To read the full version of this content please select one of the options below:

U.S. Patent Specifications

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 November 1938

Abstract

A combined longitudinal control and stabilization mechanism, for an airplane provided with a control stick, comprising split flaps, a single cam to operate the said flaps for purposes of longitudinal and stabilization control, said single cam being actuated by the control stick by means of the movement of a shaft, for purposes of elevational control, and means mounted on the control stick whereby the shaft may be rotated independently of the control stick for purposes of stabilization.

Citation

(1938), "U.S. Patent Specifications", Aircraft Engineering and Aerospace Technology, Vol. 10 No. 11, pp. 366-366. https://doi.org/10.1108/eb030406

Publisher

:

MCB UP Ltd

Copyright © 1938, MCB UP Limited