Aircraft fuel tank assembly

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 37/00 (2006.01) F04C 14/00 (2006.01)

Patent

CA 2633428

An aircraft fuel tank assembly (101) includes a tank for holding fuel (102), a canister (111) and a fuel pump assembly (103). The fuel pump assembly (103) includes: an electric motor (104), a pump (105) and an electronics unit (106). The electronics unit (106) and canister (111) are arranged so that, in use, a dry bay (115) is defined between the electronics unit and the canister.

L~invention concerne un ensemble (101) réservoir carburant d~aéronef comportant un réservoir (102) destiné à contenir un carburant, un boîtier métallique (111) et un ensemble (103) pompe à carburant. L~ensemble (103) pompe à carburant comporte : un moteur électrique (104), une pompe (105) et un module électronique (106). Le module électronique (106) et le boîtier métallique (111) sont disposés de façon à définir, en pratique, une baie sèche (115) entre le module électronique et le boîtier métallique.

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