036A1 (fr) * 2004-05-14 2005-11-16 General Electric Company Aubes creuses soudées par friction-malaxage et procédé associé

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1862579A (en) * 1930-02-11 1932-06-14 Parsons Elastic fluid turbine
GB1088032A (en) * 1964-06-12 1967-10-18 English Electric Co Ltd Turbine blades
US3752600A (en) * 1971-12-09 1973-08-14 United Aircraft Corp Root pads for composite blades
US3799701A (en) * 1972-02-28 1974-03-26 United Aircraft Corp Composite fan blade and method of construction
FR2195255A5 (fr) * 1972-08-04 1974-03-01 Snecma
GB2171151B (en) * 1985-02-20 1988-05-18 Rolls Royce Rotors for gas turbine engines
US5655883A (en) * 1995-09-25 1997-08-12 General Electric Company Hybrid blade for a gas turbine
US5881972A (en) * 1997-03-05 1999-03-16 United Technologies Corporation Electroformed sheath and airfoiled component construction
GB9915637D0 (en) * 1999-07-06 1999-09-01 Rolls Royce Plc A rotor seal
GB0100695D0 (en) * 2001-01-11 2001-02-21 Rolls Royce Plc a turbomachine blade
US6843928B2 (en) 2001-10-12 2005-01-18 General Electric Company Method for removing metal cladding from airfoil substrate
FR2831207B1 (fr) * 2001-10-24 2004-06-04 Snecma Moteurs Plates-formes pour aubes d'un ensemble rotatif
DE10307610A1 (de) * 2003-02-22 2004-09-02 Rolls-Royce Deutschland Ltd & Co Kg Verdichterschaufel für ein Flugzeugtriebwerk

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3762835A (en) * 1971-07-02 1973-10-02 Gen Electric Foreign object damage protection for compressor blades and other structures and related methods
DE4411679C1 (de) * 1994-04-05 1994-12-01 Mtu Muenchen Gmbh Schaufelblatt in Faserverbundbauweise mit Schutzprofil
US5672417A (en) * 1995-03-29 1997-09-30 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Turbomachine blade made of composite material
EP1596036A1 (fr) * 2004-05-14 2005-11-16 General Electric Company Aubes creuses soudées par friction-malaxage et procédé associé

Also Published As

Publication number Publication date
DE102006061916A1 (de) 2008-06-26
EP1939402A2 (fr) 2008-07-02
US20080152506A1 (en) 2008-06-26
US8251664B2 (en) 2012-08-28

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