METHOD FOR CONTROLLING THERMAL EFFLUENTS GENERATED BY AN AIRCRAFT AND COOLING DEVICE FOR AN AIRCRAFT IMPLEMENTING SAID METHOD

摘要

The object of the invention is a method for managing the thermal rejection of an aircraft comprising a cell (110) and at least one propulsion unit (112), said at least one propulsion unit (112) comprising a turbomachine (116) fueled via a fuel supply circuit (122) extending from a reservoir (124) disposed at the cell (110), said cell (110) including at least one thermal rejection source (134), characterized in that it consists in dissipating, at least partially at the level of at least one propulsion unit (112), the thermal rejections generated at the level of the cell (110) by using as heat transfer fluid the fuel used to feed the turbomachine (116). ).