发明名称 Aileron system for aircraft and method of operating the same.
摘要 <p>Two aileron assemblies at opposite ends of a wing. Each aileron assembly has an aileron airfoil member having a first stowed position for high speed flight, where aerodynamic contours of the airfoil member match those of the wing. Each aileron airfoil member has a second extended position forming a slot with the trailing edge of the wing. Each airfoil member is slide mounted to a track member which is in turn pivotally mounted to wing structure.</p>
申请公布号 EP0075966(A2) 申请公布日期 1983.04.06
申请号 EP19820200110 申请日期 1982.01.28
申请人 THE BOEING COMPANY 发明人 RUDOLPH, PETER K.C.
分类号 B64C9/16;(IPC1-7):64C9/16 主分类号 B64C9/16
代理机构 代理人
主权项
地址