Patent ID: 9162772
Filing Date: 2015-10-20
Classification: B64D,Y10T

Abstract:
1. A storage tank of a fuel storage system of an aircraft, wherein the storage tank includes a container and a dynamic ventilation line incorporated therein, the dynamic ventilation line being provided with an air-no-fuel valve that shuts off in the presence of fuel, the air-no-fuel valve communicating with an internal space (INT) of the container via an upstream pipe placed inside the container, a downstream pipe secured to a wall of the container extending from the air-no-fuel valve and opening out into a dynamic air intake communicating with the outside air, the storage tank having at least one communication orifice for communicating with other tanks, wherein the upstream pipe extends from a free upstream distal end towards an upstream proximal end fastened to the air-no-fuel valve, the upstream distal end being contained in a first plane (P 1 ), the upstream proximal end being contained in a second plane (P 2 ), the first plane (P 1 ) being above the second plane (P 2 ).