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.
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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 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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