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Design, Fabrication and Testing of an Advanced Composite Access Door for Use in a Lower Wing Panel

机译:用于下翼板的先进复合检修门的设计,制造和测试

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For reasons of comparison, the dimensions and the load specification of a Fokker F-27 Friendship hatch at station 5000 were chosen. The panel is designed as a carbon fiber sandwich construction in which the laminate type and thickness are determined by the strength of the mechanical joint. A full scale tensile test was carried out and a weight comparison was made with the original aluminum hatch.

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