The concept of a more electric aircraft has revolutionized the way aircraft and subsystems are being built. New components are also proving to be more efficient, resulting in the possibility of changing the way systems are cooled. Before these new concepts will be utilized, they must be evaluated to determine system level impacts. To aid in these evaluations, an engine model is developed, traditional cooling schemes system level impacts calculated, a boundary layer heat sink proposed, and several new technologies proposed for evaluation.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Heat Sink Options for a More Electric Aircraft Thermal Management System


    Additional title:

    Sae Technical Papers


    Contributors:
    Beam, Jerry (author)

    Conference:

    SAE Aerospace Power Systems Conference ; 1997



    Publication date :

    1997-06-18




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    Heat Sink Options for a More Electric Aircraft Thermal Management System

    Beam, J. / SAE | British Library Conference Proceedings | 1997


    Aircraft Thermal Management -Heat Sink Challenge

    Lui, Clarence / Dooley, Matthew / Lui, NIcholas et al. | SAE Technical Papers | 2014


    Aircraft Thermal Management -Heat Sink Challenge

    Dooley, M. / Lui, N. / Newman, R. et al. | British Library Conference Proceedings | 2014


    High Heat Sink Fuels for Improved Aircraft Thermal Management

    Binns, K. E. / Morris, R. W. / Anderson, S. D. et al. | SAE Technical Papers | 1993


    Thermal management using endothermic heat sink

    JOHNSON DOUGLAS J / NIEDBALSKI NICHOLAS P / ERVIN JAMIE S et al. | European Patent Office | 2021

    Free access