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.
Sandwich structure with shear stiffness between skins and compliance in the thickness direction
Sandwichstruktur mit Schersteifheit zwischen Schichten und Nachgiebigkeit in Dickenrichtung
Structure en sandwich avec la rigidité au cisaillement entre peaux et souplesse dans le sens de l'épaisseur
2016-07-13
Patent
Electronic Resource
English
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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