An aircraft light unit is disclosed herein. The aircraft light unit includes a housing having a first side and an opposing second side, a light coupled to the first side of the housing, a circuit board assembly coupled to second side of the housing, a thermoelectric cooler coupled to the circuit board assembly and configured to dissipated heat from the circuit board assembly, and a heat sink disposed over the thermoelectric cooler and configured to dissipate heat from the thermoelectric cooler.


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    Titel :

    LIGHTING ELECTRONICS COOLING USING HIGH TEMP TEC WITH INTEGRATED HEAT SINK


    Beteiligte:
    ACHARYA PRADEEP (Autor:in) / RAO SREEKANTH (Autor:in) / KRISHNA ABHILASH (Autor:in) / NANJUNDAPPA ANAND (Autor:in)

    Erscheinungsdatum :

    21.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F21S Ortsfeste Leuchten , NON-PORTABLE LIGHTING DEVICES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F21V FUNCTIONAL FEATURES OR DETAILS OF LIGHTING DEVICES OR SYSTEMS THEREOF , Funktionsmerkmale oder Einzelheiten von Leuchten oder Beleuchtungssystemen / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL



    LIGHTING ELECTRONICS COOLING USING HIGH TEMP TEC WITH INTEGRATED HEAT SINK

    ACHARYA PRADEEP / RAO SREEKANTH / KRISHNA ABHILASH et al. | Europäisches Patentamt | 2024

    Freier Zugriff

    Thermal Characterization of Copper Microchannel Heat Sink for Power Electronics Cooling

    Singh, Randeep / Akbarzadeh, Aliakbar / Mochizuki, Masataka et al. | AIAA | 2009


    Active Heat Sink for Automotive Electronics

    Vetrovec, John | SAE Technical Papers | 2009