FR2329402A1 - Procede de realisation d'une piece aerodynamique - Google Patents

Procede de realisation d'une piece aerodynamique

Info

Publication number
FR2329402A1
FR2329402A1 FR7632321A FR7632321A FR2329402A1 FR 2329402 A1 FR2329402 A1 FR 2329402A1 FR 7632321 A FR7632321 A FR 7632321A FR 7632321 A FR7632321 A FR 7632321A FR 2329402 A1 FR2329402 A1 FR 2329402A1
Authority
FR
France
Prior art keywords
making
aerodynamic part
aerodynamic
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Withdrawn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
FR7632321A
Other languages
English (en)
Inventor
Kenneth Alonzo Darrow
Paul Harriman Kydd
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 FR2329402A1 publication Critical patent/FR2329402A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K1/00—Soldering, e.g. brazing, or unsoldering
    • B23K1/0008—Soldering, e.g. brazing, or unsoldering specially adapted for particular articles or work
    • 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
    • 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
FR7632321A 1975-10-29 1976-10-27 Procede de realisation d'une piece aerodynamique Withdrawn FR2329402A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/626,633 US4040159A (en) 1975-10-29 1975-10-29 Method of manufacture of cooled airfoil-shaped bucket

Publications (1)

Publication Number Publication Date
FR2329402A1 true FR2329402A1 (fr) 1977-05-27

Family

ID=24511199

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7632321A Withdrawn FR2329402A1 (fr) 1975-10-29 1976-10-27 Procede de realisation d'une piece aerodynamique

Country Status (7)

Country Link
US (1) US4040159A (fr)
JP (1) JPS5254810A (fr)
DE (1) DE2648026A1 (fr)
FR (1) FR2329402A1 (fr)
GB (1) GB1554195A (fr)
NL (1) NL7609371A (fr)
NO (1) NO763676L (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5422188A (en) * 1991-05-03 1995-06-06 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Part made from ceramic composite having a metallic coating, process for producing same and powder composition used

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5152059A (en) * 1980-09-19 1992-10-06 Rolls-Royce Plc Manufacture of cooled aerofoil blades
DE3419674A1 (de) * 1983-05-26 1984-11-29 Rolls-Royce Ltd., London Verfahren zum aufbringen eines ueberzugs auf ein bauteil
FR2609936B1 (fr) * 1987-01-28 1989-03-31 Commissariat Energie Atomique Procede de fixation d'une couche poreuse sur un substrat et application de ce procede a la realisation d'une prothese
GB8917613D0 (en) * 1989-08-01 1989-09-13 British Aerospace Stopping-off process
US5511721A (en) * 1994-11-07 1996-04-30 General Electric Company Braze blocking insert for liquid phase brazing operations
US6399217B1 (en) * 1999-12-20 2002-06-04 General Electric Company Article surface with metal wires and method for making
US6796770B2 (en) * 2002-11-06 2004-09-28 Spx Corporation Impeller and method using solid free form fabrication
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
US8956105B2 (en) * 2008-12-31 2015-02-17 Rolls-Royce North American Technologies, Inc. Turbine vane for gas turbine engine
US8668442B2 (en) * 2010-06-30 2014-03-11 Honeywell International Inc. Turbine nozzles and methods of manufacturing the same
US8739404B2 (en) * 2010-11-23 2014-06-03 General Electric Company Turbine components with cooling features and methods of manufacturing the same
US20120156054A1 (en) * 2010-12-15 2012-06-21 General Electric Company Turbine component with near-surface cooling passage and process therefor
US10775115B2 (en) * 2013-08-29 2020-09-15 General Electric Company Thermal spray coating method and thermal spray coated article
US9126279B2 (en) 2013-09-30 2015-09-08 General Electric Company Brazing method
US9254537B2 (en) * 2013-12-19 2016-02-09 Siemens Energy, Inc. Plural layer putty-powder/slurry application method for superalloy component crack vacuum furnace healing
CN108672865A (zh) * 2018-04-16 2018-10-19 中国电子科技集团公司第十研究所 一种丝网钎焊方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1147233A (en) * 1910-06-04 1915-07-20 Arthur Hugo Cecil Gibson Propeller.
US2022562A (en) * 1930-10-13 1935-11-26 Firm Grumpelt Propellerbau Gmb Propeller
US2161533A (en) * 1936-02-01 1939-06-06 Hugo Heine Means for protecting wooden propellers
US2290934A (en) * 1942-03-28 1942-07-28 Rudolf W Andreasson Metal cutting tool
US2641439A (en) * 1947-10-01 1953-06-09 Chrysler Corp Cooled turbine or compressor blade
US3067982A (en) * 1958-08-25 1962-12-11 California Inst Res Found Porous wall turbine blades and method of manufacture
US3032316A (en) * 1958-10-09 1962-05-01 Bruce E Kramer Jet turbine buckets and method of making the same
US3402914A (en) * 1965-02-10 1968-09-24 Curtiss Wright Corp Method of controlling the permeability of a porous material, and turbine blade formed thereby
US3647316A (en) * 1970-04-28 1972-03-07 Curtiss Wright Corp Variable permeability and oxidation-resistant airfoil

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5422188A (en) * 1991-05-03 1995-06-06 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Part made from ceramic composite having a metallic coating, process for producing same and powder composition used

Also Published As

Publication number Publication date
JPS5254810A (en) 1977-05-04
NL7609371A (nl) 1977-05-03
NO763676L (fr) 1977-05-02
US4040159A (en) 1977-08-09
GB1554195A (en) 1979-10-17
DE2648026A1 (de) 1977-05-05

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Legal Events

Date Code Title Description
ST Notification of lapse