A ducted fan gas turbine engine has a propulsive fan, a fan case surrounding the fan, a core engine, and a plurality of support structures which transmit loads from the core engine to the fan case. Each support structure has two support struts which extend from the core engine to a joint radially outwardly of the fan case. The support struts are spaced apart at the core engine but converge to meet at the joint. Each support structure further has two structural elements which extend from the joint to respective fixing positions on the fan case at opposite sides of the joint.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Gas turbines engine support structures


    Beteiligte:
    BAGNALL ADAM M (Autor:in)

    Erscheinungsdatum :

    29.01.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke



    Support structures for offshore wind turbines

    Europäisches Patentamt | 2024

    Freier Zugriff

    Single-Engine Turbines

    British Library Online Contents | 2001


    Special fatigue aspects in support structures of offshore wind turbines

    Schaumann, P. / Lochte-Holtgreven, S. / Steppeler, S. | Tema Archiv | 2011


    Turbocharger turbines in engine cycle simulation

    Schorn,N. / Smiljanovski,V. / Spaeder,U. et al. | Kraftfahrwesen | 2008


    Ceramic composites for rocket engine turbines

    Herbell, Thomas P. / Eckel, Andrew J. | NTRS | 1991