An axial compressor includes a housing and a plurality of stages arranged within the housing and along an airflow direction, each stage of the plurality of stages including a first blade assembly and a second blade assembly, wherein the first blade assembly is a rotor, each rotor being drivable independently from the rotors in the other first blade assemblies.

    La présente invention concerne un compresseur axial comprenant un logement et une pluralité d'étages disposés à l'intérieur du logement et le long d'une direction d'écoulement d'air, chaque étage de la pluralité d'étages comprenant un premier ensemble pale et un second ensemble pale, le premier ensemble pale étant un rotor, chaque rotor étant entraînable indépendamment des rotors dans les autres premiers ensembles pales.


    Access

    Download


    Export, share and cite



    Title :

    AXIAL COMPRESSOR CONFIGURATION


    Additional title:

    CONFIGURATION DE COMPRESSEUR AXIAL


    Contributors:

    Publication date :

    2016-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B61B RAILWAY SYSTEMS , Eisenbahnanlagen



    Supersonic axial-flow compressor

    Kantrowitz, A. | Engineering Index Backfile | 1950


    Supersonic Axial-Flow Compressor

    A. Kantrowitz | NTIS | 1946


    Axial Flow Compressor Aerodynamics

    Oates, Gordon C. | AIAA | 1985


    Compressor configuration structure

    SHUHEI KATO | European Patent Office | 2016

    Free access

    Axial Compressor Performance During Surge

    Day, I.J. | Online Contents | 1994