Gas turbine

The invention discloses a gas turbine and relates to the technical field of gas turbines. The gas turbine comprises a first transmission shaft (1), a second transmission shaft (2), a flexible coupler (3), a gas compressor stator (4) and an exhaust volute (6), wherein one end of the first transmissio...

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Bibliographic Details
Main Authors HAN YONGJUN, WANG CHEN, REN LIXIN, HU YUNBIAO
Format Patent
LanguageEnglish
Published 25.11.2015
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:The invention discloses a gas turbine and relates to the technical field of gas turbines. The gas turbine comprises a first transmission shaft (1), a second transmission shaft (2), a flexible coupler (3), a gas compressor stator (4) and an exhaust volute (6), wherein one end of the first transmission shaft (1) is connected with one end of the flexible coupler (3), the other end of the first transmission shaft (1) is used for being connected with a load, and the middle of the first transmission shaft (1) is connected with the gas compressor stator (4); one end of the second transmission shaft (2) is connected with the other end of the flexible coupler (3), the other end of the second transmission shaft (2) is used for being connected with a load, and the middle of the second transmission shaft (2) is connected with the exhaust volute (6). The gas turbine has the beneficial effect that due to the fact that a power turbine shaft of the gas turbine is provided with two output ends, the requirement of a power turbine of the gas turbine for outputting torque at the gas compressor stator end and the exhaust volute at the same time is met.
Bibliography:Application Number: CN20151595094