发明名称 Extendible airfoil track assembly.
摘要 <p>An actuation and extension mechanism for aerodynamic high-lift devices such as a wing leading edge slat or a wing trailing edge flap; wherein an aerodynamic panel (20) is connected to one end of an extendible track member (23) that is supported and guided by its other end through rollers (26) fixedly mounted to wing rib structure (l5). The track member incorporates a separate rack gear segment (24) internally thereof as part of the extension or retraction mechanism and this combination of track and gear segment provides the primary support and drive means to the high-lift device, without compromising the structural strenth, safety, or operational reliability of said combination.</p>
申请公布号 EP0227643(A2) 申请公布日期 1987.07.01
申请号 EP19870200084 申请日期 1981.07.08
申请人 THE BOEING COMPANY 发明人 COLE, JAMES BYRON
分类号 B64C9/24;B64C9/14;B64C9/16;B64C9/20;B64C13/34;(IPC1-7):B64C9/14 主分类号 B64C9/24
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