FUEL SUPPLY SYSTEM FOR A COMBUSTOR

A fuel supply system (100) for a combustion section (114) of a turbine engine (10). The turbine engine (10) including a heat source (110). The fuel supply system (100) comprising a first fuel supply (102) having a liquid fuel, a second fuel supply (104) having a first gaseous fuel, and a heat exchanger (108) fluidly coupled to the first fuel supply (102) and the heat source (110). The heat exchanger (108) producing a heat sufficient to change the liquid fuel to a second gaseous fuel that is the same type of fuel as the first gaseous fuel.