The invention relates to an air-conditioning system for an aircraft cabin (5) comprising: an engine air bleed device (10); an air-conditioning pack (20) comprising a pack air inlet (21) connected to said engine bleed device (10), and a pack air outlet (22) connected to said cabin (5); an auxiliary module (50) for supplying pressurized air comprising an auxiliary turbomachine (51), comprising a compressor (52) supplied with external fresh air and a turbine suitable to be able to be supplied with air coming from the engine bleed device; and a control unit configured to activate either a standard mode in which the pack air inlet is supplied with the pressurized air coming from the engine bleed device (10), or a fresh air mode in which said pack air inlet (21) is supplied with the pressurized air coming from the auxiliary module (50).
MODULE DE FOURNITURE D'UN AIR FRAIS PRESSURISÉ À UN PACK DE CONDITIONNEMENT D'AIR D'UNE CABINE D'UN AÉRONEF, SYSTÈME DE CONDITIONNEMENT D'AIR EQUIPÉ D'UN TEL MODULE, ET PROCÉDÉ CORRESPONDANT
MODULE FOR SUPPLYING PRESSURISED FRESH AIR TO AN AIR-CONDITIONING PACK OF AN AIRCRAFT CABIN, AIR-CONDITIONING SYSTEM EQUIPPED WITH SUCH A MODULE AND CORRESPONDING METHOD
MODUL ZUR ZUFUHR VON UNTER DRUCK STEHENDER FRISCHLUFT FÜR EIN KLIMAAGGREGAT EINER FLUGZEUGKABINE, KLIMASYSTEM MIT EINEM SOLCHEN MODUL UND ENTSPRECHENDES VERFAHREN
2023-09-06
Patent
Electronic Resource
French
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
European Patent Office | 2021
|ALIMENTATION EN AIR D'UN CIRCUIT DE CONDITIONNEMENT D'AIR D'UNE CABINE D'UN AERONEF
European Patent Office | 2022
|European Patent Office | 2021
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