发明名称 HORIZONTAL STABILISING SURFACE OF AN AIRCRAFT
摘要 The invention relates to a horizontal stabilising surface (8) of an aircraft, in which the sweep angle (40) of said surface (8) is less than 90 degrees, whereby said angle (40) is that formed by the projection of the point reference line at 25% of the local chord (19) of the horizontal stabilising surface (8) onto a plane perpendicular to the plane of symmetry (21) of the aircraft, in the flight direction of the aircraft, with respect to the plane of symmetry (21) of the aircraft, said angle (40) being measured in the flight direction of the aircraft. In addition, the structural connection between the horizontal stabilising surface (8) and the fuselage (1) of the aircraft is provided by a ring frame (13) of said fuselage (1).
申请公布号 WO2010070182(A2) 申请公布日期 2010.06.24
申请号 WO2009ES70596 申请日期 2009.12.17
申请人 AIRBUS OPERATIONS, S.L.;LLAMAS SANDIN, RAUL CARLOS;LUQUE BUZO, MIGUEL 发明人 LLAMAS SANDIN, RAUL CARLOS;LUQUE BUZO, MIGUEL
分类号 B64C1/26;B64C5/02 主分类号 B64C1/26
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