FIELD: machine building.
SUBSTANCE: invention relates to gas turbine engines used as a mechanical drive and for energy generation. Complex plant (1) for energy generation and load actuation, comprising in combination the following elements: multi-shaft gas turbine engine (3) comprising high pressure turbine (316) mechanically connected to air compressor (312), and low pressure turbine (320), flow-connected to high pressure turbine (316), but mechanically separated from it and mechanically connected to power take-off shaft (11), which is connected to shaft line (9), electric generator (5), mechanically connected to shaft line (9) and driven by gas turbine engine (3), rotary load (7) mechanically connected to shaft line (9) and driven by gas turbine engine (3), load control device intended to control at least one operating parameter of rotary load (7) for adaptation of working conditions of rotary load (7) for generation of requirements from process (13). At that, turbine (320) of low pressure of gas turbine engine (3) and electric generator (5) rotate with essentially constant speed, which does not depend on speed of turbine (316) of high pressure. Also disclosed is a method of operating an integrated plant.
EFFECT: invention allows reducing dimensions of the installation, as well as increasing its efficiency.
13 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
EXPANDER-GENERATOR PRESSURE REGULATOR WITH ADDITIONAL ELECTRICAL CONTROL | 2021 |
|
RU2767847C1 |
COMBINED SYSTEM AND METHOD OF HEAT RECOVERY AND COOLING | 2018 |
|
RU2739656C1 |
DEVICE TO ACTUATE LOAD, MULTI-SPOOL GAS TURBINE FLUSHING METHOD AND METHOD OF MULTI-SPOOL GAS TURBINE SLOW-ROTATING | 2012 |
|
RU2606726C2 |
DRIVE GAS-TURBINE PLANT OF GAS COMPRESSOR UNIT WITH UTILISATION TURBINE PLANT FOR INDEPENDENT POWER SUPPLY | 2016 |
|
RU2626038C1 |
DEVICE FOR GENERATION OF ELECTRIC ENERGY IN TWO-SHAFT GAS TURBINE ENGINE | 2008 |
|
RU2472002C2 |
OPERATING METHOD OF POWER PLANT IN STANDBY MODE (VERSIONS), AND POWER PLANT | 2013 |
|
RU2562686C2 |
TWO-STAGE GAS TURBINE DEVICE | 2016 |
|
RU2704385C2 |
MULTI-STAGE GAS TURBINE DEVICE | 2016 |
|
RU2704386C2 |
DRIVE UNIT (EMBODIMENTS) AND DRIVE UNIT CONTROL METHOD | 2014 |
|
RU2703189C2 |
GAS TURBINE ENGINE IN MECHANICAL DRIVE INSTALLATIONS AND ITS OPERATING METHODS | 2013 |
|
RU2674107C2 |
Authors
Dates
2020-04-14—Published
2016-10-17—Filed