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DE60008980D1 - Durch Spritzgiessen geformte Hybridschaufel - Google Patents

Durch Spritzgiessen geformte Hybridschaufel

Info

Publication number
DE60008980D1
DE60008980D1 DE60008980T DE60008980T DE60008980D1 DE 60008980 D1 DE60008980 D1 DE 60008980D1 DE 60008980 T DE60008980 T DE 60008980T DE 60008980 T DE60008980 T DE 60008980T DE 60008980 D1 DE60008980 D1 DE 60008980D1
Authority
DE
Germany
Prior art keywords
injection molding
hybrid blade
blade molded
molded
hybrid
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.)
Expired - Lifetime
Application number
DE60008980T
Other languages
English (en)
Other versions
DE60008980T2 (de
Inventor
Charles Richard Evans
Begovich, Jr
Douglas Duane Ward
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 Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Application granted granted Critical
Publication of DE60008980D1 publication Critical patent/DE60008980D1/de
Publication of DE60008980T2 publication Critical patent/DE60008980T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • F01D5/14—Form or construction
    • F01D5/16—Form or construction for counteracting blade vibration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C45/00—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor
    • B29C45/14—Injection moulding, i.e. forcing the required volume of moulding material through a nozzle into a closed mould; Apparatus therefor incorporating preformed parts or layers, e.g. injection moulding around inserts or for coating articles
    • B29C45/14467—Joining articles or parts of a single article
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/78—Moulding material on one side only of the preformed part
    • 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
    • F01D5/14—Form or construction
    • F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2705/00—Use of metals, their alloys or their compounds, for preformed parts, e.g. for inserts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • 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
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/40—Organic materials
    • F05D2300/43—Synthetic polymers, e.g. plastics; Rubber
    • F05D2300/431—Rubber
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/49336—Blade making
    • Y10T29/49339—Hollow blade
    • Y10T29/49341—Hollow blade with cooling passage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Materials Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Architecture (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60008980T 1999-08-16 2000-08-04 Durch Spritzgiessen geformte Hybridschaufel Expired - Lifetime DE60008980T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/374,532 US6282786B1 (en) 1999-08-16 1999-08-16 Method of making injection formed hybrid airfoil
US374532 1999-08-16

Publications (2)

Publication Number Publication Date
DE60008980D1 true DE60008980D1 (de) 2004-04-22
DE60008980T2 DE60008980T2 (de) 2005-03-10

Family

ID=23477252

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60008980T Expired - Lifetime DE60008980T2 (de) 1999-08-16 2000-08-04 Durch Spritzgiessen geformte Hybridschaufel

Country Status (4)

