A system includes an inlet line (102) configured to receive a medium flowing from a low-pressure location of an engine to a chamber (104), a plurality of heat exchangers (110,120) configured to receive the medium from the inlet line (102), and a valve (106) located upstream from the plurality of heat exchangers (110,120). The valve (106) is configured to divide in parallel the medium across at least a first heat exchanger (110) and a second heat exchanger (120) of the plurality of heat exchangers. A recirculation air system (400) is configured to supply a recirculation air from the chamber (104) to the inlet line (102) upstream of the heat exchangers (110,120).
RECIRCULATION SYSTEM FOR PARALLEL RAM HEAT EXCHANGERS
RÜCKFÜHRUNGSSYSTEM FÜR PARALLELE RAM-WÄRMETAUSCHER
SYSTÈME DE RECIRCULATION POUR ÉCHANGEURS DE CHALEUR DE RAM PARALLÈLES
2021-01-20
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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