09-06-2023 дата публикации
Номер: CN116241372A
Автор:
WANG KE,
GUO QIANG,
CHEN FENG,
SUN BO,
YANG WENCHUAN,
TANG JIAN,
LI YINGKE,
CAI JIYU,
LAN HONGQIANG,
YU LANLAN,
TANG XIAOYONG,
ZHENG CHUNLAI,
LIU HAIBO,
PU LIMING,
KONG LI,
LIU JIAHONG,
ZHANG JI
Принадлежит:
The invention relates to the technical field of gas turbines, in particular to an integrated system and method suitable for a gas turbine to drive a compressor. According to the technical scheme, the integrated system suitable for the gas turbine to drive the compressor comprises a starting motor, the output end of the starting motor is connected with a compressor unit, one end of the compressor unit is connected with a gearbox, and the other end of the gearbox is connected with the gas turbine. The gas turbine is respectively connected with a gas inlet system for introducing air, a gas module for introducing natural gas, an exhaust system for exhausting tail gas and a chimney; the system further comprises a monitoring control system, and the monitoring control system is electrically connected with the starting motor, the compressor unit, the gearbox, the gas turbine, the gas inlet system and the gas module. The invention provides an integrated system and method suitable for a gas turbine ...
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