公开(公告)号：US20060208135A1

公开(公告)日：2006-09-21

申请号：US11084779

申请日：2005-03-18

申请人： Salvatore Liguore ,  Joshua Montgomery

发明人： Salvatore Liguore ,  Joshua Montgomery

IPC分类号： B64C30/00

CPC分类号： B32B37/12 ,  B29C70/088 ,  B29C70/342 ,  B29C70/865 ,  B29D99/0014 ,  B29K2995/0002 ,  B29K2995/0091 ,  B64C1/066 ,  B64C1/40 ,  B64C2001/0072 ,  F16F9/306 ,  Y02T50/43 ,  Y10T156/10

摘要： Systems and methods for reducing noise in aircraft fuselages and other structures are described herein. A noise reduction system configured in accordance with one embodiment of the invention includes an auxetic core, a damping layer, and a constraining layer. In this embodiment, the auxetic core is supported by a structural member, and the damping layer is sandwiched between the auxetic core and the constraining layer. A method for manufacturing a structural assembly in accordance with another embodiment of the invention includes forming a stiffener by positioning a first ply of composite material against a first tool surface, positioning damping material against the first ply, and positioning a second ply of composite material against the damping material to sandwich the damping material between the first and second plies. The method can further include forming a skin by positioning a third ply of composite material against a second tool surface offset from the first tool surface, and attaching the stiffener to the skin by co-curing the first, second and third plies of composite material.

公开(公告)号：US20070102239A1

公开(公告)日：2007-05-10

申请号：US11163957

申请日：2005-11-04

申请人： Salvatore Liguore ,  Joshua Montgomery ,  Mark Younie ,  Robert Rackl

发明人： Salvatore Liguore ,  Joshua Montgomery ,  Mark Younie ,  Robert Rackl

IPC分类号： E04B1/82 ,  B64F1/26

CPC分类号： B64C1/18 ,  B32B3/12 ,  B32B5/26 ,  B32B27/38 ,  B32B2260/021 ,  B32B2260/023 ,  B32B2260/046 ,  B32B2262/0269 ,  B32B2262/101 ,  B32B2262/106 ,  B32B2307/102 ,  B32B2307/54 ,  B32B2307/56 ,  B32B2419/04 ,  B32B2605/003 ,  B32B2605/18

摘要： In accordance with the present invention an aircraft floor panel is provided comprising a honeycomb core element having an upper core surface, a lower core surface, and a core thickness. An upper face sheet assembly is mounted to and seals the upper core surface and includes at least one upper material sheet impregnated with an upper epoxy resin. A lower damping face sheet assembly is mounted to and seals the lower core surface and includes at least one lower material sheet infused with a highly damped lower epoxy resin. The lower damping face sheet assembly dampens vibrational noise.

摘要翻译： 根据本发明，提供一种飞机地板镶板，其包括具有上芯表面，下芯表面和芯厚度的蜂窝芯元件。 上表面片组件安装到上芯片表面上并密封上芯片表面，并且包括至少一个浸有上部环氧树脂的上部材料片材。 下阻尼面板组件安装到下芯体表面并密封下芯表面，并且包括至少一个注入高度阻尼的下环氧树脂的下材料片。 下阻尼面板组件会抑制振动噪声。