Patent EA-004324-B1 (EA)
Title: Water distillation system
Inventor: PAXTON GREGORY MARK
IPC: C02F1/16
Filed: 2001-02-02
Abstract: 1. A water distillation system comprising feed water means arranged to supply feed water to heat exchange means, a heat generating engine arranged to supply a stream of hot fluid to the heat exchange means for heating the feed water in the heat exchange means, a water flash evaporator arranged to receive the heated feed water from the heat exchange means for evaporating the heated water, and a condenser arranged to receive vapour formed from the heated feed water in the evaporator and to convert the vapour into water, wherein the heat generating engine is a jet engine arranged to supply a stream of hot fluid in the form of gases to the heat exchange means and further comprising air extraction means arranged so that the gas stream is induced to create a partial vacuum in the flash evaporator. 2. The system according to claim 1 further comprising water recirculating means arranged for raising pressure in the heat exchange means by recirculating water therein at a predetermined flow rate. 3. The system according to of claim 2 wherein the heat exchange means includes a first heat exchanger arranged down stream to said engine, and a second heat exchanger arranged down stream to said first heat exchanger to receive residual heat from the hot fluid, and the water recirculating means including a pump arranged to increase the feed pressure in the first heat exchanger in order to increase the extraction of sensible and latent heat from the first heat exchanger. 4. The system according to claim 3 wherein the second heat exchanger is used to preheat the feed water before the relatively high temperature first heat exchanger and the pump is used to re-circulate the water at high velocities through the high temperature heat exchanger ensuring that the temperature rise of the water is no more than 2 degree C at each pass of the water, thereby reducing any build-up of solid lining in the heat exchanger means. 5. The system according to claims 3 or 4 wherein the incoming feed water is directed into the second heat exchanger for preheating before going through the first heat exchanger, and the incoming water is used to cool and condense the steam vapour within the second heat exchanger whilst allowing a heat transfer to the incoming feed water. 6. The system according to any one of claims 1 to 5 wherein the jet engine includes a fuel gas burner with regenerative heating path for the stream of hot fluid in the form of a fuel gas. 7. The system according to any one of claims 1 to 6 wherein the heat exchange means including an insulated duct provided with a number of finned carbon steel tubes arranged across the duct, the stream of hot fluid being arranged to flow into the duct and the feed water being arranged to flow through the tubes. 8. The system according to any one of claims 1 to 7 further comprising solids transfer means associated with the evaporator for transferring from the evaporator any solid resulting from evaporation of the heated feed water. 9. The system according to claim 8 wherein the transfer means is arranged to operate intermittently in order to preserve vacuum state at the evaporator. 10. The system according to claim 8 or 9 wherein the transfer means including a revolving chamber with a counterflow of drying air. 11. The system according to claim 8 or 9 wherein the transfer means including a dewatering screw in a barrel which squeezes water from paste in the barrel. 12. The system according to any one of claims 1 to 11 wherein the engine is adapted to consume a hydrocarbon gas including methane from mining operations, or a pipeline gas including ethylene or a liquid hydrocarbon, or hydrogen from electrolysed water. 13. The system according to any one of claims 1 to 12 wherein the feed water is drawn into the heat exchange means by a pump and control means being arranged to dynamically control the temperature, flow and pressure of the water. 14. The system according to claim 1 wherein the jet engine is a turbo fan type gas turbine jet engine with a large percentage of bypass air, the hot exhaust from the jet engine being directed through an insulated duct provided with the heat exchange means having a number of finned carbon steel tubes arranged across the duct, and the system is arranged so that as the hot exhaust gas ( > 650 degree C) passes through the heat exchange means, feed water in the form of sea water or other source water in the tubes is heated under pressure to a predetermined temperature above the predetermined boiling point of the feed water, and the heated water is then released through a nozzle into the evaporator in the form of a flash distillation chamber maintained at a vacuum pressure that allows the feed water to flash boil at 60 degree C.