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COMPOSITE LAMINATED PLATE HAVING REDUCED CROSSPLY ANGLE
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
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
KISMARTON MAX U (author)
2016-01-14
Patent
Electronic Resource
English
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
On inter-relationships of elastic moduli and strains in crossply laminated composites
British Library Online Contents | 1996
|British Library Online Contents | 2003
|Thermal stresses in crossply composites of glass fibre reinforced polyesters
British Library Online Contents | 1998
|Compressive strength of unidirectional and crossply carbon fibre/PEEK composites
British Library Online Contents | 1995
|Modelling of fatigue microcracking kinetics in crossply composites and experimental validation
British Library Online Contents | 1999
|