The integrated engine inlet thermal anti-icing and environmental control system (TAI/ECS) for subsonic transport airplanes was conceived primarily for the efficient use of available energy and minimum engine bleed air extraction. The concept employs the engine inlet leading edge as the heat exchanger to provide ice protection for the engine inlet surfaces and to cool bleed air for the environmental control system. The results of a study conducted for a typical wide-body airplane using high bypass ratio engines show that the system concept will result in potential improvements in airplane operation and engine maintenance.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Integrated Engine Inlet Thermal Anti-Icing and Environmental Control System (TAI/ECS)


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Shah, A. D. (Autor:in)

    Kongress:

    National Air Transportation Meeting ; 1976



    Erscheinungsdatum :

    1976-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Thermal analysis of engine inlet anti-icing systems

    KEITH, THEO G. / DEWITT, KENNETH J. / NATHMAN, JAMES K. et al. | AIAA | 1990


    Thermal analysis of engine inlet anti-icing systems

    KEITH, JR., THEO / DE WITT, KENNETH / NATHMAN, JAMES et al. | AIAA | 1989


    Thermal analysis of engine inlet anti-icing systems

    Al-Khalil, K.M. / Keith, T.G. jun. / Witt, K.J. de et al. | Tema Archiv | 1988


    COMPOUND ENGINE ASSEMBLY WITH INLET LIP ANTI-ICING

    LAMARRE SYLVAIN / FONTAINE MIKE / JULIEN ANDRE et al. | Europäisches Patentamt | 2023

    Freier Zugriff