COOLING SYSTEM AND METHOD OF HEAT REMOVAL FROM THERMAL SOURCES LOCATED INSIDE AIRCRAFT Russian patent published in 2010 - IPC F28D15/02 

FIELD: heating systems.

SUBSTANCE: inventions are intended for heat removal and can be used in aircraft. Cooling device includes tube system which is tightly closed in relation to ambient atmosphere, has thermal coupling in heat reception section with heat source, and in heat transfer section - with heat absorber and which has adiabatic transfer section. Tube system is filled with heat-transfer medium. In heat reception section and/or in heat removal section there provided is heat exchanger which connects heat source and heat absorber to tube system. Heat absorber includes aircraft external wall section. Cold accumulator is provided between heat source and heat absorber. Method of heat removal from heat source to heat absorber consists in the fact that tube system tightly closed in relation to ambient atmosphere is filled with heat transfer medium which, during heat removal from heat source in heat reception section, is changed from liquid phase to gaseous phase and supplied to heat transfer section in which it is again condensed and moves back to heat reception section. Fan is used to control heat transfer between heat source and heat exchanger.

EFFECT: reducing costs for cooling and increasing heat transfer.

15 cl, 7 dwg