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
分类号 B64C3/24;B64C5/00;(IPC1-7):64C5/00;32B5/18;64C1/00;64C3/20 主分类号 B64C3/24
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