发明名称 METHOD OF DEFINITION OF SUPERSONIC RAMJET FUEL MIX COMBUSTION EFFICIENCY
摘要 FIELD: engines and pumps.SUBSTANCE: proposed method comprises rigid attachment of ramjet onto horizontal measuring platform to be mounted at crosswise elastic supports and connected with force transducer. Force transducer is calibrated with preset mass weight to measure force at force transducer. Thereafter, cold air is fed to combustion chamber inlet to measure force at force transducer. Then, fuel is forced into combustion chamber to ignite formed fuel mix and to measure force at force transducer for fuel combustion efficiency to be defined by relationship protected by this invention.EFFECT: higher accuracy and reliability of determination, simplified procedure.1 dwg
申请公布号 RU2495270(C1) 申请公布日期 2013.10.10
申请号 RU20120120949 申请日期 2012.05.23
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "TSENTRAL'NYJ INSTITUT AVIATSIONNOGO MOTOROSTROENIJA IMENI P.I. BARANOVA" 发明人 ALEKSANDROV VADIM JUR'EVICH;KLIMOVSKIJ KONSTANTIN KONSTANTINOVICH;PROKHOROV ALEKSANDR NIKOLAEVICH
分类号 F02K7/08;G01M15/00 主分类号 F02K7/08
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