PROBLEM TO BE SOLVED: To provide a cooling system for a central wing tank of an aircraft.SOLUTION: A cooling system for a fuel tank of an aircraft includes a temperature sensor 140, a cooling system 60, and a control module 72. The temperature sensor detects a fuel temperature in the fuel tank 24. The cooling system so maintains the fuel temperature as to be lower than a control temperature. A phase change cooling system 92 includes a heat exchanger 86. A cooling fluid flows through the heat exchanger, and thermally communicates with a surface of the fuel tank. The control module performs signal communication between itself, and the temperature sensor and the cooling system. The control module includes: a control logic for monitoring the temperature sensor; a control logic for determining whether the fuel temperature is higher than the control temperature or not; and a control logic for generating an operation signal.SELECTED DRAWING: Figure 2

    【課題】航空機の中央翼タンク用の冷却システムを提供する。【解決手段】航空機の燃料タンク用の冷却システムが、温度センサ140と、冷却システム60と、制御モジュール72とを含む。温度センサは、燃料タンク24内の燃料温度を検知する。冷却システムは、燃料温度を、制御温度より低く維持する。相変化冷却システム92は、熱交換器86を含む。冷却流体が、熱交換器を通って流れ、燃料タンクの表面と、熱的に連通している。制御モジュールは、温度センサ、及び冷却システムと信号通信する。制御モジュールは、温度センサを監視する制御ロジックと、燃料温度が、制御温度より高いかどうかを判定する制御ロジックと、作動信号を生成する制御ロジックとを含む。【選択図】図2


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    Title :

    COOLING SYSTEM FOR CENTRAL WING TANK OF AIRCRAFT


    Additional title:

    航空機の中央翼タンク用の冷却システム



    Publication date :

    2016-06-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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