发明名称 METHOD OF CHILLDOWN OF THE TANK WITH CRYOGENIC FUEL DURING THE TESTING OF ROCKET UNIT
摘要 FIELD: aviation.SUBSTANCE: Method of chilldown of the tank with cryogenic fuel during the testing of rocket unit consists in removal of steam-gas mixture from the tank through the draining system with the installed cross-section area downstream with simultaneous measurement of pressure and temperature of the mixture in the tank. To implement the method the mixture pressure downstream the drainage system is measured, the composition of gas-vapor phase in the tank is determined with the calculation of the gas constant and adiabatic index for the gas-vapor mixture, they are compared with the parameters, earlier determined for real flight conditions, and using the observed-minus-computed difference the drainage system output cross-section area is adjusted.EFFECT: improvement of accuracy of the chilldown process and significant material advantage due to instruction of the operation of time adjustment of the drainage system output cross-section area.
申请公布号 RU2537204(C1) 申请公布日期 2014.12.27
申请号 RU20130150158 申请日期 2013.11.12
申请人 FEDERAL'NOE GOSUDARSTVENNOE UNITARNOE PREDPRIJATIE "NAUCHNO-PROIZVODSTVENNOE OB"EDINENIE "TEKHNOMASH" 发明人 VENGERSKIJ EHDUARD VLADIMIROVICH;USOV GENRIKH LEONIDOVICH;RJABYKH VALERIJ JUR'EVICH;KUCHKIN VLADIMIR NIKOLAEVICH;SHOSTAK ALEKSANDR VIKTOROVICH
分类号 F17C7/00;F02K1/17 主分类号 F17C7/00
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