GB350712A - Improvements in or relating to turbines with two or more peripheral intakes and with branched distributors - Google Patents
Improvements in or relating to turbines with two or more peripheral intakes and with branched distributorsInfo
- Publication number
- GB350712A GB350712A GB17229/30A GB1722930A GB350712A GB 350712 A GB350712 A GB 350712A GB 17229/30 A GB17229/30 A GB 17229/30A GB 1722930 A GB1722930 A GB 1722930A GB 350712 A GB350712 A GB 350712A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbines
- intakes
- distributors
- branched
- 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
- F01D9/00—Stators
- F01D9/06—Fluid supply conduits to nozzles or the like
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heterocyclic Carbon Compounds Containing A Hetero Ring Having Oxygen Or Sulfur (AREA)
Abstract
350,712. Motor power plant. RATEAU, L. A. J., NOBLEMAIRE, M. A. G. MARGOT-, and RATEAU, A. J. A., 10 bis, Avenue ElisÚe Reclus, Paris. June 4, 1930, No. 17229. Convention date, June 4, 1929. [Class 110 (iii).] Relates to the driving of a turbine, such as T1 or T2 by the exhaust gases of a multi-cylindered internal-combustion engine Cl .. C8, the turbine being used to drive a supercharging blower'S. The distributers d of the turbines are divided by partitions into concentric rings each of which receives gases from receivers E1 .. E4. The receivers are connected to cylinders the exhausts of which are sufficiently spaced to avoid mutual interference.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BE350712X | 1929-06-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB350712A true GB350712A (en) | 1931-06-18 |
Family
ID=3868200
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB17229/30A Expired GB350712A (en) | 1929-06-04 | 1930-06-04 | Improvements in or relating to turbines with two or more peripheral intakes and with branched distributors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB350712A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3064417A (en) * | 1957-07-02 | 1962-11-20 | Whitworth & Co | Exhaust systems for gas producing units |
US3292364A (en) * | 1963-09-06 | 1966-12-20 | Garrett Corp | Gas turbine with pulsating gas flows |
US3383092A (en) * | 1963-09-06 | 1968-05-14 | Garrett Corp | Gas turbine with pulsating gas flows |
US4311009A (en) * | 1975-10-07 | 1982-01-19 | Elsbett L | Internal combustion engine |
-
1930
- 1930-06-04 GB GB17229/30A patent/GB350712A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3064417A (en) * | 1957-07-02 | 1962-11-20 | Whitworth & Co | Exhaust systems for gas producing units |
US3292364A (en) * | 1963-09-06 | 1966-12-20 | Garrett Corp | Gas turbine with pulsating gas flows |
US3383092A (en) * | 1963-09-06 | 1968-05-14 | Garrett Corp | Gas turbine with pulsating gas flows |
US4311009A (en) * | 1975-10-07 | 1982-01-19 | Elsbett L | Internal combustion engine |
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