Disclosed is a liquid storage system having an outer tank (e.g. an aircraft fuel tank) for containing a liquid (e.g. aircraft fuel), the outer tank enclosing a liquid storage space; an inner tank located within the outer tank and enclosing the liquid storage space; and at least one coupling element associated with the outer tank and the inner tank for maintaining the tanks in a spaced apart relationship; wherein the coupling element(s) is/are deformable such that, on application of a force to the inner tank, at least part of the inner tank moves relative to the outer tank.

Disclosed is a liquid storage system comprising a tank for containing a liquid, said tank enclosing a liquid storage space, and a plurality of spaced apart protrusions extending from an internal surface of the tank into the liquid storage space. The protrusions are resistant to deformation and deflection caused by shockwaves within a liquid in the tank resulting from impact of a projectile with the tank, for example, the protrusions may be rigid and be polygonal prisms in shape.

A liquid storage tank, for example an aircraft fuel tank, comprising a tank wall enclosing a liquid storage space, and a tie assembly located at least partially within the liquid storage space. The tie assembly comprises 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.

Disclosed is a liquid storage system comprising: an outer tank (e.g. an aircraft fuel tank) for containing a liquid (e.g. aircraft fuel), said outer tank enclosing a liquid storage space; an inner tank located within the outer tank and enclosing the liquid storage space; and spacing means associated with the outer tank and the inner tank for maintaining the tanks in a spaced apart relationship; wherein the spacing means are deformable such that, on application of a force to the inner tank, at least part of the inner tank moves relative to the outer tank.

A liquid storage system comprising: a tank for containing a liquid, the tank enclosing a liquid storage space; multiple layers of a fabric material; and attachment means attaching the multiple layers of the fabric material to an internal surface of the tank. The attachment means may comprise a non-permeable envelope attached to the internal surface of the tank. The multiple layers of the fabric material may be enclosed in the envelope such that the multiple layers of a fabric are isolated from a fluid in the tank. The envelope may contain a fluid (e.g. air) in addition to the multiple layers of the fabric material.

BAFFLE Disclosed is a baffle (40) for locating in a tank (16) for containing liquid (e.g. an aircraft fuel tank). The baffle (40) is a tubular member through which a liquid may flow. The baffle (40) comprises: a first tubular portion (42) providing a tubular outer wall, and a second tubular portion (44) located within the first tubular portion (42) and providing a tubular inner wall. The first and second tubular portions (42, 44) are substantially parallel. The first and second tubular portions (42, 44) are spaced apart to define a chamber (46)therebetween. The baffle (42, 44) further comprises radial side walls between the first and second tubular portions (42, 44) such that the chamber (46) is a sealed chamber. The chamber (46) may be filled with a compressible gas or gaseous mixture.

A liquid storage system comprising: a tank for containing a liquid, the tank enclosing a liquid storage space; and a tank liner fixedly attached to an internal surface of the tank (16). The tank liner comprises: a plurality of elements, each element having a hardness value of 2 GPa or above; and a binder material in which the plurality of elements are embedded. The elements have a higher hardness value than the binder material. A distance between a first element and the internal surface of the tank in a direction normal to the internal surface of the tank is different to a distance between a second element and the internal surface of the tank in the direction normal to the internal surface of the tank, the first element being different to the second element.

A tanker aircraft capacity extension system shaped to fit within an aircraft cargo area may include a first portable fuel container having a first outlet port adapted to connect to an integral fuel system of the aircraft, and a first inlet port; and a second portable fuel container having a second outlet port adapted to connect to the first inlet port and a second inlet port adapted to connect to a third fuel container; when the second outlet port is connected to the first inlet port and the first outlet port is connected to the integral fuel system of the aircraft, fuel flows from the second fuel container, through the outlet port to the first inlet port into the interior of the first container, and out from the first outlet port of the first container.