Title:
GAS TURBINE DEVICE
Document Type and Number:
Japanese Patent JP2006083732
Kind Code:
A
Abstract:
To provide a gas turbine device lessening an impact of combustion product gas generated in a detonation combustor and providing stable rotation power.
The detonation combustor 2 has an inner tube 23 and an outer tube 24 covering the inner tube 23, and composes a return channel 26 for combustion product gas discharged from the inner tube 23. Further, in the detonation combustor 2, a conical reflection part 244 is provided at the closed end 243 of the outer tube 24. By the conical reflection part 244, combustion gas discharged from the outlet end 233 of the inner tube 23 complexly repeats reflection, thereby pressure of combustion gas is leveled.
Inventors:
ENDO TAKUMA
TAKI SHIRO
HACHIFUSA TOMOAKI
KURACHI SEIGO
AOKI SHUICHI
HANEKI SATOSHI
UMEDA YOSHITO
TAKI SHIRO
HACHIFUSA TOMOAKI
KURACHI SEIGO
AOKI SHUICHI
HANEKI SATOSHI
UMEDA YOSHITO
Application Number:
JP2004267762A
Publication Date:
March 30, 2006
Filing Date:
September 15, 2004
Export Citation:
Assignee:
UNIV HIROSHIMA
TOHO GAS KK
TOHO GAS KK
International Classes:
F02C5/00; F23R3/42
Attorney, Agent or Firm:
Patent Business Corporation Cosmos Patent Office
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