KR100467732B1 - 가스터빈용에어포일및그의제조방법 - Google Patents

가스터빈용에어포일및그의제조방법 Download PDF

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Publication number
KR100467732B1
KR100467732B1 KR1019970027193A KR19970027193A KR100467732B1 KR 100467732 B1 KR100467732 B1 KR 100467732B1 KR 1019970027193 A KR1019970027193 A KR 1019970027193A KR 19970027193 A KR19970027193 A KR 19970027193A KR 100467732 B1 KR100467732 B1 KR 100467732B1
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KR
South Korea
Prior art keywords
wall
guide vane
leading edge
extruded
fan exit
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 - Fee Related
Application number
KR1019970027193A
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English (en)
Korean (ko)
Other versions
KR980002709A (ko
Inventor
토마스 제이 와트슨
빈센트 씨 나돈
존 에이 비소스키스
스튜어트 에이 앤더슨
Original Assignee
유나이티드 테크놀로지스 코포레이션
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.)
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Publication date
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Publication of KR980002709A publication Critical patent/KR980002709A/ko
Application granted granted Critical
Publication of KR100467732B1 publication Critical patent/KR100467732B1/ko
Anticipated expiration legal-status Critical
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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
    • F01D5/147—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
    • 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
    • F05D2230/24—Manufacture essentially without removing material by extrusion
    • 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
    • F05D2300/10—Metals, alloys or intermetallic compounds
    • F05D2300/17—Alloys
    • F05D2300/173—Aluminium alloys, e.g. AlCuMgPb
    • 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
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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
    • Y10T29/49337—Composite 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

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Architecture (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Extrusion Of Metal (AREA)
KR1019970027193A 1996-06-27 1997-06-25 가스터빈용에어포일및그의제조방법 Expired - Fee Related KR100467732B1 (ko)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/670,302 US5873699A (en) 1996-06-27 1996-06-27 Discontinuously reinforced aluminum gas turbine guide vane
US08/670,302 1996-06-27

Publications (2)

Publication Number Publication Date
KR980002709A KR980002709A (ko) 1998-03-30
KR100467732B1 true KR100467732B1 (ko) 2005-03-16

Family

ID=24689863

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019970027193A Expired - Fee Related KR100467732B1 (ko) 1996-06-27 1997-06-25 가스터빈용에어포일및그의제조방법

Country Status (5)

Country Link
US (2) US5873699A (enExample)
EP (1) EP0816637B1 (enExample)
JP (1) JP4051105B2 (enExample)
KR (1) KR100467732B1 (enExample)
DE (1) DE69729026T2 (enExample)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0839589A1 (de) * 1996-11-04 1998-05-06 Alusuisse Technology & Management AG Verfahren zur Herstellung eines Metallprofilstranges
US6250127B1 (en) * 1999-10-11 2001-06-26 Polese Company, Inc. Heat-dissipating aluminum silicon carbide composite manufacturing method
US6508627B2 (en) 2001-05-30 2003-01-21 Lau Industries, Inc. Airfoil blade and method for its manufacture
EP1338793A3 (en) * 2002-02-22 2010-09-01 Mitsubishi Heavy Industries, Ltd. Serrated wind turbine blade trailing edge
FR2884550B1 (fr) 2005-04-15 2010-09-17 Snecma Moteurs Piece pour proteger le bord d'attaque d'une pale
US7481573B2 (en) * 2005-06-30 2009-01-27 Spx Corporation Mixing impeller with pre-shaped tip elements
US7648336B2 (en) * 2006-01-03 2010-01-19 General Electric Company Apparatus and method for assembling a gas turbine stator
US7900437B2 (en) * 2006-07-28 2011-03-08 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US7900438B2 (en) * 2006-07-28 2011-03-08 General Electric Company Heat transfer system and method for turbine engine using heat pipes
US7700167B2 (en) * 2006-08-31 2010-04-20 Honeywell International Inc. Erosion-protective coatings on polymer-matrix composites and components incorporating such coated composites
US7980817B2 (en) * 2007-04-16 2011-07-19 United Technologies Corporation Gas turbine engine vane
US7857588B2 (en) * 2007-07-06 2010-12-28 United Technologies Corporation Reinforced airfoils
US8393158B2 (en) 2007-10-24 2013-03-12 Gulfstream Aerospace Corporation Low shock strength inlet
US8662819B2 (en) * 2008-12-12 2014-03-04 United Technologies Corporation Apparatus and method for preventing cracking of turbine engine cases
US20100150711A1 (en) * 2008-12-12 2010-06-17 United Technologies Corporation Apparatus and method for preventing cracking of turbine engine cases
US20110136141A1 (en) * 2009-12-03 2011-06-09 Abbott Laboratories Peptide reagents and method for inhibiting autoantibody antigen binding
US8740567B2 (en) * 2010-07-26 2014-06-03 United Technologies Corporation Reverse cavity blade for a gas turbine engine
US8622692B1 (en) * 2010-12-13 2014-01-07 Florida Turbine Technologies, Inc. High temperature turbine stator vane
US8727721B2 (en) * 2010-12-30 2014-05-20 General Electric Company Vane with spar mounted composite airfoil
US8690531B2 (en) * 2010-12-30 2014-04-08 General Electroc Co. Vane with spar mounted composite airfoil
US8998575B2 (en) 2011-11-14 2015-04-07 United Technologies Corporation Structural stator airfoil
US9534498B2 (en) 2012-12-14 2017-01-03 United Technologies Corporation Overmolded vane platform
DE102014200644B4 (de) * 2014-01-16 2017-03-02 MTU Aero Engines AG Strangprofil und Verfahren zur Herstellung einer Schaufel eines Nachleitrads, Schaufel eines Nachleitrads, Nachleitrad und Turbomaschine mit solch einem Nachleitrad
CN105180212B (zh) * 2015-09-02 2017-06-16 中国人民解放军国防科学技术大学 超燃冲压发动机燃烧室

