GB222472A - Improvements in and relating to steam or gas turbines - Google Patents
Improvements in and relating to steam or gas turbinesInfo
- Publication number
- GB222472A GB222472A GB22187/24A GB2218724A GB222472A GB 222472 A GB222472 A GB 222472A GB 22187/24 A GB22187/24 A GB 22187/24A GB 2218724 A GB2218724 A GB 2218724A GB 222472 A GB222472 A GB 222472A
- Authority
- GB
- United Kingdom
- Prior art keywords
- passages
- width
- blades
- steam
- relating
- 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
-
- 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
- F01D5/142—Shape, i.e. outer, aerodynamic form of the blades of successive rotor or stator blade-rows
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
222,472. Erste Br³nner Maschinen- Fabriks-Ges. Sept. 29, 1923, [Convention date]. Axial-flow type; blades, vanes, and nozzles.- In turbines of the disc type, the outlet ends of the guide passages c and the inlet ends of the rotor blade passages a form substantially continuous passages of uniformly increasing or decreasing cross-sectional area, the gap s between the two sets of passages not exceeding 1 mm. in width. The width f of the guide blades b is approximately 1.5 times the width e of the rotor blades a.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
AT222472X | 1923-09-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB222472A true GB222472A (en) | 1925-12-03 |
Family
ID=3669840
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB22187/24A Expired GB222472A (en) | 1923-09-29 | 1924-09-19 | Improvements in and relating to steam or gas turbines |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB222472A (en) |
NL (1) | NL15774C (en) |
-
0
- NL NL15774D patent/NL15774C/xx active
-
1924
- 1924-09-19 GB GB22187/24A patent/GB222472A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
NL15774C (en) |
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