发明名称 CONTROL METHOD OF FUEL FLOW AT START OF GAS TURBINE UNIT
摘要 FIELD: engines and pumps. ^ SUBSTANCE: invention can be used in electronic hydro mechanical automatic control systems (ACS) of gas turbine engines (GTE). In addition, gas temperature change speed after compressor turbine and rotation frequency of rotor of turbo-compressor is controlled, if gas temperature increase speed is higher than the first pre-set value and rotation frequency decrease speed of turbo-compressor rotor is below the second pre-set value during pre-set time interval determined by calculation-experimental method and specified during GTU operation, "HP compressor failure" signal is shaped and GTU start is stopped. GTU operation is prevented in abnormal modes of compressor owing to higher ACS operating efficiency, which allows avoiding GTU turbine overheating, and as a result, improves GTU operating reliability. ^ EFFECT: higher GTU operating reliability. ^ 1 dwg
申请公布号 RU2427721(C1) 申请公布日期 2011.08.27
申请号 RU20090147885 申请日期 2009.12.22
申请人 ZAKRYTOE AKTSIONERNOE OBSHCHESTVO NAUCHNO-PROIZVODSTVENNAJA FIRMA (ZAO NPF) "GAZ-SISTEMA-SERVIS" 发明人 BURDIN VALERIJ VLADIMIROVICH;GLADKIKH VIKTOR ALEKSANDROVICH
分类号 F02C9/00 主分类号 F02C9/00
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