PURPOSE: To reduce an installation area by connecting the output shaft of a gas turbine with the drive shaft of a pump without interposing a bevel gear reduction gear.
CONSTITUTION: Respective rotary shafts of a turbine 27 for driving compressor for driving a compressor 24 and a turbine 30 for outputting are installed separately in a gas turbine 23 and the output shaft 31 which is the rotary shaft of the turbine 30 for outputting is installed concentrically or parallely with the drive shaft 22 of a pump 21, while slanting by a prescribed angle for the compressor drive shaft 32 which is the rotary shaft of the turbine 27 for driving the compressor and is parallel with a installation base plane L. The output shaft 31 is connected to the drive shaft 22 of the pump 21 through a high speed reduction gear 36.
SUZUKI NOBUHIRO
KONISHI MASAHIDE
