An aircraft heat exchanger system (20) according to an exemplary embodiment of this disclosure, among other possible things includes a first heat exchanger assembly (26) that is disposed in an inlet duct assembly (38), and a skin heat exchanger assembly (28) in thermal communication with an outer surface (40) of an aircraft structure (22). The skin heat exchanger (28) is in fluid communication with the first heat exchanger (26) such that a working fluid (32) is communicated therebetween.
AIRCRAFT SKIN HEAT EXCHANGER
FLUGZEUGHAUTWÄRMETAUSCHER
ÉCHANGEUR DE CHALEUR DE LA PEAU D'UN AÉRONEF
2023-08-02
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2018
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