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4678635A (en) * 1984-12-20 1987-07-07 Bbc Aktiengesellschaft Brown, Boveri & Cie Metallic joining material
WO1988007593A2 (en) * 1987-04-03 1988-10-06 Martin Marietta Corporation Process for forming metal-second phase composites utilizing compound starting materials, and products thereof

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5015534A (en) * 1984-10-19 1991-05-14 Martin Marietta Corporation Rapidly solidified intermetallic-second phase composites
US4851188A (en) * 1987-12-21 1989-07-25 United Technologies Corporation Method for making a turbine blade having a wear resistant layer sintered to the blade tip surface
US5337803A (en) * 1991-05-17 1994-08-16 The United States Of America As Represented By The Secretary Of The Navy Method of centrifugally casting reinforced composite articles
FR2697284B1 (fr) * 1992-10-27 1995-01-27 Europ Propulsion Procédé de fabrication d'une roue de turbine à aubes insérées et roue obtenue par le procédé.
US5511603A (en) * 1993-03-26 1996-04-30 Chesapeake Composites Corporation Machinable metal-matrix composite and liquid metal infiltration process for making same
WO1994027928A1 (en) * 1993-05-20 1994-12-08 Alliedsignal Inc. Process for preparation of metal carbide fibers
EP0656235B1 (en) * 1993-12-01 1997-10-29 Sumitomo Light Metal Industries Limited A hollow extruder die for extruding a hollow member of a zinc-containing aluminum alloy
US5509781A (en) * 1994-02-09 1996-04-23 United Technologies Corporation Compressor blade containment with composite stator vanes
US5614150A (en) * 1994-09-28 1997-03-25 Mcdonnell Douglas Corp. Method for producing refractory aluminide reinforced aluminum
JPH08177767A (ja) * 1994-12-20 1996-07-12 Zexel Corp ベーン型圧縮機のベーン及びその製造方法

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4678635A (en) * 1984-12-20 1987-07-07 Bbc Aktiengesellschaft Brown, Boveri & Cie Metallic joining material
WO1988007593A2 (en) * 1987-04-03 1988-10-06 Martin Marietta Corporation Process for forming metal-second phase composites utilizing compound starting materials, and products thereof

Also Published As

Publication number Publication date
JPH1068305A (ja) 1998-03-10
US5927130A (en) 1999-07-27
EP0816637A2 (en) 1998-01-07
KR980002709A (ko) 1998-03-30
US5873699A (en) 1999-02-23
EP0816637A3 (en) 1998-07-01
DE69729026T2 (de) 2004-09-09
JP4051105B2 (ja) 2008-02-20
EP0816637B1 (en) 2004-05-12
DE69729026D1 (de) 2004-06-17

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