A curved composite aircraft frame comprises a multi-ply composite laminate having a generally Z-shaped cross section. At least certain of the laminate plies include unidirectional reinforcing fibers that are substantially tangent at substantially all points along the curvature of the frame.
Curved composite frames and method of making the same
2015-08-04
Patent
Elektronische Ressource
Englisch
Curved composite frames and method of making the same
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