摘要：

composite laminate, disclosed is a method for forming the composite laminate, and how to use of the laminate. One embodiment of the composite laminate comprises a number of layers or plies (305A~305E) consists of substantially parallel reinforcing fibers embedded in the base material (305M) (315A~315E). Reinforcing fiber includes a range of 3 ~8 , the range of -3 ~-8 , the range of 10 ~40 , of -10 ~-40 range, and the orientation of about 90 , the orientation, tensile axis (T), such as those with respect to a predetermined axis (320). Method for manufacturing a composite laminate, comprising the steps of laminating the resin and fibers having these orientations, then a step of curing the laminate resulting. One example of usage is for exterior on the fuselage or wing of an aircraft.

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