To provide a gas turbine system in which an impact of a combustion product gas generated in a combustor for generating detonation is eased and thereby stable combustion is possible.
A gas turbine generating system 100 is equipped with a compressor 1, a detonation combustor 2 and a turbine 3. Further, the gas turbine generating system 100 is provided with a plurality of the detonation combustor 2, each of which is arranged so as to surround a rotating shaft of the turbine 3. The detonation combustor 2 is provided with inner and outer tubes, while an outlet end of the inner tube is covered with the outer tube. The combustion product gas within the inner tube is exhausted from an outlet pipe provided at the outer tube. Furthermore, combustion timings of the detonation combustor 2 are different from one other.
JP4993442 | Pulse detonation device for splitting strong pressure waves |
WO/1996/038659 | ROTARY INTERNAL COMBUSTION ENGINE |
JP2004076584 | JET ENGINE |
UMEDA YOSHITO
HANEKI SATOSHI
KURACHI SEIGO
ENDO TAKUMA
TAKI SHIRO
HACHIFUSA TOMOAKI
Takashi Tomizawa
Ikuo Yamanaka
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