发明名称 |
Gas turbine plant |
摘要 |
A gas turbine plant, wherein a plurality of first gas turbines positioned coaxially with compressors and a second gas turbine positioned coaxially with a generator are rotated by a coolant heated by heat energy provided by the fission of a coated particle fuel. A flow in a bypass passage is controlled by controlling the opening of bypass valves of (n-1) in quantity which bypass the first gas turbines on up to (n-1) shafts in starting. Accordingly, the rotational speeds of the first gas turbines on up to (n) shafts are increased to a rated rotational speed in order starting at the initial stage on the upstream side of a high temperature gas-cooled reactor toward the lower stage for each shaft.
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申请公布号 |
US2007137203(A1) |
申请公布日期 |
2007.06.21 |
申请号 |
US20040590014 |
申请日期 |
2004.12.22 |
申请人 |
MITSUBISHI HEAVY INDUSTRIES, LTD. |
发明人 |
YANAI NOBORU;TSUKUDA YOSHIAKI;SUGISHITA HIDEAKI;KAMOHARA SATORU |
分类号 |
G21D3/00;G21D5/00;F01D17/00;F02C1/05;F02C1/10;F02C3/10;F02C7/26;F02C9/18;G21C1/07;G21D1/02;G21D5/06 |
主分类号 |
G21D3/00 |
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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