发明名称 COMPOSITE SKIN PANEL OPENING EDGE AND METHOD FOR MANUFACTURE
摘要 The present invention disclosed herein provides a component frame (18) for supporting a component (28) in a vehicle. The component (28) may be a door, a window or another piece of equipment on an aircraft that requires a flush- fitting interface with the aircraft. The component frame (18) comprises an outer skin (20) having a recessed edge (16) disposed generally around the perimeter of the component frame (18). An inner skin (24) is disposed within the aircraft and serves to sandwich a honeycomb core (22) between itself and the outer skin (20).
申请公布号 CA2423665(A1) 申请公布日期 2002.04.11
申请号 CA20012423665 申请日期 2001.09.27
申请人 BELL HELICOPTER TEXTRON INC. 发明人 ADDISON, STEVEN JOEL;HAZEN, TIMOTHY MYRON;HOWARD, JOHN VERDI;FILA, JOSEF ANTONIN
分类号 B64C1/00;(IPC1-7):B64C1/00 主分类号 B64C1/00
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