It consists of two electrically fed pneumatic independent compressors (CAC) (2) which are connected to an independent controller of (CACs) (5), an auxiliary power unit (APU) (3) sized for independently feeding each (PACK) (1) in the operations of the aircraft both on the ground and in flight, which is connected to an independent controller of (APU) (6) and a central controller (12) connected to the controllers (5 and 6) so that the (PACKs) are individually fed either by a (CAC) (2) or by the (APU) (3) and in such a way that a single (PACK) (1) is fed or several of them.
CONTROL SYSTEM FOR PRESSURIZATION, VENTILATION AND AIR CONDITIONING OF AN AIRCRAFT
SYSTEME POUR COMMANDER LA PRESSURISATION, LA VENTILATION ET LE CONDITIONNEMENT DE L'AIR D'UN AERONEF
2016-01-19
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Air conditioning and pressurization for modern commercial aircraft
Engineering Index Backfile | 1960
|Pressurization and air-conditioning
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|AIRCRAFT CABIN PRESSURIZATION CONTROL CRITERIA
SAE Technical Papers | 1993
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TIBKAT | 2000
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Engineering Index Backfile | 1946
|