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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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