发明名称 |
LEADING EDGE ELEMENT OF AIRCRAFT, METHOD FOR MANUFACTURING ONE, WING AND STABILIZER |
摘要 |
<p>The invention relates to a leading edge element, to a method for manufacturing one, and further to an aircraft wing and stabilizer furnished with the leading edge element. The leading edge element (9) is an elongate piece that com- prises a skin plate (13) and at least onelongitudinal stiffener (16). The shape of the front edge of the skin plate is closed and the tail edge is open. The stiff- eneris fastened between the inner surfaces (13b) of the skin plate. Between the inner surface of the skin plate of the outermost longitudinal stiffener, there is a longitudinal space (19) free of transverse stiffeners.</p> |
申请公布号 |
WO2009112641(A1) |
申请公布日期 |
2009.09.17 |
申请号 |
WO2009FI50197 |
申请日期 |
2009.03.12 |
申请人 |
PATRIA AEROSTRUCTURES OY;MAEKELAE, JUHA |
发明人 |
MAEKELAE, JUHA |
分类号 |
B64C3/00;B64C3/28;B64C5/00 |
主分类号 |
B64C3/00 |
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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