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.
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
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