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. (Author)
Geared Tab
1982
5 pages
Report
Keine Angabe
Englisch
Aircraft , Mechanical Devices & Equipment , Patents , Trim tabs , Deflection , Gears , Reversible , Trim angle , Actuators , Limitations , Aerodynamic control surfaces , Auxiliary , Pivots , Hinges , Linkages , Elevators , Sensitivity , Reduction , Low velocity , Airspeed , Short takeoff aircraft , Tails(Aircraft) , TABS(Aerodynamic Control Surfaces)
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
Kraftfahrwesen | 1982
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