A sandwich structure (10) includes a first skin (18), a second skin (20), a first hinge member (32), and a second hinge member (42). The first hinge member (32) may be movably coupled to the first skin (18) and a first skin joint (40). The second hinge member (42) may be movably coupled to the second skin (20) and second skin joint (50). The first hinge member (32) and the second member (42) may be movably coupled to one another and a member joint (52) located between the first and second skin joint.


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    Titel :

    AIRCRAFT ENGINE EXHAUST NOZZLE COMPRISING SANDWICH STRUCTURE WITH SHEAR STIFFNESS BETWEEN SKINS AND COMPLIANCE IN THE THICKNESS DIRECTION


    Weitere Titelangaben:

    LUFTFAHRZEUGTRIEBWERKSAUSSTROMDÜSE SANDWICHSTRUKTUR MIT SCHERSTEIFHEIT ZWISCHEN SCHICHTEN UND KONFORMITÄT IN DER DICKENRICHTUNG
    TUYÈRE D'ÉCHAPPEMENT DU MOTEUR D'AÉRONEF COMPRENANT UNE STRUCTURE EN SANDWICH AVEC RIGIDITÉ AU CISAILLEMENT ENTRE DES PEAUX ET SOUPLESSE DANS LE SENS DE L'ÉPAISSEUR


    Beteiligte:
    GRIP ROBERT E (Autor:in) / BROWN JOHN J (Autor:in)

    Erscheinungsdatum :

    29.01.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / 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



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