GB659714A - Improvements in units comprising a gas turbine driving an electric generator - Google Patents
Improvements in units comprising a gas turbine driving an electric generatorInfo
- Publication number
- GB659714A GB659714A GB27711/49A GB2771149A GB659714A GB 659714 A GB659714 A GB 659714A GB 27711/49 A GB27711/49 A GB 27711/49A GB 2771149 A GB2771149 A GB 2771149A GB 659714 A GB659714 A GB 659714A
- Authority
- GB
- United Kingdom
- Prior art keywords
- generator
- turbine
- producers
- gas turbine
- producer
- 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
- F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
- F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
Abstract
659,714. Gas turbine plant. SVENSKA TURBINFABRIKS AKTIEBOLAGET LJUNGSTROM. Oct. 28, 1949, No. 27711. Convention date, Nov. 6, 1948. [Class 110(iii)] In a unit comprising a gas turbine driving an electric generator 1, one or each of the overhung ends of the generator shaft supports a turbine rotor 18 which receives driving fluid from a producer which comprises a compressor 8, a combustion chamber 9 and a turbine 10 driving the compressor, the producers being supported by the generator. The generator is rigidly supported on the heat exchanger 4 to which the exhaust gases from the turbines pass, and the driving fluid producers are sustained by springs 16. The generator exciter may be mounted at 11 between the generator and a turbine 18, or at the free end 12 of one of the producers, in which case it is driven either by the producer through gearing, or by a turbine 18 by means of a shaft passing through a bore in the producer shaft. The producers may be of different sizes so that the unit may be run at three different outputs.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| SE659714X | 1948-11-06 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB659714A true GB659714A (en) | 1951-10-24 |
Family
ID=20314293
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB27711/49A Expired GB659714A (en) | 1948-11-06 | 1949-10-28 | Improvements in units comprising a gas turbine driving an electric generator |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB659714A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3210553A (en) * | 1961-01-30 | 1965-10-05 | Trw Inc | Turboelectric power system |
| US3241314A (en) * | 1962-08-02 | 1966-03-22 | Bristol Siddeley Engines Ltd | Gas turbine power plant |
| US4590384A (en) * | 1983-03-25 | 1986-05-20 | Ormat Turbines, Ltd. | Method and means for peaking or peak power shaving |
-
1949
- 1949-10-28 GB GB27711/49A patent/GB659714A/en not_active Expired
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3210553A (en) * | 1961-01-30 | 1965-10-05 | Trw Inc | Turboelectric power system |
| US3241314A (en) * | 1962-08-02 | 1966-03-22 | Bristol Siddeley Engines Ltd | Gas turbine power plant |
| US4590384A (en) * | 1983-03-25 | 1986-05-20 | Ormat Turbines, Ltd. | Method and means for peaking or peak power shaving |
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