An environmental control system of an aircraft with a power turbine includes a heat exchanger (12) and a plenum (28) attached to and in fluid communication with the heat exchanger (12). The plenum (28) includes a housing (108) with a first inlet (110) fluidly connected to the power turbine, a second inlet (112) fluidly connected to a source of ram air, and an outlet (114) fluidly connected to the heat exchanger (12).
ECS DUAL ENTRY RAM INLET PLENUM
STAULUFTEINLASSKAMMER MIT DOPPELTEM EINGANG FÜR ECS
PLÉNUM D'ENTRÉE D'AIR DYNAMIQUE D'ECS À DOUBLE ENTRÉE
2023-03-15
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 |