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
06.09.2023
Patent
Elektronische Ressource
Französisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Europäisches Patentamt | 2021
|ALIMENTATION EN AIR D'UN CIRCUIT DE CONDITIONNEMENT D'AIR D'UNE CABINE D'UN AERONEF
Europäisches Patentamt | 2022
|Europäisches Patentamt | 2023
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