An aircraft pressurization system, includes an auxiliary compressor (42) for further compressing compressed air received from a low pressure compressor section (22) of a gas turbine engine (10) while the compressed air is below a predetermined pressure level; a bleed passage (40) for fluidically connecting the auxiliary compressor (42) to the low pressure compressor section (22); and an environmental control system (38) coupled to an output of the auxiliary compressor (42) for conditioning the compressed air to a predetermined level.


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    Title :

    Low pressure compressor bleed exit for an aircraft pressurization system


    Additional title:

    Entlüftungsausgang eines Niedrigdruckkompressors für ein Flugzeugdruckregelanlage
    Sortie de purge d'un compresseur basse pression pour un système de pressurisation d'un avion


    Contributors:

    Publication date :

    2015-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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