发明名称 METHOD OF THERMAL CONTROL OVER UNIT MOUNTED ON SPACESHIP AND DEVICE TO THIS END
摘要 FIELD: transport.SUBSTANCE: invention relates to space engineering, particularly, to thermal control systems. Thermal control is carried out by forcing fluid heat carrier (water) by variable-capacity pump via thermal control line to radiator. Fan is used to force dry air cooled to preset temperature to be mixed with vapor generated in the unit. Liquid heat carrier (water) is added to produce vapor-fluid mix at flow rate required to ensure preset temperature and produce condensate from vapor. Water is forced at pressure exceeding that of produced mix in the mixer. Mix of air with condensate is fed into separator wherefrom fluid is fed into bellow for further pumping into radiator. Separated gas is fed to thermally controlled unit.EFFECT: higher reliability and safety, longer life.3 cl, 1 dwg
申请公布号 RU2467931(C1) 申请公布日期 2012.11.27
申请号 RU20110114474 申请日期 2011.04.13
申请人 OTKRYTOE AKTSIONERNOE OBSHCHESTVO "RAKETNO-KOSMICHESKAJA KORPORATSIJA "EHNERGIJA" IMENI S.P. KOROLEVA" 发明人 GLUKHIKH IGOR' NIKOLAEVICH;CHELJAEV VLADIMIR FILIPPOVICH
分类号 B64G1/50;F28C3/06 主分类号 B64G1/50
代理机构 代理人
主权项
地址