发明名称 METHOD TO REGULATE MODE OF OPERATION OF LIQUID ROCKET PROPULSION SYSTEM
摘要 FIELD: power engineering.SUBSTANCE: method to regulate the mode of operation of a liquid rocket propulsion system consists in variation of a throughout section of an organ that regulates flow of supercharging gas depending on cavitation margin of pressure of turbopump set pumps, measurement of engine parameters and determination of their time derivatives. Variation of throughput section of the organ that regulates supercharging gas flow is set according to the value of derivative of pressure and temperature variation at the inlet to the engine.EFFECT: increased accuracy of regulation, reduced non-efficient power inputs due to reduced value of pressure in rocket tanks.1 dwg
申请公布号 RU2499906(C1) 申请公布日期 2013.11.27
申请号 RU20120121447 申请日期 2012.05.25
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 F02K9/56 主分类号 F02K9/56
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