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.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Recent German Patents



    Erscheinungsdatum :

    01.07.1940


    Format / Umfang :

    1 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    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