Environmental Control System (ECS) of an aircraft is a complex system which operates classically in an air standard refrigeration cycle. ECS controls the temperature, pressure and flow of supply air to the cockpit, cabin or occupied compartments. The air cycle system of ECS takes engine bleed air as input. Parameters like bleed air pressure and temperature, mass flow, the external factors like ambient temperature, pressure, and aircraft attitude affect the performance of ECS to a large extent especially during transient. So, it is very important to consider the transient characteristics of these parameters in the design stage itself in order to ascertain the dynamic response of the system. This paper explains in detail the importance of transient input characteristics during the detailed design of ECS. A typical temperature control scheme for combat aircraft ECS has been studied and modeled in LMS AMESim. Cases of transient response of temperature control system are simulated and confirmed with actual scenario. The validated model and results can be used in designing a better control on ECS.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Modeling and Simulation of a Fighter Aircraft Cabin Temperature Control System Using AMESim


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    International Conference on Advances in Design, Materials, Manufacturing and Surface Engineering for Mobility ; 2020



    Erscheinungsdatum :

    25.09.2020




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Modeling and Simulation of a Fighter Aircraft Cabin Temperature Control System Using AMESim

    Sathiyaseelan, A. / Arul Mozhi Selvan, V. | British Library Conference Proceedings | 2020


    Modeling and Simulation of a Fighter Aircraft Cabin Temperature Control System Using AMESim

    A, Sathiyaseelan / V, Arul Mozhi Selvan | British Library Conference Proceedings | 2020


    Modeling and Simulation of a Fighter Aircraft Cabin Pressure Control System Using AMESim

    A, Sathiyaseelan / Selvan, Arul Mozhi | British Library Conference Proceedings | 2022


    Modeling and Simulation of a Fighter Aircraft Cabin Pressure Control System Using AMESim

    Selvan, Arul Mozhi / A, Sathiyaseelan | SAE Technical Papers | 2022


    Modeling and Simulation of Lift Axle Control System at Vehicle Level Using AMESim

    Pendyala, Vamsi Krishna / T, Sukumar / R, Vinoth Kumar | British Library Conference Proceedings | 2021