GB934647A - Improvements relating to the production of turbine or compressor blades - Google Patents

Improvements relating to the production of turbine or compressor blades

Info

Publication number
GB934647A
GB934647A GB14323/61A GB1432361A GB934647A GB 934647 A GB934647 A GB 934647A GB 14323/61 A GB14323/61 A GB 14323/61A GB 1432361 A GB1432361 A GB 1432361A GB 934647 A GB934647 A GB 934647A
Authority
GB
United Kingdom
Prior art keywords
billet
hole
filled
produced
length
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
GB14323/61A
Inventor
Barclay Keegan
Roderick Charles Mackenzie
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 GB14323/61A priority Critical patent/GB934647A/en
Priority to US188197A priority patent/US3201856A/en
Priority to BE616751A priority patent/BE616751A/en
Publication of GB934647A publication Critical patent/GB934647A/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
    • B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21C—MANUFACTURE OF METAL SHEETS, WIRE, RODS, TUBES OR PROFILES, OTHERWISE THAN BY ROLLING; AUXILIARY OPERATIONS USED IN CONNECTION WITH METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL
    • B21C23/00—Extruding metal; Impact extrusion
    • B21C23/02—Making uncoated products
    • B21C23/04—Making uncoated products by direct extrusion
    • B21C23/14—Making other products
    • B21C23/16—Making turbo blades or propellers
    • 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
    • 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
    • Y10T29/4981—Utilizing transitory attached element or associated separate material

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Extrusion Of Metal (AREA)

Abstract

934,647. Making turbine blades. HENRY WIGGIN & CO. Ltd. April 12, 1962 [April 20, 1961], No. 14323/61. Class 83 (2). A blank for a turbine blade with longitudinal passages is produced by extruding a billet having drilled holes filled with filler rods that after elongation of the billet can be removed to leave the passages, and the resistance to deformation of the billet is reduced over a length from an end of the billet due to the presence of the filled holes. A rectangular billet 1 to be extruded has an axial hole 2 drilled therein to receive a filler rod 3. A length " L " of the hole is incompletely filled by the rod 3, which is drilled, slotted or tapered to reduce its crosssectional area over this length. The reduced resistance to deformation in the incompletely filled region results in a small passage 7 being produced, as compared with the passage 8 produced in the completely filled region of the hole 2. The reduced part of the filler rod may be positioned at either end of the hole 2. Fig. 10 shows a billet which has been partially extruded to leave a part 13 from which the root 14 of the blade is subsequently formed. Specification 763,115 is referred to.
GB14323/61A 1961-04-20 1961-04-20 Improvements relating to the production of turbine or compressor blades Expired GB934647A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB14323/61A GB934647A (en) 1961-04-20 1961-04-20 Improvements relating to the production of turbine or compressor blades
US188197A US3201856A (en) 1961-04-20 1962-04-17 Process of producing holes with reduced openings
BE616751A BE616751A (en) 1961-04-20 1962-04-20 Reduced opening holes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB14323/61A GB934647A (en) 1961-04-20 1961-04-20 Improvements relating to the production of turbine or compressor blades

Publications (1)

Publication Number Publication Date
GB934647A true GB934647A (en) 1963-08-21

Family

ID=10039121

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14323/61A Expired GB934647A (en) 1961-04-20 1961-04-20 Improvements relating to the production of turbine or compressor blades

Country Status (3)

Country Link
US (1) US3201856A (en)
BE (1) BE616751A (en)
GB (1) GB934647A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2328793A1 (en) * 1973-06-06 1975-01-02 Bayer Ag PROCESS FOR MANUFACTURING HOLLOW SCREWS FOR HEAT EXCHANGERS
US4639568A (en) * 1984-07-13 1987-01-27 Ex-Cell-O Corporation Apparatus and method for finishing fuel injector spray tips using EDM
DE102008052409A1 (en) * 2008-10-21 2010-04-22 Rolls-Royce Deutschland Ltd & Co Kg Turbomachine with near-suction edge energization

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2093775A (en) * 1931-10-29 1937-09-21 Thompson Prod Inc Method of making valves
US2047555A (en) * 1933-05-31 1936-07-14 Parsons & Co Ltd C A Manufacture of hollow turbine blades
US2948052A (en) * 1956-06-30 1960-08-09 Teves Kg Alfred Method of manufacturing hollow poppet valves for internal combustion engines
US3044153A (en) * 1956-10-12 1962-07-17 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
BE564389A (en) * 1957-01-30
US2970368A (en) * 1957-05-23 1961-02-07 Int Nickel Co Hollow turbine or compressor blades

Also Published As

Publication number Publication date
BE616751A (en) 1962-08-16
US3201856A (en) 1965-08-24

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