Digital system gives pilot partial command when primary system fails. Emergency system provides digital control of rigid circulation-control rotor for experimental X-wing aircraft. In addition to centering collective-pitch control, new command provides limited roll control via collective pitch and gyroscopic decoupling in pitch and aerodynamic decoupling.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Emergency Control for a Circulation-Control Helicopter Rotor


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1987-06-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Investigation of a Stoppable Helicopter Rotor with Circulation Control

    J. D. Ballard / J. L. Mccloud / T. J. Forsyth | NTIS | 1980


    Helicopter control rotor

    Stuart III, J. | Engineering Index Backfile | 1948


    An investigation of a stoppable helicopter rotor with circulation control

    Ballard, J. D. / Mccloud, J. L., III / Forsyth, T. J. | NTRS | 1980


    Dual-rotor emergency rescue unmanned helicopter

    CHEN LUODAN | Europäisches Patentamt | 2024

    Freier Zugriff