An aircraft light unit is disclosed herein. The aircraft light unit includes a housing (302) having a first side and an opposing second side, a light coupled to the first side of the housing (302), a circuit board assembly (306) coupled to second side of the housing (302), a thermoelectric cooler coupled to the circuit board assembly (306) and configured to dissipated heat from the circuit board assembly (306), and a heat sink (312) disposed over the thermoelectric cooler and configured to dissipate heat from the thermoelectric cooler.
LIGHTING ELECTRONICS COOLING USING HIGH TEMP TEC WITH INTEGRATED HEAT SINK
KÜHLUNG EINER BELEUCHTUNGSELEKTRONIK UNTER VERWENDUNG VON HOCHTEMPERATUR-TEC MIT INTEGRIERTEM KÜHLKÖRPER
REFROIDISSEMENT D'ÉLECTRONIQUE D'ÉCLAIRAGE À L'AIDE D'UN TEC À TEMPÉRATURE ÉLEVÉE AVEC DISSIPATEUR THERMIQUE INTÉGRÉ
2024-02-28
Patent
Electronic Resource
English
IPC: | 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 / F21W Index-Schema in Verbindung mit den Unterklassen F21K, F21L, F21S und F21V, betreffend den Gebrauch oder Einsatz von Leuchten oder Beleuchtungssystem , INDEXING SCHEME ASSOCIATED WITH SUBCLASSES F21K, F21L, F21S and F21V, RELATING TO USES OR APPLICATIONS OF LIGHTING DEVICES OR SYSTEMS |
LIGHTING ELECTRONICS COOLING USING HIGH TEMP TEC WITH INTEGRATED HEAT SINK
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