PROBLEM TO BE SOLVED: To provide a fuel manifold (1) adapted to communicate with at least one fuel tank of an aircraft, the manifold (1) defining an enclosure (2) adapted to be filled with fuel and to have an internal pressure P1 higher than an internal pressure P2 of the fuel tank, the enclosure (2) including at least one ceiling (3) and at least one side wall (4a) provided with overflow holes (7) adapted to communicate with the fuel tank.SOLUTION: The manifold (1) includes means (10, 11) for discharging an air pocket (6) trapped between the ceiling (3) and the level of the overflow holes (7), to the fuel tank.SELECTED DRAWING: Figure 2

    【課題】本発明は、航空機の少なくとも1つの燃料タンクと連通するようになっている燃料マニホールド(1)であって、燃料が充填され且つ燃料タンクの内圧P2よりも高い内圧P1を有するようになっているエンクロージャ(2)を画成し、エンクロージャ(2)が、少なくとも1つの天井部(3)と、燃料タンクと連通するようになっているオーバーフロー孔(7)が設けられた少なくとも1つの側壁部(4a)とを有する、マニホールド(1)に関する。【解決手段】本発明によれば、マニホールド(1)は、天井部(3)とオーバーフロー孔(7)の高さとの間に捕捉されたエアポケット(6)を燃料タンクに排出する手段(10,11)を備える。【選択図】図2


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    Title :

    FUEL MANIFOLD FOR AIRCRAFT TANK


    Additional title:

    航空機タンク用の燃料マニホールド


    Contributors:

    Publication date :

    2017-10-19


    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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