Control system for pressurization, ventilation and air...

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 13/06 (2006.01) B64D 41/00 (2006.01)

Patent

CA 2720895

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.

Comprende dos compresores independientes neumáticos alimentados eléctricamente (CAC) (2) que están conectados a un controlador independiente de (CACs) (5), una unidad de potencia auxiliar (APU) (3) dimensionada para alimentar cada (PAC) (1) de forma independiente en las operaciones de la aeronave tanto en tierra como en vuelo, que está conectado a un controlador independiente de (APU) (6) y un controlador central (12) conectado a los controladores (5 y 6) para que los (PACKs) sean alimentados individualmente bien por un (CAC) (2) o por el (APU) (3) y de forma que se alimente un único (PACK) (1) o varios de ellos.

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