Recent German Patents
- 1 July 1940
- journal article
- Published by Emerald Publishing in Aircraft Engineering and Aerospace Technology
- Vol. 12 (7) , 221
- https://doi.org/10.1108/eb030671
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.Keywords
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