GB909948A - Method of making turbine blades - Google Patents

Method of making turbine blades

Info

Publication number
GB909948A
GB909948A GB13287/60A GB1328760A GB909948A GB 909948 A GB909948 A GB 909948A GB 13287/60 A GB13287/60 A GB 13287/60A GB 1328760 A GB1328760 A GB 1328760A GB 909948 A GB909948 A GB 909948A
Authority
GB
United Kingdom
Prior art keywords
heat treatment
nickel
recrystallation
ingot
workpiece
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
Application number
GB13287/60A
Inventor
Jack Raymond Bird
Doulas Wilson Hall
David Anthony Denton
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
Priority to GB13287/60A priority Critical patent/GB909948A/en
Priority to US101806A priority patent/US3228095A/en
Publication of GB909948A publication Critical patent/GB909948A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21K—MAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K3/00—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
    • B21K3/04—Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like blades, e.g. for turbines; Upsetting of blade roots
    • 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
    • B23P15/02—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from one piece
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • 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
    • Y10T29/4998—Combined manufacture including applying or shaping of fluent material
    • Y10T29/49988—Metal casting

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

909,948. Making gas-turbine blades; working at specified temperatures; forging. ROLLSROYCE Ltd. April 6, 1961 [April 13, 1960], No. 13287/60. Drawings to Specification. Classes 83 (2) and 83 (4). A gas-turbine blade is made, from an alloy having the following percentage composition by weight: Cr 5-30 ; Co 0-30 ; Mo 5-30 ; W 0-20 ; Ti 0.5-7 ; A1 2-17 ; B 0.003-0.3 ; Zr 0.001-1 ; C 0.01-5 ; Ca 0-0.1 ; Mn 0- 0.4; Si 0-0.4 ; Fe 0-1 ; Be 0-0.5 ; Ta 0-5 ; Nb 0-5 ; Hf 0-10 ; S 0-0.005 ; P 0-0.008 ; V 0-3 ; N2 0-0.2 ; Mg 0-0.15 ; Cu 0-0.5 ; Pb 0-0.005 ; combined O 2 0-0.2 ; rare earths 0-0.2 ; the combined titanium and aluminium content being at least 6.5% and the balance of the alloy being nickel and impurities; there being at least 35% of nickel if cobalt is present or at least 45% of nickel if cobalt is not present, by the method of casting an ingot and forming one blade from substantially the whole of the ingot by a process involving forging. The ingot is cast into a dumb-bell shape which is inspected by X-ray method and given an homogenization heat treatment at 1200‹ C. for 2-24 hours. A number of castings may be interconnected by a single riser. After machining to size the surface of the workpiece is cold worked by shot peening, reeling or cold swaging and it is given a first recrystallation heat treatment at 1150-1250‹ C. for ten minutes and quenched if necessary. The workpiece is then vapour blasted, coated with nickel or glass as a lubricant and a first press forging operation is performed. This is followed by a second recrystallation heat treatment at 1200‹ C. and the workpiece is then forged to final shape. A further recrystallization heat treatment may be necessary and finally a solution and ageing heat treatment are given at one or two temperatures. The homogenization heat treatment, machining, cold surface working, first recrystallation heat treatment and vapour-blasting may be omitted. Specification 909,356 is referred to.
GB13287/60A 1960-04-13 1960-04-13 Method of making turbine blades Expired GB909948A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB13287/60A GB909948A (en) 1960-04-13 1960-04-13 Method of making turbine blades
US101806A US3228095A (en) 1960-04-13 1961-04-10 Method of making turbine blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB13287/60A GB909948A (en) 1960-04-13 1960-04-13 Method of making turbine blades

Publications (1)

Publication Number Publication Date
GB909948A true GB909948A (en) 1962-11-07

Family

ID=10020222

Family Applications (1)

Application Number Title Priority Date Filing Date
GB13287/60A Expired GB909948A (en) 1960-04-13 1960-04-13 Method of making turbine blades

Country Status (2)

Country Link
US (1) US3228095A (en)
GB (1) GB909948A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106563753A (en) * 2015-10-08 2017-04-19 陕西宏远航空锻造有限责任公司 Forging method of high-temperature alloy turbine moving blade

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE658054A (en) * 1964-01-08
US4530727A (en) * 1982-02-24 1985-07-23 The United States Of America As Represented By The Department Of Energy Method for fabricating wrought components for high-temperature gas-cooled reactors and product
US4528048A (en) * 1982-12-06 1985-07-09 United Technologies Corporation Mechanically worked single crystal article
US5980653A (en) * 1997-01-23 1999-11-09 Ngk Metals Corporation Nickel-copper-beryllium alloy compositions
US6054197A (en) * 1997-09-19 2000-04-25 State University Of New York At Albany Structural elements
US20050155679A1 (en) * 2003-04-09 2005-07-21 Coastcast Corporation CoCr alloys and methods for making same
FR2867095B1 (en) * 2004-03-03 2007-04-20 Snecma Moteurs METHOD FOR MANUFACTURING A HOLLOW DAWN FOR TURBOMACHINE
US10414003B2 (en) * 2013-09-30 2019-09-17 Liburdi Engineering Limited Welding material for welding of superalloys
JP6506389B2 (en) * 2014-04-28 2019-04-24 リバルディ エンジニアリング リミテッド Malleable boron supported nickel-based welding material
US10493568B2 (en) 2014-10-21 2019-12-03 Liburdi Engineering Limited Ductile boron bearing nickel based welding material
CZ2015749A3 (en) * 2015-10-25 2017-05-24 Univerzita J. E. Purkyně V Ústí Nad Labem An aluminium alloy, especially for the production of thin-walled and dimensionally complex castings
RU2737835C1 (en) * 2020-06-03 2020-12-03 Акционерное общество "Объединенная двигателестроительная корпорация (АО "ОДК") Nickel-based heat-resistant wrought alloy and article made from it
CN114160728A (en) * 2021-11-18 2022-03-11 王江明 Machining process of aviation part turbine fan blade

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA548777A (en) * 1957-11-12 G. Bieber Clarence Nickel-base heat-resistant alloy
US2447897A (en) * 1946-05-23 1948-08-24 Armco Steel Corp High-temperature stainless steel
US2977222A (en) * 1955-08-22 1961-03-28 Int Nickel Co Heat-resisting nickel base alloys
US2987806A (en) * 1956-05-24 1961-06-13 Thompson Ramo Wooldridge Inc Method of making turbine blades and the like
US3047381A (en) * 1958-02-03 1962-07-31 Gen Motors Corp High temperature heat and creep resistant alloy
US3110587A (en) * 1959-06-23 1963-11-12 Int Nickel Co Nickel-chromium base alloy
GB887746A (en) * 1959-11-04 1962-01-24 Mond Nickel Co Ltd Creep-resistant nickel-base alloys

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106563753A (en) * 2015-10-08 2017-04-19 陕西宏远航空锻造有限责任公司 Forging method of high-temperature alloy turbine moving blade

Also Published As

Publication number Publication date
US3228095A (en) 1966-01-11

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