Integrally damped composite aircraft floor panels
作者： Salvatore L. Liguore , Robert G. Rackl , Mark L. Younie , Joshua M. Montgomery
DOI:
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摘要: In accordance with the present invention an aircraft floor panel (14) is provided comprising a honeycomb core element (16) having upper surface (20), lower (22), and thickness (18). An face sheet assembly (36) mounted to seals includes at least one material (38) impregnated epoxy resin (40). A damping (24) (26) infused highly damped (28). The dampens vibrational noise.
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