GB347374A - Improvements in and relating to turbines - Google Patents
Improvements in and relating to turbinesInfo
- Publication number
- GB347374A GB347374A GB6209/30A GB620930A GB347374A GB 347374 A GB347374 A GB 347374A GB 6209/30 A GB6209/30 A GB 6209/30A GB 620930 A GB620930 A GB 620930A GB 347374 A GB347374 A GB 347374A
- Authority
- GB
- United Kingdom
- Prior art keywords
- discs
- turbines
- steam
- relating
- wheel
- 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
- F01D5/02—Blade-carrying members, e.g. rotors
- F01D5/06—Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
347,374. Steam turbines. AKT.- GES. BROWN, BOVERI, ET CIE, Baden, Switzerland. Feb. 25, 1930, No. 6209. Convention date, April 29, 1929. [Class 110 (iii).] A reaction turbine rotor is built up of discs p, r, u welded together on their outer periphery. An impulse wheel v may be included, and the dummy piston w, and the last wheel u are preferably forged in one piece with the gudgeons x, y. To secure rapid and uniform heating-up on starting, the spaces between the discs may be connected by holes with the steam-space and with one another.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE347374X | 1929-04-29 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB347374A true GB347374A (en) | 1931-04-30 |
Family
ID=6256150
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6209/30A Expired GB347374A (en) | 1929-04-29 | 1930-02-25 | Improvements in and relating to turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB347374A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2448825A (en) * | 1944-03-20 | 1948-09-07 | Lockheed Aircraft Corp | Turbine rotor |
-
1930
- 1930-02-25 GB GB6209/30A patent/GB347374A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2448825A (en) * | 1944-03-20 | 1948-09-07 | Lockheed Aircraft Corp | Turbine rotor |
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