The invention relates to an air conditioning system for a cabin (10) of an aircraft (80) comprising: a bleed air source (12); a ram-air circulation channel (13); a network of pipes and control valves; an air cycle turbine engine comprising at least one compressor (3) and a power turbine (4) which are mechanically connected to one another; and at least one primary cooling exchanger (PHX) which is accommodated in said channel (13), characterized in that said pipe network comprises a thermal power pipe (53) which is suitable for being able to fluidically connect, upon control of at least one control valve (25, 21), said air outlet (4b) of said power turbine (4) and said ram-air circulation channel (13) upstream of said primary exchanger (PHX) so that said bleed air expanded by said power turbine (4) can form a thermal energy source for said ram air being supplied to said primary circuit of said primary exchanger (PHX).
SYSTÈME DE CONDITIONNEMENT D'AIR D'UNE CABINE D'UN VÉHICULE DE TRANSPORT AÉRIEN OU FERROVIAIRE UTILISANT UNE SOURCE D'AIR PNEUMATIQUE ET THERMIQUE DISTINCTE DE LA SOURCE D'AIR DE CONDITIONNEMENT
AIR-CONDITIONING SYSTEM FOR A CABIN OF AN AIR OR RAIL TRANSPORT VEHICLE USING A PNEUMATIC AND THERMAL AIR SOURCE SEPARATE FROM THE AIR-CONDITIONING SOURCE
KLIMAANLAGE FÜR EINE KABINE EINES LUFT- ODER SCHIENENVERKEHRSFAHRZEUGS MIT EINER VON DER KLIMATISIERUNGSQUELLE GETRENNTEN PNEUMATISCHEN UND THERMISCHEN LUFTQUELLE
2022-09-28
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2023
|European Patent Office | 2020
|SYSTÈME DE CONDITIONNEMENT D'AIR À RÉCUPÉRATION D'AIR CABINE
European Patent Office | 2023
|