A system (10) is provided for an aircraft. This aircraft system (10) includes a heat exchanger (20), a lubricant flow circuit (16) and a bypass valve (24). The lubricant flow circuit (16) includes an inlet passage, an outlet passage, a heat exchanger passage (34) and a bypass passage (36). The heat exchanger passage (34) extends through the heat exchanger (20). The bypass passage (36) bypasses the heat exchanger (20). The heat exchanger passage (34) and the bypass passage (36) are fluidly coupled in parallel between the inlet passage and the outlet passage. The bypass valve (24) is fluidly coupled inline along the lubricant flow circuit (16). The bypass valve (24) is operable to regulate lubricant flow through the bypass passage (36). The bypass valve (24) includes a rotary electric motor (52).


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    Title :

    AIRCRAFT HEAT EXCHANGER BYPASS FLOW CONTROL WITH ELECTRIC MOTOR


    Additional title:

    BYPASS-FLUSSSTEUERUNG FÜR EINEN FLUGZEUGWÄRMETAUSCHER MIT ELEKTROMOTOR
    COMMANDE DE FLUX DE DÉRIVATION D'ÉCHANGEUR DE CHALEUR D'AÉRONEF AVEC MOTEUR ÉLECTRIQUE


    Contributors:

    Publication date :

    2025-05-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F01M Schmierung von Kraft- und Arbeitsmaschinen oder Kraftmaschinen allgemein , LUBRICATING OF MACHINES OR ENGINES IN GENERAL / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F16K VALVES , Ventile



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