A bleed valve module (144;244) for mounting to a support structure (31) within an aircraft includes a pipe (152;252), a plurality of bleed valves (156a-156c; 256a-256c) connected to the pipe, a plurality of pneumatic actuators (158a-158c; 258a-258c) connected to the plurality of bleed valves, and a vibration isolating element (154;254). The pipe contains a flow of bleed air and includes a plurality of inlets (160a,160b; 260a,260b) and an outlet (160c;260c). The plurality of bleed valves (156a-156c; 256a-256c) controls the flow of bleed air in the pipe. The plurality of pneumatic actuators (158a-158c; 258a-258c) actuate the plurality of bleed valves. The vibration isolating element (154;254) connects the bleed valve module (144;244), to the support structure (31) within the aircraft and isolates the bleed valve module from vibration.


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    Title :

    Bleed valve module


    Additional title:

    Entlüftungsventilmodul
    Module de soupape de purge


    Contributors:

    Publication date :

    2019-08-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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