GB368318A - Improvements in or relating to turbines - Google Patents
Improvements in or relating to turbinesInfo
- Publication number
- GB368318A GB368318A GB33157/30A GB3315730A GB368318A GB 368318 A GB368318 A GB 368318A GB 33157/30 A GB33157/30 A GB 33157/30A GB 3315730 A GB3315730 A GB 3315730A GB 368318 A GB368318 A GB 368318A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbines
- plant
- gas turbine
- housings
- turbine plant
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/36—Open cycles
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
Abstract
368,318. Gas turbine plant. AKTIEBOLAGET MILO, 17, Võstra Tradgardsgatan, Stockholm. Nov. 4, 1930, No. 33157. Convention date, March 24. [Class 110 (iii).] In a gas turbine plant comprising a plurality of radial flow turbines in separate housings, combustion apparatus is arranged in the conducts for the driving medium leading to at least two of the turbine housings. In the Figure, turbines 1, 2 arranged in series drive a generator 6 on the same shaft. Combustion chambers are provided at 9, 13, and extra air may be supplied to the second chamber. Plant lay-outs of the type described in Specification 368,317 are illustrated. Specification 368,319 also is referred to.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE368318X | 1930-03-24 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB368318A true GB368318A (en) | 1932-03-04 |
Family
ID=6318064
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB33157/30A Expired GB368318A (en) | 1930-03-24 | 1930-11-04 | Improvements in or relating to turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB368318A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2415110A (en) * | 1943-08-02 | 1947-02-04 | Pescara Raul Pateras | Power plant |
US2626501A (en) * | 1944-10-07 | 1953-01-27 | Turbolectric Corp | Gas turbine power plant having compressor, turbine, and hollow shaft therebetween |
US2877622A (en) * | 1954-11-18 | 1959-03-17 | Associated British Oil Engines | Heat engines |
-
1930
- 1930-11-04 GB GB33157/30A patent/GB368318A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2415110A (en) * | 1943-08-02 | 1947-02-04 | Pescara Raul Pateras | Power plant |
US2626501A (en) * | 1944-10-07 | 1953-01-27 | Turbolectric Corp | Gas turbine power plant having compressor, turbine, and hollow shaft therebetween |
US2877622A (en) * | 1954-11-18 | 1959-03-17 | Associated British Oil Engines | Heat engines |
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