GB750011A - Process for making turbine and like blades - Google Patents
Process for making turbine and like bladesInfo
- Publication number
- GB750011A GB750011A GB1573953A GB1573953A GB750011A GB 750011 A GB750011 A GB 750011A GB 1573953 A GB1573953 A GB 1573953A GB 1573953 A GB1573953 A GB 1573953A GB 750011 A GB750011 A GB 750011A
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- blank
- blades
- rolls
- blanks
- 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
- B21H—MAKING PARTICULAR METAL OBJECTS BY ROLLING, e.g. SCREWS, WHEELS, RINGS, BARRELS, BALLS
- B21H7/00—Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons
- B21H7/16—Making articles not provided for in the preceding groups, e.g. agricultural tools, dinner forks, knives, spoons turbine blades; compressor blades; propeller blades
Landscapes
- Life Sciences & Earth Sciences (AREA)
- Agronomy & Crop Science (AREA)
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Forging (AREA)
Abstract
750,011. Making turbine &c.blades. POWER JETS (RESEARCH & DEVELOPMENT), Ltd. May 27,1954 [June 8, 1953], No. 15739/53. Classes 83 (2) and 83 (4). Rolling; forging.-In a method of making turbine blades, pairs of rough blades are rolled from blanks 1, Fig. 2, with an enlarged portion 2 formed mid-way between the ends from which the roots of the blade pairs are formed. The blanks 1 which may be previously tapered towards the ends as by rotary swaging are rolled between a pair of rolls 29, having recesses 29a to accommodate the enlargement 2. The rolls 29 are rotated firstly in one direction and then in the opposite direction to impart a blade form to each end of the blank in succession. Shrouds 31 on one roll guide the blank which may have a twist imparted during rolling or the twist may be imparted subsequently. The method is also applicable to blade cores which are fluted to provide cooling passages and around which an aerofoil blade surface is subsequently placed. Blade roots 3, Fig. 3, may be formed by suitably shaping the recesses 29a in the rolls or may be formed subsequently after dividing the blank in two. The enlargement 2 is initially formed in the blank by upsetting in a forging machine similar to that described in Specification 749,997 but modified to accommodate blanks of two blade lengths.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1573953A GB750011A (en) | 1953-06-08 | 1953-06-08 | Process for making turbine and like blades |
GB1617054A GB770192A (en) | 1953-06-08 | 1954-06-01 | Process for making turbine or compressor blades |
US511083A US3002264A (en) | 1953-06-08 | 1955-05-25 | Process for making turbine or compressor blades |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1573953A GB750011A (en) | 1953-06-08 | 1953-06-08 | Process for making turbine and like blades |
Publications (1)
Publication Number | Publication Date |
---|---|
GB750011A true GB750011A (en) | 1956-06-06 |
Family
ID=10064622
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1573953A Expired GB750011A (en) | 1953-06-08 | 1953-06-08 | Process for making turbine and like blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB750011A (en) |
-
1953
- 1953-06-08 GB GB1573953A patent/GB750011A/en not_active Expired
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