发明名称 Lift enhancing tabs for airfoils
摘要 A tab deployable from the trailing edge of a main airfoil element forces flow onto a following airfoil element, such as a flap, to keep the flow attached and thus enhance lift. For aircraft wings with high lift systems that include leading edge slats, the slats may also be provided with tabs to turn the flow onto the following main element.
申请公布号 US5294080(A) 申请公布日期 1994.03.15
申请号 US19930014581 申请日期 1993.02.08
申请人 THE UNITED STATES OF AMERICA AS REPRESENTED BY THE ADMINISTRATOR OF NATIONAL AERONAUTICS AND SPACE ADMINISTRATION 发明人 ROSS, JAMES C.
分类号 B64C9/14;B64C23/00;(IPC1-7):B64C9/16 主分类号 B64C9/14
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