Dehydration of liquid fuel
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[0032]FIG. 1 illustrates a plan view of an aircraft 1, such as a commercial airliner, comprising a fuselage 2, a wing 3 and under wing mounted engines 4. The interior volume of the wing 3 is used as fuel tanks for storing liquid hydrocarbon aviation fuel, such as Jet A-1. The aircraft 1 has a three tank configuration, which forms part of an aircraft fuel system.
[0033]FIG. 2 illustrates schematically the three tank configuration which comprises a left wing tank 5, a right wing tank 6 and a centre tank 7. The aircraft fuel system further comprises a ventilation system for ventilating the ullage of each of the fuel tanks 5, 6, 7. The ventilation system includes a left vent tank 8 and a right vent tank 9 disposed at the tips of the wing 3. The vent tank 8 ventilates the left wing tank 5 by means of ventilation pipe 10, and also ventilates the centre tank 7 by means of ventilation pipe 11. The right vent tank 9 ventilates the right wing tank 6 by means of ventilation pipe 12. Each vent ...
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