发明名称 Extendible airfoil track assembly
摘要 An actuation and extension mechanism for aerodynamically high-lift devices such as a wing leading edge slat or a wing trailing edge flap; wherein an aerodynamic panel is connected to one end of an extendible track member that is supported and guided by its other end through rollers fixedly mounted to wing rib structure. The track member incorporates a separate rack gear segment 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 strength, safety, or operational reliability of said combination.
申请公布号 US4471928(A) 申请公布日期 1984.09.18
申请号 US19820429871 申请日期 1982.09.30
申请人 THE BOEING COMPANY 发明人 COLE, JAMES B.
分类号 B64C9/00;B64C9/16;B64C9/20;B64C13/34;(IPC1-7):B64C9/24 主分类号 B64C9/00
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