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US08524025B2 One-piece inner shell for full barrel composite fuselage 有权
全套复合机身的单件内壳

One-piece inner shell for full barrel composite fuselage
Abstract:
A mandrel for manufacturing a unitary seamless section of an aircraft fuselage comprises a thin lay-up mandrel element disposed onto the outer shell surface of an inner mandrel shell, forming a mandrel with a substantially continuous lay-up surface. A unitary pre-cured section of an aircraft fuselage is formed by laying up a plurality of resin impregnated skin fibers onto the mandrel's lay-up surface while the mandrel rotates.
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