发明名称 Wing fold push-pin locking assembly
摘要 An improved wing fold assembly for use in aircraft which provides relative rotational movement of a first wing tip about a second fixed wing including a plurality of wing tip flanges, and a plurality of fixed wing flanges wherein all of said flanges are rotatably mounted to a central shaft and wherein the improvement comprises means for selectively interlocking said wing tip flanges in relation to said fixed wing flanges to thereby lock said wing tip in position relative said fixed wing in either of a folded or faired position.
申请公布号 US5558299(A) 申请公布日期 1996.09.24
申请号 US19940229637 申请日期 1994.04.19
申请人 MCDONNELL DOUGLAS CORPORATION 发明人 VEILE, JOSEPH R.
分类号 B64C3/56;B64C13/34;(IPC1-7):F16H59/00;G05G5/00 主分类号 B64C3/56
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