The invention proposes an arrangement of a tank of lubrication liquid for an aircraft turbomachine (12), under a nacelle cowling (10) covering said turbomachine (12), with the tank being arranged in the volume located between the turbomachine (12) and the nacelle cowling (10), with the nacelle cowling (10) comprising an opening (22) for access to said volume, characterised in that the tank (18) is fastened to an internal face (20a) of a panel (20) closing off said opening (22), with the unit formed by the panel (20) and the tank being added onto the nacelle cowling (10) and able to be mounted and dismounted from the nacelle cowling (10).

    Linvention propose une disposition dun réservoir de liquide de lubrification pour une turbomachine daéronef (12) sous un capot de nacelle (10) couvrant la turbomachine (12), le réservoir étant disposé dans le volume situé entre la turbomachine (12) et le capot de nacelle (10), ce capot de nacelle (10) comprenant une ouverture (22) pour accéder au volume, laquelle est caractérisée de sorte que le réservoir (18) est attaché à une face interne (20a) dun panneau (20) fermant louverture (22), lunité étant formée par le panneau (20) et le réservoir étant ajouté au capot de nacelle (10) et pouvant être monté et démonté du capot de nacelle (10).


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    Title :

    ARRANGEMENT FOR A TANK BETWEEN A NACELLE COWLING AND A TURBOMACHINE


    Additional title:

    AGENCEMENT DE CITERNE ENTRE UN CAPOT DE NACELLE ET UNE TURBOMACHINE


    Contributors:

    Publication date :

    2021-05-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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