This paper covers the development of two piezoelectric actuators for trailing edge flap control on mach scaled model helicopter rotors. The design, analysis and bench tests of these two actuators are described. Under different voltages and frequencies, their drive performances are tested and compared. Results showed that these two actuators all can effectively drive and control the flaps with each advantages and disadvantages.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Piezoelectric Actuators Used for Helicopter Vibration Reduction



    Erschienen in:

    Advanced Materials Research ; 718-720 ; 1729-1733


    Erscheinungsdatum :

    2013-07-31


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Reduction of the vibration in a helicopter blade using piezoelectric actuators

    Sergejs Gluhihs / Andrejs Kovalovs | DOAJ | 2006

    Freier Zugriff



    Piezoelectric actuators for helicopter rotor control

    Spangler, Ronald L., 1964- | DSpace@MIT | 1989

    Freier Zugriff