An aircraft cabin blower system (100) comprising: a transmission (110) for receiving mechanical power from a gas turbine engine; and a cabin blower compressor (102), an output of the transmission (110) being configured to drive the cabin blower compressor (102); wherein the transmission (110) has a variable gear ratio and the cabin blower compressor (102) has a variable geometry, wherein variation of the gear ratio and the geometry provides a variable output of the cabin blower compressor (102).
CABIN BLOWER SYSTEM
KABINENGEBLÄSESYSTEM
SYSTÈME DE VENTILATEUR DE CABINE
2020-05-27
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |