To provide a gas turbine device capable of stably burning by relieving an impact of combustion product gas generated at a combustor for generating detonation.
A gas turbine power system 100 is provided with a compressor 1, a detonation combustor 2, and a turbine 3. The gas turbine power system 100 is provided with a plurality of the detonation combustors 2 respectively arranged so as to surround a rotation shaft of the turbine. The detonation combustor 2 is provided with an inner tube and outer tube. An outlet end of the inner tube is covered with the outer tube. The combustion product gas in the inner tube is exhausted from an exhaust pipe provided on the outer tube. Combustion timings of the detonation combustors 2 are respectively different for each of the detonation combustors.
UMEDA YOSHITO
HANEKI SATOSHI
KURACHI SEIGO
ENDO TAKUMA
MATSUO AKIKO
WATANABE KAZUYA
Takashi Tomizawa
Ikuo Yamanaka