发明名称 Segmented variable sweep wing aircraft
摘要 A segmented variable sweep wing for an aircraft has a plurality of wing segments. A structural device movably affixes the wing segments to the fuselage of the aircraft adjacent each other at their root areas. The structural device moves the segments conjointly to a power position where the segments are perpendicular to the fuselage and spaced from each other. The structural device also moves the segments conjointly to a cruise position wherein the segments are swept back at an angle with the fuselage and in abutment with each other thereby forming a unitary continuous surface airfoil.
申请公布号 US5312070(A) 申请公布日期 1994.05.17
申请号 US19920862318 申请日期 1992.04.02
申请人 GRUMMAN AEROSPACE CORPORATION 发明人 ARENA, ALDO
分类号 B64C3/40;B64C9/28;(IPC1-7):B64C3/38 主分类号 B64C3/40
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