GB755610A - Improvements in the manufacture of turbine blades - Google Patents

Improvements in the manufacture of turbine blades

Info

Publication number
GB755610A
GB755610A GB1201753A GB1201753A GB755610A GB 755610 A GB755610 A GB 755610A GB 1201753 A GB1201753 A GB 1201753A GB 1201753 A GB1201753 A GB 1201753A GB 755610 A GB755610 A GB 755610A
Authority
GB
United Kingdom
Prior art keywords
turbine blades
manufacture
blade
group xxii
wiggin
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
GB1201753A
Inventor
Alexander Barbour Graham
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.)
Henry Wiggin and Co Ltd
Original Assignee
Henry Wiggin and Co Ltd
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 Henry Wiggin and Co Ltd filed Critical Henry Wiggin and Co Ltd
Priority to GB1201753A priority Critical patent/GB755610A/en
Publication of GB755610A publication Critical patent/GB755610A/en
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
    • B23P15/02Making 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Extrusion Moulding Of Plastics Or The Like (AREA)

Abstract

755,610. Turbine blades. WIGGIN & CO., Ltd., H. July 30, 1954 [April 30, 1953], No. 12017/53. Class 110(3) [Also in Group XXII] A gas turbine blade having longitudinal holes 6, 3 therein and an integral root 4 is made by an extruding peration (see Group XXII). The blade is of nickel chromium creep - resisting alloy.
GB1201753A 1953-04-30 1953-04-30 Improvements in the manufacture of turbine blades Expired GB755610A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1201753A GB755610A (en) 1953-04-30 1953-04-30 Improvements in the manufacture of turbine blades

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1201753A GB755610A (en) 1953-04-30 1953-04-30 Improvements in the manufacture of turbine blades

Publications (1)

Publication Number Publication Date
GB755610A true GB755610A (en) 1956-08-22

Family

ID=9996902

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1201753A Expired GB755610A (en) 1953-04-30 1953-04-30 Improvements in the manufacture of turbine blades

Country Status (1)

Country Link
GB (1) GB755610A (en)

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2914841A (en) * 1956-10-04 1959-12-01 Int Nickel Co Manufacture of hollow turbine blades
US2965955A (en) * 1956-10-23 1960-12-27 Int Nickel Co Production of hollow turbine blades
US2965959A (en) * 1956-12-04 1960-12-27 Int Nickel Co Method of locating the blind terminals of filled holes in a deformed metal object
US2970368A (en) * 1957-05-23 1961-02-07 Int Nickel Co Hollow turbine or compressor blades
US2972182A (en) * 1957-02-22 1961-02-21 Rolls Royce Turbine and compressor blades
US2972805A (en) * 1956-06-20 1961-02-28 Int Nickel Co Production of hollow metal articles
US2972807A (en) * 1957-02-19 1961-02-28 Int Nickel Co Method of making hollow turbine or compressor blades
US2972806A (en) * 1957-01-30 1961-02-28 Int Nickel Co Production of turbine or compressor blades
US2975509A (en) * 1956-05-07 1961-03-21 Cefilac Methods of extruding metals
US2986806A (en) * 1957-01-21 1961-06-06 Int Nickel Co Production of turbine or compressor blades
US3014692A (en) * 1956-12-04 1961-12-26 Int Nickel Co Gas turbine blades
US3028661A (en) * 1956-09-03 1962-04-10 Int Nickel Co Manufacture of turbine or compressor blades
US3039178A (en) * 1957-01-11 1962-06-19 Rolls Royce Manufacture by extrusion of turbine engine blades
US3044153A (en) * 1956-10-12 1962-07-17 Rolls Royce Manufacture by extrusion of turbine engine blades
US3045328A (en) * 1956-05-08 1962-07-24 Int Nickel Co Manufacture of hollow turbine blades
DE1144571B (en) * 1958-02-10 1963-02-28 Rolls Royce Hole arrangement in billets for the production of gas turbine and compressor blades with cooling ducts by deformation
US3088192A (en) * 1957-04-26 1963-05-07 Int Nickel Co Method of joining turbine blade parts
US3107416A (en) * 1958-05-20 1963-10-22 Int Nickel Co Method of making turbine and compressor blades
US3112557A (en) * 1958-02-10 1963-12-03 Rolls Royce Turbine and compressor blades
DE1219137B (en) * 1960-12-16 1966-06-16 Atomic Energy Authority Uk Process for the manufacture of a wrapped nuclear reactor fuel plate by multi-stage rolling
US3707754A (en) * 1969-07-11 1973-01-02 Secr Defence Metal working

Cited By (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2975509A (en) * 1956-05-07 1961-03-21 Cefilac Methods of extruding metals
US3045328A (en) * 1956-05-08 1962-07-24 Int Nickel Co Manufacture of hollow turbine blades
US2972805A (en) * 1956-06-20 1961-02-28 Int Nickel Co Production of hollow metal articles
US3028661A (en) * 1956-09-03 1962-04-10 Int Nickel Co Manufacture of turbine or compressor blades
US2914841A (en) * 1956-10-04 1959-12-01 Int Nickel Co Manufacture of hollow turbine blades
US3044153A (en) * 1956-10-12 1962-07-17 Rolls Royce Manufacture by extrusion of turbine engine blades
US2965955A (en) * 1956-10-23 1960-12-27 Int Nickel Co Production of hollow turbine blades
US3014692A (en) * 1956-12-04 1961-12-26 Int Nickel Co Gas turbine blades
US2965959A (en) * 1956-12-04 1960-12-27 Int Nickel Co Method of locating the blind terminals of filled holes in a deformed metal object
US3039178A (en) * 1957-01-11 1962-06-19 Rolls Royce Manufacture by extrusion of turbine engine blades
US2986806A (en) * 1957-01-21 1961-06-06 Int Nickel Co Production of turbine or compressor blades
US2972806A (en) * 1957-01-30 1961-02-28 Int Nickel Co Production of turbine or compressor blades
US2972807A (en) * 1957-02-19 1961-02-28 Int Nickel Co Method of making hollow turbine or compressor blades
US2972182A (en) * 1957-02-22 1961-02-21 Rolls Royce Turbine and compressor blades
US3088192A (en) * 1957-04-26 1963-05-07 Int Nickel Co Method of joining turbine blade parts
US2970368A (en) * 1957-05-23 1961-02-07 Int Nickel Co Hollow turbine or compressor blades
DE1144571B (en) * 1958-02-10 1963-02-28 Rolls Royce Hole arrangement in billets for the production of gas turbine and compressor blades with cooling ducts by deformation
US3112557A (en) * 1958-02-10 1963-12-03 Rolls Royce Turbine and compressor blades
US3107416A (en) * 1958-05-20 1963-10-22 Int Nickel Co Method of making turbine and compressor blades
DE1219137B (en) * 1960-12-16 1966-06-16 Atomic Energy Authority Uk Process for the manufacture of a wrapped nuclear reactor fuel plate by multi-stage rolling
US3707754A (en) * 1969-07-11 1973-01-02 Secr Defence Metal working

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