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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    Title :

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


    Additional title:

    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


    Contributors:

    Publication date :

    2020-01-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    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 / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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