发明名称 |
LEADING EDGE STRUCTURE |
摘要 |
The invention provides a leading edge structure for providing an aerodynamic surface of an aircraft, the leading edge structure comprising a skin structure, the skin structure providing an outer aerodynamic surface and an inner surface, both surfaces extending in a chordwise and spanwise direction of the structure, and a plurality of structural members, each structural member being connected to the inner surface of the skin structure and extending in the chordwise direction along the inner surface, wherein the structural members are integrally formed with the inner surface of the skin structure. The invention also provides an aircraft wing, aircraft tailplane, wing box structure, wing or wing structure and an aircraft including the leading edge structure. |
申请公布号 |
EP2785586(B1) |
申请公布日期 |
2016.09.14 |
申请号 |
EP20120795599 |
申请日期 |
2012.11.22 |
申请人 |
AIRBUS OPERATIONS LIMITED;AIRBUS OPERATIONS GMBH |
发明人 |
WILLIAMS, LLIFON;SALISBURY, ROSS;RAFLA, MARCUS;THEOBALD, HUGH;PAYNE, CHRISTOPHER;MCCORMICK, ROBERT;HANSEN, HEINZ;EVANS, TIMOTHY |
分类号 |
B64C3/00;B64C3/14;B64C3/18;B64C3/24;B64C3/28 |
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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