发明名称 |
METHOD AND SYSTEM FOR CONTROLLING GAS TURBINE ENGINE |
摘要 |
In a control method of a gas turbine engine, an engine controller 4 outputs a combustor power command FD based on an engine condition from an engine condition detector 3. Then, a combustion controller 6 determines each fuel flow rate based on the combustion power command FD. The combustor controller 6 overrides each fuel flow rate for a certain period, to realize smooth stage-process. <IMAGE>
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申请公布号 |
EP1555407(A1) |
申请公布日期 |
2005.07.20 |
申请号 |
EP20030756645 |
申请日期 |
2003.10.16 |
申请人 |
KAWASAKI JUKOGYO KABUSHIKI KAISHA |
发明人 |
BAINO, MAKOTO;KOUNO, YUKINOBU;SASAE, KEISUKE;KIMURA, HIDEO;KINOSHITA, YASUHIRO;KOBAYASHI, MASAYOSHI;YOSHIMURA, TAKANOBU |
分类号 |
F23R3/34;F02C7/228;F02C7/26;F02C9/26;F02C9/28;F02C9/34;F23R3/00;F23R3/30;(IPC1-7):F02C9/34 |
主分类号 |
F23R3/34 |
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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