SE8006809L - GAS TURBINE ENGINE - Google Patents
GAS TURBINE ENGINEInfo
- Publication number
- SE8006809L SE8006809L SE8006809A SE8006809A SE8006809L SE 8006809 L SE8006809 L SE 8006809L SE 8006809 A SE8006809 A SE 8006809A SE 8006809 A SE8006809 A SE 8006809A SE 8006809 L SE8006809 L SE 8006809L
- Authority
- SE
- Sweden
- Prior art keywords
- gas
- driving part
- generating
- rotor
- rotors
- Prior art date
Links
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 title 1
- 230000005540 biological transmission Effects 0.000 abstract 1
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
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/02—Plural gas-turbine plants having a common power output
-
- 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
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/312—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being parallel to each other
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2250/00—Geometry
- F05D2250/30—Arrangement of components
- F05D2250/31—Arrangement of components according to the direction of their main axis or their axis of rotation
- F05D2250/313—Arrangement of components according to the direction of their main axis or their axis of rotation the axes being perpendicular to each other
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Gear Transmission (AREA)
Abstract
In order to be able to construct gas turbine power plants with a variable output power on the basis of a limited number of basic components in a drive unit having three turbine rotors, the number of rotors (16, 17, 18) in the gas generating part and/or driving part is doubled. The driving part has a turbine rotor (16) which is mounted on the same shaft as the compressor (14) and the two other rotors (17, 18) form a drive unit which is connected to a gear set (10) for an output shaft. It is possible to double the number of rotors both in the gas-generating and in the driving part and one of them can have a common inner transmission shaft (21) between the gearing and gas-generating parts. The arrangement can be such that the driving part has a considerably larger gas capacity than the rotor of the gas generator, at least two gas-generating parts being connected to the same driving part. However, the arrangement can also be such that the rotor of the gas-generating part has a considerably larger gas capacity than the driving part, in which case at least two such parts are connected to the same gas-generating part. In the two last-mentioned cases, it is possible, depending on the space available and on specific requirements, to arrange the double rotor shafts parallel to or at an angle to the larger, common rotor shaft. <IMAGE>
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8006809A SE439337B (en) | 1980-09-29 | 1980-09-29 | GAS TURBINE ENGINE |
DE19813137599 DE3137599A1 (en) | 1980-09-29 | 1981-09-22 | Gas turbine power plant |
FR8117854A FR2491135A1 (en) | 1980-09-29 | 1981-09-22 | GAS TURBINE MECHANISM |
JP15608581A JPS5791327A (en) | 1980-09-29 | 1981-09-29 | Gas turbine apparatus |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE8006809A SE439337B (en) | 1980-09-29 | 1980-09-29 | GAS TURBINE ENGINE |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8006809L true SE8006809L (en) | 1982-03-30 |
SE439337B SE439337B (en) | 1985-06-10 |
Family
ID=20341849
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8006809A SE439337B (en) | 1980-09-29 | 1980-09-29 | GAS TURBINE ENGINE |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS5791327A (en) |
DE (1) | DE3137599A1 (en) |
FR (1) | FR2491135A1 (en) |
SE (1) | SE439337B (en) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3143389A1 (en) * | 1981-11-02 | 1983-08-25 | Roland Fahrzeugplanung und -Vertrieb GmbH, 8000 München | Combined engine for heavy agricultural vehicles |
DE3915003A1 (en) * | 1989-05-08 | 1990-11-15 | Hammer Gmbh Geb | Catalytic and adsorptive purificn. of nitrogen - in single reactor with integral adsorbent regeneration |
FR2674286A1 (en) * | 1991-03-20 | 1992-09-25 | Aiello Francois | ELECTRICITY GENERATOR. |
US5402631A (en) * | 1991-05-10 | 1995-04-04 | Praxair Technology, Inc. | Integration of combustor-turbine units and integral-gear pressure processors |
AU2003213998A1 (en) * | 2003-02-11 | 2004-09-06 | Uwe Borchert | Method for producing gas turbines and gas turbine assembly |
FR2894621B1 (en) * | 2005-12-09 | 2011-10-14 | Hispano Suiza Sa | AUXILIARY MACHINE DRIVE SYSTEM OF A DUAL BODY TURBOMOTEUR |
FR3121708B1 (en) * | 2021-04-12 | 2023-02-24 | Psa Automobiles Sa | ENERGY CONVERTER, TURBOGENERATOR TYPE, COMPRISING A PNEUMATIC COUPLING SYSTEM |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2660033A (en) * | 1949-03-08 | 1953-11-24 | Parsons C A & Co Ltd | Freewheeling clutch between a compressor turbine and an output turbine |
GB701552A (en) * | 1949-03-25 | 1953-12-30 | Centrax Power Units Ltd | Improvements relating to gas turbine power plants |
US2944609A (en) * | 1956-06-01 | 1960-07-12 | United Aircraft Corp | Helicopter power transmission system |
FR1374918A (en) * | 1963-07-17 | 1964-10-09 | Mechanical Tech Inc | Charging device operated by gas generators |
FR1447734A (en) * | 1965-09-23 | 1966-07-29 | English Electric Co Ltd | Turbogroup gas engine |
-
1980
- 1980-09-29 SE SE8006809A patent/SE439337B/en not_active IP Right Cessation
-
1981
- 1981-09-22 DE DE19813137599 patent/DE3137599A1/en not_active Withdrawn
- 1981-09-22 FR FR8117854A patent/FR2491135A1/en not_active Withdrawn
- 1981-09-29 JP JP15608581A patent/JPS5791327A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
DE3137599A1 (en) | 1982-05-19 |
FR2491135A1 (en) | 1982-04-02 |
JPS5791327A (en) | 1982-06-07 |
SE439337B (en) | 1985-06-10 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |
Ref document number: 8006809-1 Effective date: 19940410 Format of ref document f/p: F |