GB726909A - Improvements in or relating to the manufacture of turbine and like blades - Google Patents
Improvements in or relating to the manufacture of turbine and like bladesInfo
- Publication number
- GB726909A GB726909A GB4919/52A GB491952A GB726909A GB 726909 A GB726909 A GB 726909A GB 4919/52 A GB4919/52 A GB 4919/52A GB 491952 A GB491952 A GB 491952A GB 726909 A GB726909 A GB 726909A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- turbine
- section
- die
- head
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
- F01D5/12—Blades
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Architecture (AREA)
- General Engineering & Computer Science (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Abstract
726,909. Making turbine blades. OMES, Ltd. Jan. 15, 1953 [Feb. 25, 1952], No. 4919/52. Addition to 569,514. Class 83 (2). A modification of the invention claimed in the parent Specification comprises a method of making a turbine or compressor blade from aerofoil section stock whose cross-section approximates to the section of the finished blade but is narrower and thicker, by upsetting a head on the stock in an electrical upsetting machine, reheating the entire blade and die-pressing both the blade portion 22 and the head 23 to the required form. The die may also impart blade twist and form locating lugs 24, 125 for use in any subsequent machining operations after which the lugs are removed. The blade may finally be electro-polished. Preferably the blade is made of aluminium bronze or stainless steel.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4919/52A GB726909A (en) | 1952-02-25 | 1952-02-25 | Improvements in or relating to the manufacture of turbine and like blades |
FR1060577D FR1060577A (en) | 1952-02-25 | 1952-07-24 | Improvements in the manufacture of turbine blades and the like |
CH310902D CH310902A (en) | 1952-02-25 | 1952-09-27 | Process for the manufacture of blades for turbomachinery. |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4919/52A GB726909A (en) | 1952-02-25 | 1952-02-25 | Improvements in or relating to the manufacture of turbine and like blades |
GB1060577X | 1952-02-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB726909A true GB726909A (en) | 1955-03-23 |
Family
ID=26239467
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4919/52A Expired GB726909A (en) | 1952-02-25 | 1952-02-25 | Improvements in or relating to the manufacture of turbine and like blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB726909A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2999303A (en) * | 1958-05-21 | 1961-09-12 | Rolls Royce | Blades for gas turbine engines |
US3026605A (en) * | 1956-09-13 | 1962-03-27 | Int Nickel Co | Hollow turbine blades |
US3028661A (en) * | 1956-09-03 | 1962-04-10 | Int Nickel Co | Manufacture of turbine or compressor blades |
US3747182A (en) * | 1970-05-07 | 1973-07-24 | United Aircraft Corp | Method of fabricating a hollow turbine blade having an insert therein |
EP1500444A1 (en) * | 2003-07-23 | 2005-01-26 | Snecma Moteurs | Process for the manufacture of forgings by precision forging |
EP1841562A1 (en) * | 2004-12-21 | 2007-10-10 | Pratt & Whitney Canada Corp. | Gas turbine fuel nozzle manufacturing |
-
1952
- 1952-02-25 GB GB4919/52A patent/GB726909A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3028661A (en) * | 1956-09-03 | 1962-04-10 | Int Nickel Co | Manufacture of turbine or compressor blades |
US3026605A (en) * | 1956-09-13 | 1962-03-27 | Int Nickel Co | Hollow turbine blades |
US2999303A (en) * | 1958-05-21 | 1961-09-12 | Rolls Royce | Blades for gas turbine engines |
US3747182A (en) * | 1970-05-07 | 1973-07-24 | United Aircraft Corp | Method of fabricating a hollow turbine blade having an insert therein |
EP1500444A1 (en) * | 2003-07-23 | 2005-01-26 | Snecma Moteurs | Process for the manufacture of forgings by precision forging |
FR2857889A1 (en) * | 2003-07-23 | 2005-01-28 | Snecma Moteurs | PROCESS FOR PRODUCING PARTS BY PRECISION FORGING |
EP1841562A1 (en) * | 2004-12-21 | 2007-10-10 | Pratt & Whitney Canada Corp. | Gas turbine fuel nozzle manufacturing |
EP1841562A4 (en) * | 2004-12-21 | 2010-09-01 | Pratt & Whitney Canada | Gas turbine fuel nozzle manufacturing |
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