Distillation system that uses gas turbine engine exhaust

A distillation system, comprising:

• a tank having a first end wall, a second end wall, a front wall, a back wall, a top wall, and a bottom wall that together define an inner volume, a divider wall disposed within the tank and dividing the inner volume into a main chamber and a settling chamber, the main chamber having at least a fluid inlet port and an exhaust gas inlet port, the settling chamber having at least an exhaust gas outlet port, the divider wall having a divider wall opening formed therein that provides fluid communication between the main chamber and the settling chamber;
• a diffuser disposed within the main chamber and coupled to the exhaust gas inlet port;
• a first nozzle wall disposed within the main chamber and coupled to the diffuser, the first nozzle wall spaced apart from the front wall of the tank to define, within the main chamber, an inlet volume between the first nozzle wall and the front wall, the first nozzle wall having at least one first baffle nozzle formed therein;
• a first baffle wall having a plurality of first baffle openings extending therethrough, the first baffle wall disposed within the main chamber and spaced apart from the first nozzle wall to define, within the main chamber, a first mixing volume between the first nozzle wall and the first baffle wall;
• a second nozzle wall disposed within the main chamber and spaced apart from the first baffle wall to define, within the main chamber, an intermediate volume, the second nozzle wall having at least one second baffle nozzle formed therein;
• and
• a second baffle wall having a plurality of second baffle openings extending therethrough, the second baffle wall disposed within the main chamber and spaced apart from the second nozzle wall to define, the within the main chamber, a second mixing volume between the second nozzle wall and the second baffle wall, the second baffle wall further spaced apart from the back wall of the tank to define, within the main chamber, an outlet volume;
• a gas turbine engine in fluid communication with the exhaust gas inlet port, the gas turbine engine configured, during operation thereof, to discharge exhaust gas into the inlet volume via the diffuser;
• and
• an engine control in operable communication with the gas turbine engine, and configured to control the operation of the gas turbine engine.