Title:
GAS TURBINE SYSTEM
Document Type and Number:
WIPO Patent Application WO/2022/209562
Kind Code:
A1
Abstract:
A gas turbine system 1 is provided with: an ammonia tank 14; a combustor 13 that is connected to the ammonia tank 14 and that has a combustion chamber 13a; a suction flow channel 41 that is connected to the combustor 13; a compressor 11a that is provided to the suction flow channel 41; a decomposition gas reservoir 17 that is connected to the combustor 13; and an ammonia decomposition catalyst 16 that is provided to a bleed air flow channel 43 connected to the compressor 11a, is provided between the combustor 13 and the compressor 11a in the suction flow channel 41, or is provided in a space connecting the combustion chamber 13a and the suction flow channel 41 in the combustor 13, and that is connected to the ammonia tank 14 and the decomposition gas reservoir 17.
Inventors:
ITO SHINTARO (JP)
UCHIDA MASAHIRO (JP)
UCHIDA MASAHIRO (JP)
Application Number:
PCT/JP2022/009179
Publication Date:
October 06, 2022
Filing Date:
March 03, 2022
Export Citation:
Assignee:
IHI CORP (JP)
International Classes:
F02C9/40; F02C3/22; F02C3/24; F02C7/14; F02C7/22; F02C7/26
Foreign References:
| JP2012255420A | 2012-12-27 | |||
| JPH10110630A | 1998-04-28 | |||
| JP2010270594A | 2010-12-02 | |||
| JP2017180266A | 2017-10-05 | |||
| JP2006077698A | 2006-03-23 | |||
| JP2021057441A | 2021-04-08 | |||
| JP2016191507A | 2016-11-10 |
Attorney, Agent or Firm:
AOMI PATENT (JP)
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