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

Recent German Patents

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 1 July 1940

Abstract

A differential effect of the angular displacements of control surfaces is often required in the case of aileron controls, viz., a movement whereby for a given angle of rotation the upwardly‐moved aileron shows a range of deflexion which is different, measured from the common neutral position than that of the downwardly‐moved aileron. Fig. 4 shows the position of the device if the neutral position of the aileron is moved upwards. Fig. 5 shows the same operation, but with the neutral position displaced downwards.

Citation

(1940), "Recent German Patents", Aircraft Engineering and Aerospace Technology, Vol. 12 No. 7, pp. 221-221. https://doi.org/10.1108/eb030671

Publisher

:

MCB UP Ltd

Copyright © 1940, MCB UP Limited