GB721478A - Improvements relating to the shaping of metal articles - Google Patents
Improvements relating to the shaping of metal articlesInfo
- Publication number
- GB721478A GB721478A GB829452A GB829452A GB721478A GB 721478 A GB721478 A GB 721478A GB 829452 A GB829452 A GB 829452A GB 829452 A GB829452 A GB 829452A GB 721478 A GB721478 A GB 721478A
- Authority
- GB
- United Kingdom
- Prior art keywords
- face
- blade
- die
- pressure
- turbine
- 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
- 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
- B23P15/04—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine or like blades from several pieces
Abstract
721,478. Making turbine blades. METROPOLITAN-VICKERS ELECTRICAL CO., Ltd. March 5, 1953,[April 1, 1952], No. 8294/62. Classes 83 (2) and 83 (4). Stamping.-A method of forging a turbine or compressor blade casting to produce accurate shaping of a face thereof to a predetermined form consists in forcing said face against a die surface by the application of pressure at the opposite face of said blade casting through the intermediary of a loose pad of material deformable under pressure and without application of heat so as to ensure uniform pressure distribution on the blade casting to transfer errors from said face in contact with the die surface to the opposite face. The press tool comprises dies 1 and 2 mounted on plates 11 and 21 respectively located by pillars 3 over which slide bushes 3<SP>1</SP> in the plate 2<SP>1</SP> when the plate 21 is depressed. Springs 4 keep the dies apart when no pressure is being exerted. The bottom die 1 has an accurate convex face 5 corresponding to the accurate shape desired for the concave face 6 of the cast turbine or compressor blade 7 which is accurately located in the die by means of pins 14 and a spring-loaded plunger 10 located in semi-cylindrical grooves on each die. In operation, a turbine or compressor blade of high tensile steel is heated to say 650‹ C. and positioned in the bottom die of the press tool. A pad of asbestos covered by graphite and white spirit as lubricant is placed over the blade and the press operated at a pressure of 50 tons per square inch, whereby the under face of the blade is caused accurately to conform to the shape of the bottom die. All errors are now contained in the upper face of the blade and these are later removed by polishing or grinding. Turbine blades of austentic steel can be pressed to accurate shape when cold, using rubber as the deformable material for the pad.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB829452A GB721478A (en) | 1952-04-01 | 1952-04-01 | Improvements relating to the shaping of metal articles |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB829452A GB721478A (en) | 1952-04-01 | 1952-04-01 | Improvements relating to the shaping of metal articles |
Publications (1)
Publication Number | Publication Date |
---|---|
GB721478A true GB721478A (en) | 1955-01-05 |
Family
ID=9849758
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB829452A Expired GB721478A (en) | 1952-04-01 | 1952-04-01 | Improvements relating to the shaping of metal articles |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB721478A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1568424A1 (en) * | 2004-02-27 | 2005-08-31 | Snecma Moteurs | Press for holding and pressing a workpiece |
FR2970192A1 (en) * | 2011-01-10 | 2012-07-13 | Snecma | TOOLING AND METHOD FOR HOT FORGING SHEETS |
WO2018069933A1 (en) * | 2016-10-12 | 2018-04-19 | Bharat Forge Limited | Aero engine fan blade and its manufacturing |
-
1952
- 1952-04-01 GB GB829452A patent/GB721478A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1568424A1 (en) * | 2004-02-27 | 2005-08-31 | Snecma Moteurs | Press for holding and pressing a workpiece |
FR2866821A1 (en) * | 2004-02-27 | 2005-09-02 | Snecma Moteurs | PRESS FOR MAINTAINING AND PRESSING A PIECE |
US7194887B2 (en) | 2004-02-27 | 2007-03-27 | Snecma Moteurs | Press for holding and pressing a workpiece |
FR2970192A1 (en) * | 2011-01-10 | 2012-07-13 | Snecma | TOOLING AND METHOD FOR HOT FORGING SHEETS |
US8732920B2 (en) | 2011-01-10 | 2014-05-27 | Snecma | Tooling and a method for hot forging pieces of sheet metal |
WO2018069933A1 (en) * | 2016-10-12 | 2018-04-19 | Bharat Forge Limited | Aero engine fan blade and its manufacturing |
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