发明名称 MONOLITHIC, SELF-STIFFENED, AND PIVOTING COMPOSITE PANEL, IN PARTICULAR FOR A MOBILE PART OF AN AIRCRAFT
摘要 <p>The invention relates to a panel pivoting about an axis parallel to a side of the panel, which comprises a first continuous coating (1),a main structural frame of a composite stiffener (2, 3, 4, 5, 6) connected to the coating (1) and including a stiffening mesh (2, 3) with at least one pair of cross-shaped stiffeners each oriented in one of two directions, respectively, not parallel or perpendicular to the rotation axis. The two parts (3a, 3b) of each stiffener (3, 2) extending on either side of the centre of the cross are in structural continuity, and the two stiffeners (2, 3) each have an end located at one point (A, B, C) on the side of the panel parallel to the rotation axis, wherein the end is connected to a rigid member for connection to the rotation axis, the opposite end of at least one stiffener being blocked in rotation on a bearing point on the opposite side of the panel.</p>
申请公布号 EP2242683(A1) 申请公布日期 2010.10.27
申请号 EP20090720526 申请日期 2009.02.19
申请人 SOCATA 发明人 VALLEE, PHILIPPE
分类号 B64C1/06;B64C9/00;B64C9/02;B64C25/16 主分类号 B64C1/06
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