发明名称 |
Geared tab |
摘要 |
An improved geared tab configuration for a moveable airfoil, such as an elevator of an aircraft, is provided which comprises a tab pivotally connected to the airfoil, and linkage connecting the airfoil to the tab for simultaneous opposing pivotal movement of the tab relative to the airfoil to a maximum tab deflection at a determinable intermediate upward airfoil deflection beyond which the relative tab deflection reverses and fairs to the airfoil at a determinable maximum upward airfoil deflection.
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申请公布号 |
US4431149(A) |
申请公布日期 |
1984.02.14 |
申请号 |
US19820347807 |
申请日期 |
1982.02.11 |
申请人 |
THE UNITED STATES OF AMERICA AS REPRESENTED BY THE SECRETARY OF THE AIR FORCE |
发明人 |
BRISLAWN, MARK G.;BRYANT, DAVID W.;RAYBURN, GERALD A. |
分类号 |
B64C9/10;(IPC1-7):B64C9/04 |
主分类号 |
B64C9/10 |
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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