METHOD OF THERMAL CONTROL OVER UNIT MOUNTED ON SPACESHIP AND DEVICE TO THIS END Russian patent published in 2012 - IPC B64G1/50 F28C3/06 

Abstract RU 2467931 C1

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

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RU 2 467 931 C1

Authors

Glukhikh Igor' Nikolaevich

Cheljaev Vladimir Filippovich

Dates

2012-11-27Published

2011-04-13Filed