发明名称 METHOD OF ROCKET ENGINE CONTROL AND DIAGNOSTICS
摘要 FIELD: engines and pumps.SUBSTANCE: proposed method consists in intermittent measurement of engine and engine compartment controlled parameters, their comparison with preset threshold values and executing control and diagnostics proceeding the results of comparison. Said controlled parameters include temperature and pressure in gas and fluid channels of engine and engine compartment. Note here that, additionally, derivate changes of parameters in time are defined to be compared with their appropriate threshold values. in case derivatives exist in the limits of threshold values, fault is considered tolerable to continuation of test and engine is changed into lower power conditions to feed inert medium into engine compartment.EFFECT: higher validity of diagnostics.1 cl, 1 dwg
申请公布号 RU2476850(C1) 申请公布日期 2013.02.27
申请号 RU20110148474 申请日期 2011.11.30
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "TEKHNOMASH" 发明人 VASIN ANATOLIJ SERGEEVICH;VENGERSKIJ EHDUARD VLADIMIROVICH;USOV GENRIKH LEONIDOVICH;ERMOLOV MIKHAIL IVANOVICH;RJABYKH VALERIJ JUR'EVICH;KUCHKIN VLADIMIR NIKOLAEVICH
分类号 G01M15/14 主分类号 G01M15/14
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