发明名称 |
Lightweight plane aerofoil section has upper and lower walls - with tabs secured in moulded edging piece at leading edge |
摘要 |
<p>The parent patent describes an aerofoil section for a plane comprising moulded upper and lower walls of reinforced resin secured together at their leading edge by a rounded edging strip which itself forms the leading edge. According to the improvement each wall has a shoulder and an projecting tab at its leading edge, the tabs being glued together and being glued in a longitudinal slot in the edging strip. At the point where the aerofoil section is joined to another part of the plane a smoothing piece is secured in the joint. The method is specifically used for a tail-plane and fin. The smoothing piece reduces turbulence which may damage the plane structure.</p> |
申请公布号 |
FR2239381(A2) |
申请公布日期 |
1975.02.28 |
申请号 |
FR19730028582 |
申请日期 |
1973.08.03 |
申请人 |
STE NALE INDLE AEROSPATIALE,FR |
发明人 |
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分类号 |
B64C3/24;B64C5/00;(IPC1-7):64C5/00;32B5/18;64C1/00;64C3/20 |
主分类号 |
B64C3/24 |
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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