FR2325802A1 - Procede de fabrication d'aube de turbomachine - Google Patents

Procede de fabrication d'aube de turbomachine

Info

Publication number
FR2325802A1
FR2325802A1 FR7628433A FR7628433A FR2325802A1 FR 2325802 A1 FR2325802 A1 FR 2325802A1 FR 7628433 A FR7628433 A FR 7628433A FR 7628433 A FR7628433 A FR 7628433A FR 2325802 A1 FR2325802 A1 FR 2325802A1
Authority
FR
France
Prior art keywords
manufacturing process
dawn
turbomachine
turbomachine dawn
manufacturing
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Withdrawn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
FR7628433A
Other languages
English (en)
Inventor
Kenneth Alonzo Darrow
John William Daly
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
Publication of FR2325802A1 publication Critical patent/FR2325802A1/fr
Withdrawn legal-status Critical Current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
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/288—Protective coatings for blades
    • 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
    • Y10T29/49341—Hollow blade with cooling passage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Shovels (AREA)
  • Component Parts Of Construction Machinery (AREA)
FR7628433A 1975-09-25 1976-09-22 Procede de fabrication d'aube de turbomachine Withdrawn FR2325802A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/616,563 US4023249A (en) 1975-09-25 1975-09-25 Method of manufacture of cooled turbine or compressor buckets

Publications (1)

Publication Number Publication Date
FR2325802A1 true FR2325802A1 (fr) 1977-04-22

Family

ID=24470025

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7628433A Withdrawn FR2325802A1 (fr) 1975-09-25 1976-09-22 Procede de fabrication d'aube de turbomachine

Country Status (7)

Country Link
US (1) US4023249A (fr)
JP (1) JPS5260321A (fr)
DE (1) DE2642737A1 (fr)
FR (1) FR2325802A1 (fr)
GB (1) GB1547203A (fr)
NL (1) NL7607144A (fr)
NO (1) NO763297L (fr)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA1267514A (fr) * 1987-07-15 1990-04-10 Jobst Ulrich Gellert Buse d'injection a revetement pour le moulage
US5038014A (en) * 1989-02-08 1991-08-06 General Electric Company Fabrication of components by layered deposition
US6059533A (en) * 1997-07-17 2000-05-09 Alliedsignal Inc. Damped blade having a single coating of vibration-damping material
US6468669B1 (en) * 1999-05-03 2002-10-22 General Electric Company Article having turbulation and method of providing turbulation on an article
US20040228976A1 (en) * 2002-04-23 2004-11-18 Gerneral Electric Company Sprayable noble metal coating for high tempreature use on ceramic and smoothcoat coated aircraft engine parts
US7250192B2 (en) * 2002-04-23 2007-07-31 General Electric Company Sprayable noble metal coating for high temperature use directly on aircraft engine alloys
US6910620B2 (en) 2002-10-15 2005-06-28 General Electric Company Method for providing turbulation on the inner surface of holes in an article, and related articles
US7758314B2 (en) * 2003-03-12 2010-07-20 Florida Turbine Technologies, Inc. Tungsten shell for a spar and shell turbine vane
US7080971B2 (en) * 2003-03-12 2006-07-25 Florida Turbine Technologies, Inc. Cooled turbine spar shell blade construction
US20050000674A1 (en) * 2003-07-01 2005-01-06 Beddard Thomas Bradley Perimeter-cooled stage 1 bucket core stabilizing device and related method
US6966756B2 (en) * 2004-01-09 2005-11-22 General Electric Company Turbine bucket cooling passages and internal core for producing the passages
US20060088727A1 (en) * 2004-10-25 2006-04-27 General Electric Company High reflectivity infrared coating applications for use in HIRSS applications
EP1828544B1 (fr) * 2004-12-24 2011-06-22 Alstom Technology Ltd Procede de production d'un composant comprenant un canal incorpore et composant
US7748601B2 (en) * 2005-09-28 2010-07-06 General Electric Company Brazed articles, braze assemblies and methods therefor utilizing gold/copper/nickel brazing alloys
US8846206B2 (en) * 2008-07-31 2014-09-30 Siemens Energy, Inc. Injection molded component
US20120082553A1 (en) * 2010-09-30 2012-04-05 Andreas Eleftheriou Metal encapsulated stator vane
US20120082556A1 (en) * 2010-09-30 2012-04-05 Enzo Macchia Nanocrystalline metal coated composite airfoil
US9587645B2 (en) 2010-09-30 2017-03-07 Pratt & Whitney Canada Corp. Airfoil blade
US9429029B2 (en) 2010-09-30 2016-08-30 Pratt & Whitney Canada Corp. Gas turbine blade and method of protecting same
US9427835B2 (en) 2012-02-29 2016-08-30 Pratt & Whitney Canada Corp. Nano-metal coated vane component for gas turbine engines and method of manufacturing same
US10982551B1 (en) 2012-09-14 2021-04-20 Raytheon Technologies Corporation Turbomachine blade
US20150118060A1 (en) * 2013-10-25 2015-04-30 General Electric Company Turbine engine blades, related articles, and methods
US20160089692A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine component coating processes and turbine components
US10815787B1 (en) * 2017-01-17 2020-10-27 Raytheon Technologies Corporation Gas turbine engine airfoil frequency design
US11199096B1 (en) * 2017-01-17 2021-12-14 Raytheon Technologies Corporation Turbomachine blade
US20200039641A1 (en) * 2018-08-02 2020-02-06 Bell Helicopter Textron Inc. Abrasion strip and method of manufacturing the same
FR3094253B1 (fr) * 2019-03-29 2023-06-16 Safran Aircraft Engines Procede de collage d’une piece metallique sur un element en materiau composite d’une turbomachine d’aeronef

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2641439A (en) * 1947-10-01 1953-06-09 Chrysler Corp Cooled turbine or compressor blade
US2648520A (en) * 1949-08-02 1953-08-11 Heinz E Schmitt Air-cooled turbine blade
US2993678A (en) * 1955-07-21 1961-07-25 Gen Electric Coated molybdenum article
US3068556A (en) * 1958-10-09 1962-12-18 Bruce E Kramer Method of making jet turbine buckets
US3269856A (en) * 1962-06-07 1966-08-30 Lockheed Aircraft Corp Coating for refractory metal
US3748110A (en) * 1971-10-27 1973-07-24 Gen Motors Corp Ductile corrosion resistant coating for nickel base alloy articles
US3841805A (en) * 1973-04-04 1974-10-15 Houdaille Industries Inc Screw liner

Also Published As

Publication number Publication date
JPS5260321A (en) 1977-05-18
US4023249A (en) 1977-05-17
NL7607144A (nl) 1977-03-29
DE2642737A1 (de) 1977-04-07
NO763297L (no) 1977-03-28
GB1547203A (en) 1979-06-06

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Legal Events

Date Code Title Description
ST Notification of lapse