Fluid loading system

Details Fluid loading system Fluid loading system

B - Operations, Transporting

64

D

B64D 1/22 (2006.01) A62C 3/02 (2006.01) B64D 1/00 (2006.01)

Patent

CA 2402907

A pump system for loading fluid into a tank onboard a translating aircraft includes a substantially rigid tube member having a diving device on the distal end of the tube member. A strut structure may also be provided on a front face of the tube member. In use, the tube member is directed rearward relative to the translating aircraft so that splashing of fluid onto the underside of the aircraft is substantially avoided.

L'invention se rapporte à un système à pompe permettant de charger un fluide dans le réservoir d'un aéronef en translation. Ce système comporte un élément tubulaire sensiblement rigide possédant, sur son extrémité distale, un dispositif plongeur. Une structure de type étai peut également être disposée sur la face avant de l'élément tubulaire. En cours de fonctionnement, l'élément tubulaire est dirigé vers le bas par rapport à l'aéronef en translation de sorte que toute projection de fluide sur la partie inférieure de l'aéronef peut être sensiblement évitée.

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