发明名称 Transition shim between structure for fastening a wing to a fuselage of an aircraft, and aircraft having such a shim
摘要 A shim adapted for positioning on the upper surface of at least one wing of an aircraft. The shim restores an aerodynamic profile of the wing at the position of a zone of transition between structure fastening the wing to the fuselage of the aircraft and the upper surface of the aircraft. The shim enables a seal to run from the fastening structure to the upper surface of the wing, in eliminating the zones at which the seal may break open. An aircraft provided with such a shim is also disclosed.
申请公布号 US7607614(B2) 申请公布日期 2009.10.27
申请号 US20050114659 申请日期 2005.04.26
申请人 AIRBUS FRANCE 发明人 ROUYRE FRANCOIS
分类号 B64C1/00;B64C7/00;B64D29/06 主分类号 B64C1/00
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