A method of manufacturing an assembly including a first structure which is arranged to be rigidly connected to a housing of a turbojet engine; a second annular structure surrounding the first structure; and a hyperstatic trellis of connecting rods which maintains the first structure relative to the second structure, is provided. The method includes mounting the connecting rods of the hyperstatic trellis between the structures; and pre-stressing at least one of the connecting rods to a pre-determined level, which is carried out before the mounting thereof between the structures.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Method of producing suspension for a structure in a turbojet engine using a hyperstatic trellis with pre-stressed link elements


    Beteiligte:

    Erscheinungsdatum :

    20.11.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / B21D WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL , Bearbeiten oder Verarbeiten von Blechen, Metallrohren, -stangen oder -profilen ohne wesentliches Abtragen des Werkstoffs / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    Method of producing suspension for a structure in a turbojet engine using a hyperstatic trellis with pre-stressed link elements

    FRANCOIS ROBERT BELLABAL / NICOLAS MARC FLORENT | Europäisches Patentamt | 2020

    Freier Zugriff


    Magnetic suspension propeller and turbojet engine using same

    WANG HAIBO | Europäisches Patentamt | 2022

    Freier Zugriff

    TURBOJET ENGINE SUSPENSION USING A DOUBLE REAR SUPPORT

    BELLABAL FRANCOIS ROBERT | Europäisches Patentamt | 2015

    Freier Zugriff

    Turbojet engine suspension using a double rear support

    BELLABAL FRANCOIS ROBERT | Europäisches Patentamt | 2019

    Freier Zugriff