TY  - JOUR
AB  - 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.
VL  - 12
IS  - 7
SN  - 0002-2667
DO  - 10.1108/eb030671
UR  - https://doi.org/10.1108/eb030671
PY  - 1940
Y1  - 1940/01/01
TI  - Recent German Patents
T2  - Aircraft Engineering and Aerospace Technology
PB  - MCB UP Ltd
SP  - 221
EP  - 221
Y2  - 2024/09/21
ER  -