公开(公告)号：US20090014591A1

公开(公告)日：2009-01-15

申请号：US12165965

申请日：2008-07-01

申请人： Bernard PAULY ,  Bruno Chauveau

发明人： Bernard PAULY ,  Bruno Chauveau

IPC分类号： B64C1/14

CPC分类号： B64C25/16 ,  B64C23/06 ,  B64C2025/003 ,  B64D1/06 ,  Y02T50/162

摘要： The invention relates to an aircraft (10) provided with: a wall (14) having an exterior surface in contact with air flows external to the aircraft, an internal cavity (16) in the aircraft, recessed relative to the exterior surface of the wall, at least one mobile trapdoor (18, 20), which in closed position prolongs the exterior surface in such a way as to shut off the cavity from the exterior, and which in open position projects relative to the exterior surface in such a way as to open the cavity to the exterior, characterized in that it is provided with at least one mobile aerodynamic deflector (30, 32), whose movement is slaved to that of the said at least one trapdoor, the said at least one aerodynamic deflector projecting relative to the exterior surface in a zone thereof situated outside the zone covered by the said at least one trapdoor when the said at least one trapdoor is open.

摘要翻译： 本发明涉及一种飞机（10），其具有：具有与飞机外部的空气相接触的外表面的壁（14），飞行器中的内腔（16）相对于壁的外表面凹陷 ，至少一个移动的收集门（18,20），其处于关闭位置，以使得所述外部表面的外表面延伸，从而将所述空腔与所述外部相隔离，并且处于打开位置，所述外部表面以相对于所述外表面的方式突出， 以将空腔打开到外部，其特征在于，其设置有至少一个可移动的空气动力学偏转器（30,32），其移动被移动到所述至少一个陷门的运动，所述至少一个空气动力学偏转器相对于所述至少一个 到达位于由所述至少一个诱捕门所覆盖的区域外部的区域中的外表面，当所述至少一个诱捕门打开时。