A composite laminated plate comprising a first plurality of plies of reinforcing fibers for lengthwise strength with respect to a dominant load direction, and a second plurality of reinforcing fibers oriented at angles ±β with respect to the dominant load direction, where β is between 15 and 35 degrees.
COMPOSITE LAMINATED PLATE HAVING REDUCED CROSSPLY ANGLE
14.01.2016
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / E04C STRUCTURAL ELEMENTS , Bauelemente |
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