Country Link
US (1) US6282786B1 (de)
EP (1) EP1077126B1 (de)
JP (1) JP5178971B2 (de)
DE (1) DE60008980T2 (de)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6287080B1 (en) * 1999-11-15 2001-09-11 General Electric Company Elastomeric formulation used in the construction of lightweight aircraft engine fan blades
US6431850B1 (en) * 2000-08-11 2002-08-13 General Electric Company Composite caul sheet with integral seal used in the fabrication of lightweight airfoils and method of making
US6814541B2 (en) 2002-10-07 2004-11-09 General Electric Company Jet aircraft fan case containment design
US7104761B2 (en) * 2004-07-28 2006-09-12 General Electric Company Hybrid turbine blade and related method
US7278830B2 (en) * 2005-05-18 2007-10-09 Allison Advanced Development Company, Inc. Composite filled gas turbine engine blade with gas film damper
US8844090B2 (en) * 2005-06-17 2014-09-30 United Technologies Corporation Tool for filling voids in turbine vanes and other articles
US7380321B2 (en) * 2006-03-28 2008-06-03 The Boeing Company Machining technique with selective and localized placement of tooling material
GB2450937B (en) * 2007-07-13 2009-06-03 Rolls Royce Plc Component with tuned frequency response
US8221085B2 (en) * 2007-12-13 2012-07-17 General Electric Company Wind blade joint bonding grid
DE102008031329A1 (de) * 2008-07-02 2010-01-07 Mtu Aero Engines Gmbh Verfahren zum Herstellen von Gasturbinenschaufeln
DE102011109977B4 (de) * 2011-08-11 2013-03-07 Airbus Operations Gmbh Vorrichtung zur urformtechnischen Herstellung eines integralen Strukturbauteils aus einem mit Stringern verstärkten Faserverbundwerkstoff für ein Flugzeug
US9011087B2 (en) 2012-03-26 2015-04-21 United Technologies Corporation Hybrid airfoil for a gas turbine engine
EP2900923B1 (de) * 2012-09-25 2019-12-25 United Technologies Corporation Schaufelanordnung aus leitschaufeln mit unterschiedlicher geometrie nach geometrieklassen
FR3012515B1 (fr) * 2013-10-31 2018-02-09 Safran Aube composite de turbomachine
DE102015203868A1 (de) 2015-03-04 2016-09-08 Rolls-Royce Deutschland Ltd & Co Kg Fanschaufel für einen Flugantrieb
US9982684B2 (en) 2015-08-07 2018-05-29 General Electric Company Hybrid metal compressor blades
US10465715B2 (en) * 2017-10-18 2019-11-05 Goodrich Corporation Blade with damping structures
US10677068B2 (en) 2018-01-18 2020-06-09 Raytheon Technologies Corporation Fan blade with filled pocket
FR3081370B1 (fr) * 2018-05-22 2020-06-05 Safran Aircraft Engines Corps d'aube et aube en materiau composite ayant un renfort fibreux compose d'un tissage tridimensionnel et de fibres courtes et leur procede de fabrication
FR3082877B1 (fr) * 2018-06-21 2020-09-25 Safran Aircraft Engines Aube a structure hybride pour turbomachine
FR3100471B1 (fr) 2019-09-10 2022-12-09 Safran Aircraft Engines Préforme pour aube composite

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1084537A (en) 1965-07-31 1967-09-27 Rolls Royce A compressor or turbine rotor for a gas turbine engine
US3796513A (en) 1972-06-19 1974-03-12 Westinghouse Electric Corp High damping blades
US4118147A (en) 1976-12-22 1978-10-03 General Electric Company Composite reinforcement of metallic airfoils
JPS58107318A (ja) * 1981-12-18 1983-06-27 Sanyo Electric Co Ltd 積層断熱体の製造方法
JPH01178417A (ja) * 1988-01-06 1989-07-14 Sumitomo Chem Co Ltd 積層体の製造方法
JP3055955B2 (ja) * 1991-02-18 2000-06-26 三菱樹脂株式会社 繊維強化プラスチックファンの製造法
JP2973565B2 (ja) * 1991-04-25 1999-11-08 住友化学工業株式会社 多層成形品の製造方法
FR2688264A1 (fr) 1992-03-04 1993-09-10 Snecma Redresseur de turbomachine a aubes ayant une face alveolee chargee en materiau composite.
JP2960861B2 (ja) * 1994-12-22 1999-10-12 株式会社イノアックコーポレーション 発泡成形品の製造方法
US5634771A (en) 1995-09-25 1997-06-03 General Electric Company Partially-metallic blade for a gas turbine
US5655883A (en) * 1995-09-25 1997-08-12 General Electric Company Hybrid blade for a gas turbine
FR2745589B1 (fr) * 1996-02-29 1998-04-30 Snecma Piece hybride a haut rapport resistance-masse et procede de realisation
JPH1054204A (ja) 1996-05-20 1998-02-24 General Electric Co <Ge> ガスタービン用の多構成部翼
US5875549A (en) * 1997-03-17 1999-03-02 Siemens Westinghouse Power Corporation Method of forming internal passages within articles and articles formed by same
US5839882A (en) 1997-04-25 1998-11-24 General Electric Company Gas turbine blade having areas of different densities
JPH1177711A (ja) * 1997-09-01 1999-03-23 Sumitomo Chem Co Ltd 積層体の製造方法
US6039542A (en) * 1997-12-24 2000-03-21 General Electric Company Panel damped hybrid blade

Also Published As

Publication number Publication date
DE60008980T2 (de) 2005-03-10
JP2001073997A (ja) 2001-03-21
JP5178971B2 (ja) 2013-04-10
EP1077126B1 (de) 2004-03-17
EP1077126A1 (de) 2001-02-21
US6282786B1 (en) 2001-09-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN