DE1915532B2 - - Google Patents

Info

Publication number
DE1915532B2
DE1915532B2 DE1915532A DE1915532A DE1915532B2 DE 1915532 B2 DE1915532 B2 DE 1915532B2 DE 1915532 A DE1915532 A DE 1915532A DE 1915532 A DE1915532 A DE 1915532A DE 1915532 B2 DE1915532 B2 DE 1915532B2
Authority
DE
Germany
Prior art keywords
blade
parts
soldering
solder
sheet
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.)
Granted
Application number
DE1915532A
Other languages
German (de)
English (en)
Other versions
DE1915532A1 (de
DE1915532C3 (de
Inventor
John Windsor Skipton Yorkshire Jones (Ver. Koenigreich)
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Publication of DE1915532A1 publication Critical patent/DE1915532A1/de
Publication of DE1915532B2 publication Critical patent/DE1915532B2/de
Application granted granted Critical
Publication of DE1915532C3 publication Critical patent/DE1915532C3/de
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/04Making 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
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49336Blade making
    • Y10T29/49339Hollow blade
    • Y10T29/49341Hollow blade with cooling passage

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE1915532A 1968-03-27 1969-03-26 Verfahren zur Hartverlötung von Schaufelteilen oder -rohlingsteilen Expired DE1915532C3 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB04781/68A GB1224521A (en) 1968-03-27 1968-03-27 Method of making an aerofoil-shaped blade or blade blank

Publications (3)

Publication Number Publication Date
DE1915532A1 DE1915532A1 (de) 1969-12-11
DE1915532B2 true DE1915532B2 (en, 2012) 1980-02-21
DE1915532C3 DE1915532C3 (de) 1980-10-09

Family

ID=10047379

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1915532A Expired DE1915532C3 (de) 1968-03-27 1969-03-26 Verfahren zur Hartverlötung von Schaufelteilen oder -rohlingsteilen

Country Status (4)

Country Link
US (1) US3656222A (en, 2012)
DE (1) DE1915532C3 (en, 2012)
FR (2) FR2004807A1 (en, 2012)
GB (1) GB1224521A (en, 2012)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4195396A (en) * 1977-12-15 1980-04-01 Trw Inc. Method of forming an airfoil with inner and outer shroud sections
US5152059A (en) * 1980-09-19 1992-10-06 Rolls-Royce Plc Manufacture of cooled aerofoil blades
GB2095589B (en) * 1981-04-01 1984-08-01 Rolls Royce Method of making a blade for a gas turbine engine
GB2096525B (en) * 1981-04-14 1984-09-12 Rolls Royce Manufacturing gas turbine engine blades
US4619580A (en) * 1983-09-08 1986-10-28 The Boeing Company Variable camber vane and method therefor
US5176499A (en) * 1991-06-24 1993-01-05 General Electric Company Photoetched cooling slots for diffusion bonded airfoils
US5259730A (en) * 1991-11-04 1993-11-09 General Electric Company Impingement cooled airfoil with bonding foil insert
US5318406A (en) * 1992-11-02 1994-06-07 General Electric Company Multipart gas turbine blade
US5503532A (en) * 1994-11-14 1996-04-02 General Electric Company Diffusion bonded airfoil and method
US6162347A (en) * 1998-09-28 2000-12-19 General Electric Company Co-machined bonded airfoil
US6193465B1 (en) 1998-09-28 2001-02-27 General Electric Company Trapped insert turbine airfoil
US6505672B2 (en) 2001-05-22 2003-01-14 Howmet Research Corporation Fugitive patterns for investment casting
US7371049B2 (en) 2005-08-31 2008-05-13 United Technologies Corporation Manufacturable and inspectable microcircuit cooling for blades
US20070163114A1 (en) * 2006-01-13 2007-07-19 General Electric Company Methods for fabricating components
GB0701904D0 (en) * 2007-02-01 2007-03-14 Rolls Royce Plc A method of manufacturing a component by consolidating powder material
FR2984786B1 (fr) * 2011-12-23 2014-01-03 Snecma Procede de fabrication d'une aube creuse
CN105765305B (zh) 2013-11-27 2018-05-08 通用电气公司 具有流体锁和吹扫设备的燃料喷嘴
WO2015147935A1 (en) 2013-12-23 2015-10-01 General Electric Company Fuel nozzle with flexible support structures
JP6606080B2 (ja) 2013-12-23 2019-11-13 ゼネラル・エレクトリック・カンパニイ エアアシスト式燃料噴射用の燃料ノズル構造体

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2807437A (en) * 1952-05-01 1957-09-24 Thompson Prod Inc Method for making intricate hollow powder metal parts
US2821495A (en) * 1955-06-24 1958-01-28 Aluminum Co Of America Brazing and heat treatment of aluminum base alloy castings
US3088192A (en) * 1957-04-26 1963-05-07 Int Nickel Co Method of joining turbine blade parts
US3110102A (en) * 1958-10-31 1963-11-12 North American Aviation Inc Method of fusion joining employing stop-off material
US3025596A (en) * 1959-06-26 1962-03-20 Combustion Eng Braze bonding of concentric tubes and shells and the like
US3083451A (en) * 1959-09-21 1963-04-02 Ass Elect Ind Manchester Ltd Beryllium brazing
US3197858A (en) * 1961-07-28 1965-08-03 Westinghouse Electric Corp Process for diffusion-bonding
US3170234A (en) * 1962-09-17 1965-02-23 Charles O Tarr Jointing of refractory metals by solidstate diffusion bonding
US3329596A (en) * 1963-08-07 1967-07-04 Gen Electric Method of electrolytically machining branch passages providing communication betweenmain passages in a metal article
US3342971A (en) * 1964-06-16 1967-09-19 Gen Dynamics Corp Method for brazing super alloys and refractory metals
US3349465A (en) * 1965-05-14 1967-10-31 United Aircraft Corp Tube-to-sheet joint making

Also Published As

Publication number Publication date
DE1915532A1 (de) 1969-12-11
FR2004807A1 (en, 2012) 1969-12-05
GB1224521A (en) 1971-03-10
DE1915532C3 (de) 1980-10-09
US3656222A (en) 1972-04-18
FR2077495A1 (en, 2012) 1971-10-29

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Legal Events

Date Code Title Description
OGA New person/name/address of the applicant
C3 Grant after two publication steps (3rd publication)
8339 Ceased/non-payment of the annual fee