An aeroengine 100 comprising a cowling 101 with at least two zones 1, 2 enclosed by the cowling 101, wherein a first zone 1 and at least one second zone 2 are separated by a wall 3, the cowling 101 circumferentially enclosing a core engine 104, surrounded by a bypass duct comprising a radially outer fairing 118 and a radially inner fairing 111, the at least one second zone 2 to receive fluid leakages from at least one supply line for fluids 5, 6, 7, entering the at least one second zone 2 through at least one fluid passage in a section of the radially outer fairing of bypass duct 118, the at least one second zone 2 comprises at least one duct 4 connecting the at least one second zone 2 to the environment (E).


    Access

    Download


    Export, share and cite



    Title :

    Aeroengine and process of operating an aeroengine


    Contributors:

    Publication date :

    2025-05-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B64C AEROPLANES , Flugzeuge



    Aeroengine mounting device

    YE BIN / LUO JINLIANG / PENG ZHIJUN et al. | European Patent Office | 2016

    Free access

    Aeroengine installation vehicle

    ZHANG HAIFENG / HAO HAO / ZHANG DEMING et al. | European Patent Office | 2015

    Free access

    Introduction to Aeroengine Controls

    Wang, Jiqiang / Zhang, Weicun / Hu, Zhongzhi | Springer Verlag | 2021


    Aeroengine neural network control

    Tao, T. / Zhang, J. | British Library Online Contents | 1997


    On-Line Aeroengine Testing

    Sharma, G. S. / Institution of Engineers / Indian Institute of Technology | British Library Conference Proceedings | 1995