Geared tab

Aeronautics and astronautics – Aircraft control

Patent

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Details

244 82, 244 90R, 244 87, B64C 904, B64C 910

Patent

active

044311494

ABSTRACT:
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.

REFERENCES:
patent: 2207387 (1940-07-01), Tampier
patent: 2357465 (1944-09-01), Focht
patent: 2370844 (1945-03-01), Davis
patent: 2395671 (1946-02-01), Kleinhans et al.
patent: 2517680 (1950-08-01), Knowler et al.
patent: 2557426 (1951-06-01), George
patent: 2696956 (1954-12-01), Farr et al.
patent: 3000595 (1961-09-01), Dorn
patent: 3020008 (1962-02-01), Rumsey
patent: 3295797 (1967-01-01), Roberts et al.
patent: 3704843 (1972-12-01), Jenny
patent: 3785596 (1974-01-01), Chinchester-Miles

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