This SAE Aerospace Information Report (AIR) identifies and summarizes the various factors that should be considered during design, development, certification, or testing of helicopter rotor blade ice protection systems. Although various concepts of ice protection are mentioned in this report, the text is limited generally to those factors associated with design and substantiation of cyclic electrothermal ice protection systems as applicable to the protection of helicopter rotor blades. Other systems are described briefly in Appendix A. Applications consider main rotor blades, conventional tail rotor blades, and other types of antitorque devices. The information contained in this report is also limited to the identification of factors that should be considered and why the factor is important. Specific design, analysis and test methodologies are not included. For additional information refer to the references listed in 2.1. AIR1667A has been reaffirmed to comply with the SAE five-year review policy.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Rotor Blade Electrothermal Ice Protection Design Considerations


    Erscheinungsdatum :

    2013-04-23



    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





    Numerical Investigation of the Electrothermal De-Icing Process of a Rotor Blade

    Lei, Guilin / Dong, Wei / Zhu, Jianjun et al. | British Library Conference Proceedings | 2015


    Numerical Investigation of the Electrothermal De-Icing Process of a Rotor Blade

    Lei, Guilin / Zhu, Jianjun / Zheng, Mei et al. | SAE Technical Papers | 2015


    Rotor blade erosion protection system

    NISSEN JEFFREY P | Europäisches Patentamt | 2016

    Freier Zugriff

    ROTOR BLADE EROSION PROTECTION SYSTEMS

    NISSEN JEFFREY PAUL / MCCULLOUGH JOHN RICHARD | Europäisches Patentamt | 2019

    Freier Zugriff