The equipment has fuel supply architecture whose fuel supply units (4, 5) supply fuel to driving units (2, 3). Fuel systems (9, 10) comprise feed pumps (11, 12) and ejectors (13-16). The pumps induce circulation of fuel inside systems. Feeders (6, 7) comprise discharge devices (17-20). An intercommunication unit (21) is interposed between supply units. A transfer circuit comprises transfer pump inducing bidirectional circulation of fuel selectively from one of the supply units to the other supply unit. The ejectors are plunged into inner side of container (8) commonly arranged to supply units.


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    Title :

    ARCHITECTURE D'ALIMENTATION EN CARBURANT D'UN GROUPE DE MOTORISATION D'UNE VOITURE TOURNANTE EQUIPANT UN GIRAVION


    Contributors:

    Publication date :

    2016-05-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT