GB1477061A - Gas turbine - Google Patents
Gas turbineInfo
- Publication number
- GB1477061A GB1477061A GB1152275A GB1152275A GB1477061A GB 1477061 A GB1477061 A GB 1477061A GB 1152275 A GB1152275 A GB 1152275A GB 1152275 A GB1152275 A GB 1152275A GB 1477061 A GB1477061 A GB 1477061A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shaft
- rotor
- turbine
- gas turbine
- march
- 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
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Applications Or Details Of Rotary Compressors (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
1477061 Gas turbines TURBINE INDUSTRIE 19 March 1975 [20 March 1974] 11522/75 Headings F1G and FIT A gas turbine plant comprises a first turbine rotor 17 on a shaft 4, and a second turbine rotor 20 on a shaft 22, the shafts being supported on respective oil bearings 5 and 23, 24 arranged so that there is an oil bearing on one side only of each rotor. One or more combustion chambers 11 are arranged eccentrically of the shaft axes. As shown, the shaft 4 also causes a low-pressure compressor rotor 3 and a supersonic compressor rotor 8.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7409497A FR2264972B1 (en) | 1974-03-20 | 1974-03-20 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1477061A true GB1477061A (en) | 1977-06-22 |
Family
ID=9136605
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1152275A Expired GB1477061A (en) | 1974-03-20 | 1975-03-19 | Gas turbine |
Country Status (9)
Country | Link |
---|---|
JP (1) | JPS50128012A (en) |
BE (1) | BE826108A (en) |
CA (1) | CA1009046A (en) |
DE (1) | DE2511821A1 (en) |
FR (1) | FR2264972B1 (en) |
GB (1) | GB1477061A (en) |
IT (1) | IT1034362B (en) |
NO (1) | NO750921L (en) |
SE (1) | SE7502988L (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112696269A (en) * | 2020-11-18 | 2021-04-23 | 靳普 | Multi-rotor micro gas turbine and starting method thereof |
EP3812563A1 (en) * | 2019-10-23 | 2021-04-28 | Rolls-Royce plc | A turboshaft gas turbine engine |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE423741B (en) * | 1980-09-29 | 1982-05-24 | Motor Turbine & Transmissions | GAS TURBINE MACHINERY, SPECIAL FOR VEHICLE OPERATION |
EP0227638B1 (en) * | 1984-01-07 | 1990-11-07 | ROLLS-ROYCE plc | Improvements in or relating to gas turbine power plant |
US5832715A (en) * | 1990-02-28 | 1998-11-10 | Dev; Sudarshan Paul | Small gas turbine engine having enhanced fuel economy |
US5253472A (en) * | 1990-02-28 | 1993-10-19 | Dev Sudarshan P | Small gas turbine having enhanced fuel economy |
-
1974
- 1974-03-20 FR FR7409497A patent/FR2264972B1/fr not_active Expired
-
1975
- 1975-02-28 BE BE1006489A patent/BE826108A/en not_active IP Right Cessation
- 1975-03-17 SE SE7502988A patent/SE7502988L/xx unknown
- 1975-03-18 DE DE19752511821 patent/DE2511821A1/en active Pending
- 1975-03-18 IT IT21361/75A patent/IT1034362B/en active
- 1975-03-18 NO NO750921A patent/NO750921L/no unknown
- 1975-03-19 GB GB1152275A patent/GB1477061A/en not_active Expired
- 1975-03-19 CA CA222,589A patent/CA1009046A/en not_active Expired
- 1975-03-20 JP JP50033077A patent/JPS50128012A/ja active Pending
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP3812563A1 (en) * | 2019-10-23 | 2021-04-28 | Rolls-Royce plc | A turboshaft gas turbine engine |
US11486302B2 (en) | 2019-10-23 | 2022-11-01 | Rolls-Royce Plc | Turboshaft gas turbine engine and expansion ratio relationship |
CN112696269A (en) * | 2020-11-18 | 2021-04-23 | 靳普 | Multi-rotor micro gas turbine and starting method thereof |
Also Published As
Publication number | Publication date |
---|---|
DE2511821A1 (en) | 1975-09-25 |
IT1034362B (en) | 1979-09-10 |
NO750921L (en) | 1975-09-23 |
JPS50128012A (en) | 1975-10-08 |
SE7502988L (en) | 1975-09-22 |
FR2264972B1 (en) | 1977-06-17 |
BE826108A (en) | 1975-08-28 |
CA1009046A (en) | 1977-04-26 |
FR2264972A1 (en) | 1975-10-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PCNP | Patent ceased through non-payment of renewal fee |