发明名称 Tank, a fuel storage system, and an aircraft
摘要 A storage tank (25) of a storage system. The storage tank (25) includes a container (30) and a dynamic ventilation line (35) incorporated therein, said dynamic ventilation line (35) being provided with an air-no-fuel valve (45) that shuts off in the presence of fuel, the air-no-fuel valve (45) communicating with an internal space (INT) of the container (30) via an upstream pipe (40) placed inside the container (30), a downstream pipe (50) secured to a wall (31) of the container (30) extending from the air-no-fuel valve (45) and opening out into a dynamic air intake (53) communicating with the outside air (200), said storage tank having at least one communication orifice (300) for communicating with other tanks.
申请公布号 US9162772(B2) 申请公布日期 2015.10.20
申请号 US201313904232 申请日期 2013.05.29
申请人 Airbus Helicopters 发明人 Basset Gregory
分类号 B64D1/00;B64D37/06;B64D37/32;B64D37/00;B64D37/08;B64D37/16;B64D37/20 主分类号 B64D1/00
代理机构 Brooks Kushman P.C. 代理人 Brooks Kushman P.C.
主权项 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 (P1), the upstream proximal end being contained in a second plane (P2), the first plane (P1) being above the second plane (P2).
地址 Marignane Cedex FR
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