发明名称 |
Gas turbine engine system |
摘要 |
A gas turbine engine system (1) is provided with a gas turbine engine (2), a purge gas supply line (4) connected to a first connecting part (P1) of a fuel supply line (3) leading to the gas turbine engine (2), a fuel diffusion line (7) connected to a second connecting part (P2) downstream of the first connecting part (P1) of the fuel supply line (3), a blow-off valve (72) provided to the fuel diffusion line (7), and a channel-switching device (50) for switching the fuel supply line (3) between a fuel supply mode and a purge mode. A check valve (73) and a flame arrester (74) are provided downstream of the blow-off valve (72) of the fuel diffusion line (7). |
申请公布号 |
AU2015307907(A1) |
申请公布日期 |
2017.03.16 |
申请号 |
AU20150307907 |
申请日期 |
2015.08.21 |
申请人 |
Kawasaki Jukogyo Kabushiki Kaisha |
发明人 |
Okada, Kunio;Horikawa, Atsushi;Yamashita, Seiji;Kazari, Masahide;Sano, Hikaru |
分类号 |
F02C7/232;F23R3/28;F23R3/36 |
主分类号 |
F02C7/232 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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