A heat exchanger assembly (12) for an aircraft includes a first heat exchanger (18) with a first hot air circuit, a second heat exchanger (16) with a second hot air circuit, a third heat exchanger (14) with a third hot air circuit, and a cold circuit (58). The first heat exchanger (18) is in fluid communication with a source of bleed air from the engine. The second heat exchanger (16) is disposed adjacent to and in fluid communication with the first heat exchanger (18). The third heat exchanger (14) is disposed adjacent to and in fluid communication with the second heat exchanger (16). The first, second, and third heat exchangers (18, 16, 14) are fluidly connected in series. The cold air circuit (58) passes through each of the first, second, and third heat exchangers (18, 16, 14). The first, second, and third heat exchangers (18, 16, 14) are in cross-flow communication with the cold air circuit (58).
ENVIRONMENTAL CONTROL SYSTEM TRI-HEAT EXCHANGER
KLIMAREGELUNGSSYSTEM DREIFACH-WÄRMETAUSCHER
ÉCHANGEUR TRI-THERMIQUE DE SYSTÈME DE COMMANDE ENVIRONNEMENTAL
2021-06-16
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F28D Wärmetauscher, soweit in keiner anderen Unterklasse vorgesehen, in denen die Wärmetauschmittel nicht in direkte Berührung miteinander kommen , HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS, IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT / F28F Einzelheiten von Wärmetauschern oder Wärmeübertragungsvorrichtungen für allgemeine Verwendung , DETAILS OF HEAT-EXCHANGE OR HEAT-TRANSFER APPARATUS, OF GENERAL APPLICATION |