U.S. Patent Specifications

Abstract

An aircraft control system comprising a wing, means mounting the wing for hinge movement so that the leading edge thereof is movable upwardly and downwardly, a link, means pivotally connecting one end of the link to the wing for movement in response to adjustment of the wing, an elevator, means mounting the elevator for pivotal movement, a post, the link being pivotally connected to the post in order to cause the post to be pivotally actuated in response to pivotal movement of the wing, a control for the elevator and including a cable having one part connected to the post and operativcly connected to the upper surface part of the elevator and having another part connected to the lower surface of the elevator and to the post.

Citation

(1960), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 32 No. 3, pp. 93-93. https://doi.org/10.1108/eb033230