发明名称 CONTROL METHOD OF GAS TURBINE PLANT
摘要 FIELD: engines and pumps. ^ SUBSTANCE: in addition, in all GTP operating modes from idle mode to maximum mode the air pressure is measured after GTP compressor, relative change and relative change speed of air pressure after compressor is calculated, relative pressure change is compared to the first pre-set value determined for each GTP type experimentally, and relative speed is compared to the second pre-set value determined for each GTP type experimentally; if relative pressure change is more than the first pre-set value, and relative speed is more than the second pre-set value, air bleed valves are opened from behind the intermediate stages of GTP compressor and due to GTP compressor and ignition unit is actuated for the pre-set time; if after that, relative pressure change becomes less than the first pre-set value, and relative speed becomes less than the second pre-set value, GTP is operated in compliance with standard control programs; if relative pressure change remains more than the first pre-set value and relative speed remain more than the second pre-set value during the pre-set time determined by calculation experimental method, emergency shutdown of GTP is performed. ^ EFFECT: higher GTP operating reliability owing to performing the actions allowing to take GTP compressor from surging without fuel cut-off. ^ 1 dwg
申请公布号 RU2422683(C1) 申请公布日期 2011.06.27
申请号 RU20090148009 申请日期 2009.12.23
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 F04D27/02 主分类号 F04D27/02
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