GB355028A - Rotor blade for explosion turbines - Google Patents
Rotor blade for explosion turbinesInfo
- Publication number
- GB355028A GB355028A GB24607/30A GB2460730A GB355028A GB 355028 A GB355028 A GB 355028A GB 24607/30 A GB24607/30 A GB 24607/30A GB 2460730 A GB2460730 A GB 2460730A GB 355028 A GB355028 A GB 355028A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor blade
- parts
- explosion turbines
- turbines
- explosion
- 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
- F01D5/141—Shape, i.e. outer, aerodynamic form
Landscapes
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
A blade for a combustion turbine is formed of an alloy containing 10 parts iron, 65 parts nickel, 15 parts chromium, and 7 parts molybdenum.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE355028X | 1929-08-22 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB355028A true GB355028A (en) | 1931-08-20 |
Family
ID=6289852
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24607/30A Expired GB355028A (en) | 1929-08-22 | 1930-08-16 | Rotor blade for explosion turbines |
Country Status (4)
Country | Link |
---|---|
US (1) | US1800730A (en) |
BE (1) | BE372479A (en) |
FR (1) | FR699920A (en) |
GB (1) | GB355028A (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447896A (en) * | 1946-02-01 | 1948-08-24 | Armco Steel Corp | High-temperature turbine |
US2686654A (en) * | 1948-10-19 | 1954-08-17 | Thompson Prod Inc | Coated member and method of making the same |
US3041040A (en) * | 1955-12-23 | 1962-06-26 | Gen Electric | Metal clad blade |
US20090324419A1 (en) * | 2006-07-25 | 2009-12-31 | Luciano Cozza | Highly corrosion-resistant movable blade assembly for a steam turbine, in particular a geothermal impulse turbine |
-
0
- BE BE372479D patent/BE372479A/xx unknown
-
1930
- 1930-03-11 US US434871A patent/US1800730A/en not_active Expired - Lifetime
- 1930-08-01 FR FR699920D patent/FR699920A/en not_active Expired
- 1930-08-16 GB GB24607/30A patent/GB355028A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
US1800730A (en) | 1931-04-14 |
FR699920A (en) | 1931-02-21 |
BE372479A (en) | 1930-08-05 |
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