초록 ▼

A liquid storage tank, for example an aircraft fuel tank, having a tank wall enclosing a liquid storage space, and a tie assembly located at least partially within the liquid storage space. The tie assembly includes an elongate member, for example a wire or cable, and a plurality of attachment devic

A liquid storage tank, for example an aircraft fuel tank, having a tank wall enclosing a liquid storage space, and a tie assembly located at least partially within the liquid storage space. The tie assembly includes an elongate member, for example a wire or cable, and a plurality of attachment devices fixed to an inner surface of the tank wall. The elongate member includes a plurality of spaced part points along its length, each of the spaced apart points being fixed to a respective attachment device such that the tie assembly resists outward deformation of the tank wall.

대표청구항 ▼

1. An aircraft fuel tank comprising: a tank wall enclosing a liquid storage space, the tank wall comprising two opposing aircraft external skins and an aircraft substructure disposed between the two aircraft external skins; anda plurality of tensionable tie assemblies located at least partially with

1. An aircraft fuel tank comprising: a tank wall enclosing a liquid storage space, the tank wall comprising two opposing aircraft external skins and an aircraft substructure disposed between the two aircraft external skins; anda plurality of tensionable tie assemblies located at least partially within the liquid storage space, each tensionable tie assembly comprising:a first attachment device fixed to an inner surface of a first of the aircraft external skins;a second attachment device fixed to an inner surface of a second of the aircraft external skins; andan elongate member fixed between the first and second attachment devices of that tie assembly such that the elongate member of that tie assembly crosses the liquid storage space;wherein the tensionable tie assemblies are capable of being tightened during installation, configured to exert an inward force on the tank wall, and are more closely spaced together at or proximate to points at which the aircraft external skins are attached to the aircraft substructure. 2. The aircraft fuel tank according to claim 1, wherein each elongate member comprises one or more wires. 3. The aircraft fuel tank according to claim 2, wherein each elongate member comprises a plurality of wires that are coupled together so as to form a cable. 4. The aircraft fuel tank according to claim 1, wherein one or more elongate members are made of poly-paraphenylene terephthalamide. 5. The aircraft fuel tank according to claim 1, wherein one or more of the elongate members are normal to the aircraft external skins at points at which that elongate member is fixed to the aircraft external skins. 6. The aircraft fuel tank according to claim 1, wherein a total cavity volume of the tensionable tie assemblies in the liquid storage space is less than or equal to 5% by volume of the liquid storage space. 7. An aircraft comprising the aircraft fuel tank according to claim 1. 8. A method of providing an aircraft fuel tank, the method comprising: providing a tank wall enclosing a liquid storage space, the tank wall comprising two opposing aircraft external skins and an aircraft substructure disposed between the two aircraft external skins; andattaching a plurality of tensionable tie assemblies to the tank wall;wherein, for each tensionable tie assembly, attaching that assembly to the tank wall comprises:attaching a first attachment device to an inner surface of a first of the aircraft external skins;attaching a second attachment device to an inner surface of a second of the aircraft external skins; andfixing an elongate member between the first and second attachment devices such that the elongate member crosses the liquid storage space;wherein the tensionable tie assemblies are capable of being tightened during installation, configured to exert an inward force on the tank wall, and are more closely spaced together at or proximate to points at which the aircraft external skins are attached to the aircraft substructure. 9. The method according to claim 8, wherein: one or more of the elongate members comprise one or more wires; andthe method further includes, fixing the one or more wires between the first and second attachment devices, and subsequently tightening the one or more wires so as to exert an inward force on the tank wall.