Surface hold-down mechanism

Aeronautics and astronautics – Aircraft control

Patent

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Details

244213, 244 75A, B64C 902

Patent

active

044986475

ABSTRACT:
A mechanical biasing device to drive an aircraft control surface to a predetermined position relative to the main airfoil, either directly or indirectly through a linkage system, while also providing sufficient clamping force at the neutral position so that the airfoil and control surface behave dynamically like a single structure.

REFERENCES:
patent: 221168 (1879-11-01), Gilfillian
patent: 590572 (1897-09-01), Henry
patent: 2370844 (1945-03-01), Davis
patent: 2550756 (1951-05-01), Bartoszek
patent: 2584667 (1952-02-01), Bockrath
patent: 2711867 (1955-06-01), Feeney et al.
patent: 2881631 (1959-04-01), Riccius
patent: 3805413 (1974-04-01), Burny et al.
patent: 3883093 (1975-05-01), Violleau
patent: 4173322 (1979-11-01), Macdonald

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