This paper describes the development and optimization of a conceptual thermal management system for electrified aircraft. Here, a vertical takeoff and landing (VTOL) vehicle is analyzed with the following electrically sourced heat loads considered: motors, generators, rectifiers, and inverters. The vehicle will employ liquid-cooling techniques in order to acquire, transport, and reject waste heat from the vehicle. The purpose of this paper is to threefold: 1) Present a potential modeling framework for system level thermal management system simulation, 2) Analyze typical system characteristics, and 3) Perform optimization on a system developed for a specific vehicle to minimize weight gain, power utilization, and drag. Additionally, the paper will study the design process, specifically investigating the differences between steady state and transient sizing, comparing simulation techniques with a lower fidelity option and quantifying expected error.


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    Titel :

    Development of a Thermal Management System for Electrified Aircraft


    Beteiligte:

    Kongress:

    AIAA SciTech Forum ; 2020 ; Orlando, FL, United States


    Erscheinungsdatum :

    2020-03-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    DEVELOPMENT OF A THERMAL MANAGEMENT SYSTEM FOR ELECTRIFIED AIRCRAFT

    Chapman, Jeffryes W. / Schnulo, Sydney L. / Nitzsche, Michael P. | TIBKAT | 2020


    Development of a Thermal Management System for Electrified Aircraft

    Chapman, Jeffryes W. / Schnulo, Sydney L. / Nitzsche, Michael P. | AIAA | 2020


    Thermal Management System Design for Electrified Aircraft Propulsion Concepts

    Chapman, Jeffryes W. / Hasseeb, Hashmatullah / Schnulo, Sydney L. | AIAA | 2020


    Thermal Management System Design for Electrified Aircraft Propulsion Concepts

    Chapman, Jeffryes W. / Hasseeb, Hashmatullah / Schnulo, Sydney | IEEE | 2020