The concept of the lateralizer device is to sense the difference in wing tip static pressures (differential pressures being created by wing tip venturis) produced when any deviation from straight to level flight occurs. In a steady state turn the low slow wing tip experiences less venturi suction than the high fast wing tip. This signal activates the appropriate servos connected to the ailerons to produce a wing leveling restoring moment. If the wing is subjected to rolling velocities due to changes of the local angle of attack at the tip, the downgoing wing tip operates at a higher angle than the upgoing one. If with an increase in the angle of attack the signal is such that it increases the venturi pressure, then the servos are activated to produce the most negative signal to an upgoing aileron which results in a wing leveling restoring moment. In other words, any deviation from straight and level flight in either roll or yaw is exploited and the difference signal from the differential pressures activates the servo to effect or produce the necessary corrective action to null the signal.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Inherent Spiral Stability in a Fixed Wing Aircraft by Means of a Simplified Pneumatic Wing Tip Control System


    Beteiligte:
    G. L. Goglia (Autor:in) / B. K. Arunkumar (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    27 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Pneumatic fixed-wing aircraft

    WANG DENGSEN / WANG PEINAN | Europäisches Patentamt | 2022

    Freier Zugriff

    Pneumatic wing aircraft

    XU GUANGDI / XU ZHIHONG / XU ZHIJUN | Europäisches Patentamt | 2020

    Freier Zugriff

    FIXED-WING AIRCRAFT

    SMEENK COENRAAD LOUIS | Europäisches Patentamt | 2023

    Freier Zugriff

    FIXED-WING AIRCRAFT

    PICCOLO ANTONIO / MASTROIANNI GAETANA / PAPA UMBERTO et al. | Europäisches Patentamt | 2021

    Freier Zugriff