GB381851A - Improvements in and relating to turbine blades - Google Patents
Improvements in and relating to turbine bladesInfo
- Publication number
- GB381851A GB381851A GB8693/32A GB869332A GB381851A GB 381851 A GB381851 A GB 381851A GB 8693/32 A GB8693/32 A GB 8693/32A GB 869332 A GB869332 A GB 869332A GB 381851 A GB381851 A GB 381851A
- Authority
- GB
- United Kingdom
- Prior art keywords
- per cent
- relating
- turbine blades
- crosion
- vanadium
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
An crosion-resisting blade for gas turbines is made of an iron alloy containing 15-20 per cent of tungsten, 1-3 per cent of vanadium, and 2-4 per cent of aluminium, with or without up to 20 per cent of chromium, and up to 10 per cent of molybdenum.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE381851X | 1931-04-18 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB381851A true GB381851A (en) | 1932-10-13 |
Family
ID=6355524
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB8693/32A Expired GB381851A (en) | 1931-04-18 | 1932-03-23 | Improvements in and relating to turbine blades |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB381851A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2737366A (en) * | 1950-05-02 | 1956-03-06 | Simmering Graz Pauker Ag | Gas turbine |
US2883152A (en) * | 1953-01-19 | 1959-04-21 | Gen Motors Corp | Evaporative cooled turbine |
EP0508387A1 (en) * | 1991-04-09 | 1992-10-14 | Mitsubishi Jukogyo Kabushiki Kaisha | Method for preventing adhesion of scale and nozzle of a geothermal steam turbine |
-
1932
- 1932-03-23 GB GB8693/32A patent/GB381851A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2737366A (en) * | 1950-05-02 | 1956-03-06 | Simmering Graz Pauker Ag | Gas turbine |
US2883152A (en) * | 1953-01-19 | 1959-04-21 | Gen Motors Corp | Evaporative cooled turbine |
EP0508387A1 (en) * | 1991-04-09 | 1992-10-14 | Mitsubishi Jukogyo Kabushiki Kaisha | Method for preventing adhesion of scale and nozzle of a geothermal steam turbine |
US5399067A (en) * | 1991-04-09 | 1995-03-21 | Mitsubishi Jukogyo Kabushiki Kaisha | Nozzle for use in a geothermal steam turbine and method for preventing adhesion of scale thereto |
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