发明名称 METHOD AND SYSTEM FOR AIRCRAFT ENGINE TANK OIL LEVEL CONTROL
摘要 FIELD: engines and pumps.SUBSTANCE: invention relates to aircraft engines. This process comprises the steps that follow. First, multiple measurements of tank fuel level are performed during at least one flight of aircraft for preset engine working phases. Note here that every measurement is related with oil temperature and engine rpm. Selected are measurements that display oil level variation and are related with oil temperatures that approximate to reference temperature and with engine rpm approximating to reference rpm. Combined are (F40) measurements selected by phases of operation during at least one flight of aircraft and to compare (F60) combined measurements with reference data for identification (F70) of engine oil abnormal consumption.EFFECT: higher validity of estimation.13 cl, 4 dwg
申请公布号 RU2557838(C2) 申请公布日期 2015.07.27
申请号 RU20120148901 申请日期 2011.04.14
申请人 SNEKMA 发明人 DEMEZON FRANSUA;FLANDRUA KSAV'E;MASS ZHAN-REMI;MASSO ZHILL';RIKORDO ZHJUL'EN;MAD UADIR
分类号 F02C9/00 主分类号 F02C9/00
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