GB755610A - Improvements in the manufacture of turbine blades - Google Patents
Improvements in the manufacture of turbine bladesInfo
- 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
Links
Classifications
-
- 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
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.
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)
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 |
-
1953
- 1953-04-30 GB GB1201753A patent/GB755610A/en not_active Expired
Cited By (21)
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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