An electronic circuit comprising a power transistor of the MOSFET type comprising a gate connected to a control circuit of the gate. The control circuit of the gate configured to operate at a temperature called ambient temperature, non-cryogenic. The power transistor as well as an interfacing circuit connected between said gate and said control circuit configured to operate at a cryogenic temperature. Each component of the interfacing circuit established at a maximum distance (L) from the power transistor. At least one measurement means configured to measure at least one measurement signal, representative of a junction temperature of the power transistor, is connected between the interfacing circuit operating at a cryogenic temperature and the control circuit operating at ambient temperature.


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    Titel :

    POWER COMPONENT FOR ELECTRIC OR HYBRID AIRCRAFT


    Beteiligte:
    STEINER GERHARD (Autor:in) / KAPAUN FLORIAN (Autor:in) / YBANEZ LUDOVIC (Autor:in) / SURAPANENI RAVI KIRAN (Autor:in) / GALLA GOWTHAM (Autor:in)

    Erscheinungsdatum :

    23.11.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    H03K PULSE TECHNIQUE , Impulstechnik / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



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