发明名称 Gas turbine regulation system has shut-off device that deactivates gas temperature regulator in response to abnormality sensor so valve is regulated by speed-load regulator
摘要 The system has an inlet control blade (1) regulator for varying the rate of air flow into a compressor (2), a fuel regulating valve (5) for varying the rate of fuel flow into a combustion unit (4), a speed-load regulator that acts on the valve to regulate the fuel flow rate, and hence the gas turbine (7) revolution rate, a combustion gas temperature regulator and a system frequency abnormality sensor. The gas temperature regulator has a shut-off device that operates in response to the operation of the abnormality sensor to deactivate the gas temperature regulator so that the valve is regulated by the speed-load regulator to restore a system frequency.
申请公布号 DE10322703(A1) 申请公布日期 2003.12.04
申请号 DE2003122703 申请日期 2003.05.20
申请人 KABUSHIKI KAISHA TOSHIBA, TOKIO/TOKYO 发明人 HIRAYAMA, KAIICHIROU;KOBAYASHI (VERSTORBEN), TADASHI;KATAURI, TOMOO;OOTSUKI, YASUHIKO;MIZUNO, TAKASHI
分类号 F02C7/042;F02C9/28;F02C9/46;F02C9/54;F04D27/00;F04D29/56;G05B23/02;H02P9/04;(IPC1-7):F02C9/28 主分类号 F02C7/042
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