A vapor cycle refrigeration system (100) for an aircraft comprises a compressor (10), a condenser unit (20) with a condenser radiator (22), a condenser fan (24) and a condenser air duct (26) configured to direct a stream of air generated by the condenser fan (24) through the condenser radiator (22), an expansion device (30), an evaporator unit (40) with an evaporator radiator (42), an evaporator fan (44) and an evaporator air duct (46) configured to direct a stream of air generated by the evaporator fan (44) through the evaporator radiator (42), and a piping system (50) connecting the compressor (10), the condenser radiator (22), the expansion device (30) and the evaporator radiator (42) in a closed circuit for a refrigerant,wherein each of the compressor (10), the condenser radiator (22), the condenser fan (24), the expansion device (30), the evaporator radiator (42), the evaporator fan (44) and the piping system (50) is fully supported directly or indirectly by at least one of the condenser air duct (26) and the evaporator air duct (46), preferably by the condenser air duct (26), in such a manner that the system (100) is self-supporting.
SELF-SUPPORTING VAPOR CYCLE REFRIGERATION SYSTEM FOR AN AIRCRAFT
SELBSTTRAGENDES DAMPFKREISLAUF-KÄLTESYSTEM FÜR EIN FLUGZEUG
SYSTÈME DE RÉFRIGÉRATION À CYCLE DE VAPEUR AUTOPORTANT POUR AÉRONEF
2023-04-05
Patent
Elektronische Ressource
Englisch
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