发明名称 |
Window frame for aircraft, is made from resin reinforced with unidirectionally-arranged fiber bundles |
摘要 |
<p>#CMT# #/CMT# The frame (1) includes at least one outer flange (2) attached to the window opening edge of the aircraft fuselage, and at least one inner flange (3) and a vertical flange (4) which support a window piece e.g. glass panel. The frame is made from resin reinforced with fiber webbing semifinished components. #CMT# : #/CMT# An independent claim is also included for a window frame manufacturing method. #CMT#USE : #/CMT# For aircraft. #CMT#ADVANTAGE : #/CMT# Reduces weight and manufacturing cost of window frame. Simplifies window frame manufacture. #CMT#DESCRIPTION OF DRAWINGS : #/CMT# The figure shows the isometric view of the window frame. 1 : Window frame 2 : Outer flange 3 : Inner flange 4 : Vertical flange.</p> |
申请公布号 |
DE102004025380(A1) |
申请公布日期 |
2005.12.22 |
申请号 |
DE20041025380 |
申请日期 |
2004.05.24 |
申请人 |
AIRBUS DEUTSCHLAND GMBH |
发明人 |
BOLD, JENS |
分类号 |
B29C70/48;B64C1/14;(IPC1-7):B64C1/14 |
主分类号 |
B29C70/48 |
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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