DE602004029836D1 - Herstellung von Turbinenelementen - Google Patents

Herstellung von Turbinenelementen

Info

Publication number
DE602004029836D1
DE602004029836D1 DE602004029836T DE602004029836T DE602004029836D1 DE 602004029836 D1 DE602004029836 D1 DE 602004029836D1 DE 602004029836 T DE602004029836 T DE 602004029836T DE 602004029836 T DE602004029836 T DE 602004029836T DE 602004029836 D1 DE602004029836 D1 DE 602004029836D1
Authority
DE
Germany
Prior art keywords
production
turbine elements
turbine
elements
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
DE602004029836T
Other languages
English (en)
Inventor
Peter E Liebfried
Brian J Hamilla
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.)
RTX Corp
Original Assignee
United Technologies Corp
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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE602004029836D1 publication Critical patent/DE602004029836D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
    • 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
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • 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
    • 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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Architecture (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
DE602004029836T 2003-02-10 2004-02-09 Herstellung von Turbinenelementen Expired - Lifetime DE602004029836D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US10/361,279 US6705011B1 (en) 2003-02-10 2003-02-10 Turbine element manufacture

Publications (1)

Publication Number Publication Date
DE602004029836D1 true DE602004029836D1 (de) 2010-12-16

Family

ID=31946657

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004029836T Expired - Lifetime DE602004029836D1 (de) 2003-02-10 2004-02-09 Herstellung von Turbinenelementen

Country Status (4)

Country Link
US (1) US6705011B1 (de)
EP (1) EP1445057B1 (de)
JP (1) JP2004243515A (de)
DE (1) DE602004029836D1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2855441B1 (fr) * 2003-05-27 2006-07-14 Snecma Moteurs Aube creuse pour turbomachine et procede de fabrication d'une telle aube.
FR2867095B1 (fr) * 2004-03-03 2007-04-20 Snecma Moteurs Procede de fabrication d'une aube creuse pour turbomachine.
FR2867096B1 (fr) * 2004-03-08 2007-04-20 Snecma Moteurs Procede de fabrication d'un bord d'attaque ou de fuite de renforcement pour une aube de soufflante
US7083388B2 (en) * 2004-04-29 2006-08-01 United Technologies Corporation Double near-net forging of article
US7441331B2 (en) 2004-08-26 2008-10-28 United Technologies Corporation Turbine engine component manufacture methods
US7849596B2 (en) * 2007-11-19 2010-12-14 Ocean Renewable Power Company, Llc High efficiency turbine and method of making the same
GB0903614D0 (en) * 2009-03-04 2009-04-08 Rolls Royce Plc Method of manufacturing an aerofoil
US8616852B2 (en) * 2009-11-25 2013-12-31 United Technologies Corporation Welding repair method of an integrally bladed rotor
US20110211965A1 (en) * 2010-02-26 2011-09-01 United Technologies Corporation Hollow fan blade
US20170074116A1 (en) * 2014-07-17 2017-03-16 United Technologies Corporation Method of creating heat transfer features in high temperature alloys
FR3063663B1 (fr) * 2017-03-13 2021-02-26 Mecachrome France Procede de fabrication de pieces en alliage metallique de forme complexe

Family Cites Families (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3004607A (en) 1956-05-15 1961-10-17 Bell Aerospace Corp Helicopter metal main rotor blade
US3588980A (en) 1969-07-17 1971-06-29 Gen Electric Method for making a contoured article
US3628226A (en) 1970-03-16 1971-12-21 Aerojet General Co Method of making hollow compressor blades
US4257737A (en) 1978-07-10 1981-03-24 United Technologies Corporation Cooled rotor blade
US4364160A (en) * 1980-11-03 1982-12-21 General Electric Company Method of fabricating a hollow article
US4594761A (en) 1984-02-13 1986-06-17 General Electric Company Method of fabricating hollow composite airfoils
US4642863A (en) 1985-04-15 1987-02-17 Ontario Technologies Corporation Manufacturing method for hollow metal airfoil type structure
US4726101A (en) 1986-09-25 1988-02-23 United Technologies Corporation Turbine vane nozzle reclassification
US5018271A (en) 1988-09-09 1991-05-28 Airfoil Textron Inc. Method of making a composite blade with divergent root
US5063662A (en) 1990-03-22 1991-11-12 United Technologies Corporation Method of forming a hollow blade
US5099573A (en) 1990-06-27 1992-03-31 Compressor Components Textron Inc. Method of making hollow articles
US5123814A (en) 1990-07-27 1992-06-23 The Marley Cooling Tower Company Industrial cooling tower fan blade having abrasion resistant leading edge
US5083371A (en) 1990-09-14 1992-01-28 United Technologies Corporation Hollow metal article fabrication
US5269658A (en) 1990-12-24 1993-12-14 United Technologies Corporation Composite blade with partial length spar
US5253419A (en) 1991-02-20 1993-10-19 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Method of manufacturing a hollow blade for a turboshaft engine
US5222297A (en) 1991-10-18 1993-06-29 United Technologies Corporation Composite blade manufacture
GB2269555B (en) 1992-08-14 1995-01-04 Rolls Royce Plc A method of manufacturing an article by superplastic forming and diffusion bonding
US5269058A (en) * 1992-12-16 1993-12-14 General Electric Company Design and processing method for manufacturing hollow airfoils
DE4327189C2 (de) 1993-08-13 1996-02-01 Mtu Muenchen Gmbh Reparaturverfahren für im Kopf- oder Kantenbereich beschädigte Schaufelblätter von Turbomaschinen
US5469618A (en) 1993-12-06 1995-11-28 General Electric Company Method for manufacturing hollow airfoils (two-piece concept)
US5448829A (en) 1994-01-31 1995-09-12 United Technologies Corporation Hollow titanium blade manufacturing
FR2724127B1 (fr) 1994-09-07 1996-12-20 Snecma Procede de fabrication d'une aube creuse de turbomachine
US5692881A (en) 1995-06-08 1997-12-02 United Technologies Corporation Hollow metallic structure and method of manufacture
FR2739045B1 (fr) 1995-09-27 1997-10-31 Snecma Procede de fabrication d'une aube creuse de turbomachine
GB2306353B (en) 1995-10-28 1998-10-07 Rolls Royce Plc A method of manufacturing a blade
US6162347A (en) * 1998-09-28 2000-12-19 General Electric Company Co-machined bonded airfoil
US6193141B1 (en) * 2000-04-25 2001-02-27 Siemens Westinghouse Power Corporation Single crystal turbine components made using a moving zone transient liquid phase bonded sandwich construction

Also Published As

Publication number Publication date
JP2004243515A (ja) 2004-09-02
EP1445057A1 (de) 2004-08-11
EP1445057B1 (de) 2010-11-03
US6705011B1 (en) 2004-03-16

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