GB602244A - Improvements in or relating to turbine buckets for exhaust turbine superchargers - Google Patents
Improvements in or relating to turbine buckets for exhaust turbine superchargersInfo
- Publication number
- GB602244A GB602244A GB53045A GB53045A GB602244A GB 602244 A GB602244 A GB 602244A GB 53045 A GB53045 A GB 53045A GB 53045 A GB53045 A GB 53045A GB 602244 A GB602244 A GB 602244A
- Authority
- GB
- United Kingdom
- Prior art keywords
- per cent
- turbine
- relating
- superchargers
- buckets
- 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
- F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
Abstract
Turbine buckets having high tensile strength and high corrosion-resistance when exposed to a high-temperature, high-velocity stream of combustion gases are cast of alloys consisting of cobalt 50 to 70 per cent, and chromium 20 to 40 per cent, molybdenum and/or tungsten 3 to 5 per cent, and carbon up to 0.5 per cent. The alloys may also contain silicon up to 1 per cent and manganese up to 1 per cent. A preferred composition consists of cobalt 60 to 65 per cent, chromium 28 to 32 per cent, molybdenum 5 to 7 per cent, silicon .10 to 1.0 per cent, manganese .20 to 1.0 per cent, carbon up to .50 per cent.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB53045A GB602244A (en) | 1945-01-05 | 1945-01-05 | Improvements in or relating to turbine buckets for exhaust turbine superchargers |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB53045A GB602244A (en) | 1945-01-05 | 1945-01-05 | Improvements in or relating to turbine buckets for exhaust turbine superchargers |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB602244A true GB602244A (en) | 1948-05-24 |
Family
ID=9705966
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB53045A Expired GB602244A (en) | 1945-01-05 | 1945-01-05 | Improvements in or relating to turbine buckets for exhaust turbine superchargers |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB602244A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2855295A (en) * | 1956-12-26 | 1958-10-07 | Gen Electric | Cobalt base hard surfacing alloy |
-
1945
- 1945-01-05 GB GB53045A patent/GB602244A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2855295A (en) * | 1956-12-26 | 1958-10-07 | Gen Electric | Cobalt base hard surfacing alloy |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| GB623508A (en) | Improvements relating to gas-turbine-engines | |
| JPS51133807A (en) | Turbo type impeller with high performance | |
| GB602244A (en) | Improvements in or relating to turbine buckets for exhaust turbine superchargers | |
| GB676441A (en) | Improved sintered material, particularly suitable for cutting-tools and heat-engine elements, especially turbine-blades and jet-propulsion nozzles | |
| AT168357B (en) | Drive turbine, in particular for exhaust gas turbochargers | |
| GB688299A (en) | Improvements in or relating to composite metal products and method of making same | |
| GB586556A (en) | Improvements in internal combustion turbine plant for propulsion | |
| GB749365A (en) | Improvements in or relating to the hot working of titanium and titanium base alloy materials | |
| GB1382026A (en) | Intermetallic composite materials | |
| GB616207A (en) | Improvements relating to alloys for use at elevated temperatures | |
| GB776649A (en) | Improvements in or relating to alloys of magnesium | |
| GB619912A (en) | Improvements relating to alloy steels for use at elevated temperatures | |
| GB653311A (en) | Improvements in and relating to nickel chromium steels | |
| GB584873A (en) | Improvements in and relating to gas turbines | |
| GB769822A (en) | Improvements in nickel-base alloys | |
| GB800120A (en) | Improvements in or relating to vanadium alloys | |
| GB692867A (en) | Improvements relating to turbine blades | |
| GB775455A (en) | Improvements in or relating to turbines and nozzle mechanism therefor | |
| GB849365A (en) | Manufacture of turbine and compressor blades | |
| GB754557A (en) | Improvements in or relating to an iron alloy and articles for high temperature uses | |
| GB579318A (en) | Improvements in and relating to apparatus for utilising the exhaust from a gas or oil engine | |
| GB578601A (en) | Improvements relating to cast iron shot | |
| GB647716A (en) | Improvements in or relating to steel articles | |
| GB700246A (en) | Improvements in or relating to alloy steels | |
| GB654354A (en) | Improvements in or relating to heat-resisting alloys containing cobalt |