This report describes 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 means 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 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. (Author)
Geared Tab
1982
20 pages
Report
Keine Angabe
Englisch
Geared turbines to geared diesels
Engineering Index Backfile | 1934
Geared turbines to geared diesels
Engineering Index Backfile | 1934
Geared turbines to geared diesels
Engineering Index Backfile | 1934
Online Contents | 1995
NTIS | 1982
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