This aeronautical equipment for an aircraft, comprising a part configured to be positioned at the level of a skin of the aircraft and means for reheating this part comprising a closed-circuit thermodynamic loop in which a phase-change heat transfer fluid circulates, is wherein it includes means for monitoring the fluid pressure in the loop in order to detect and report a malfunction of the equipment.
AERONAUTICAL EQUIPMENT
2020-11-12
Patent
Elektronische Ressource
Englisch
American export trade in aeronautical equipment
Engineering Index Backfile | 1929
SLUB | 1957
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