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.


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    Title :

    Recent German Patents



    Publication date :

    1940-07-01


    Size :

    1 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Recent German Patents

    Emerald Group Publishing | 1940


    Recent German Patents

    Emerald Group Publishing | 1940


    Recent German Patents

    Emerald Group Publishing | 1940


    Recent patents

    Waterlow, C.B. | Engineering Index Backfile | 1930


    Recent patents

    Waterlow, C.B. | Engineering Index Backfile | 1929