Turbine engine including a steam system

A turbine engine for an aircraft, the turbine engine comprising:

• a core turbine engine including:
• a core air flow path for core air to flow therethrough;
• a combustor positioned in the core air flow path to receive compressed air and fluidly coupled to a fuel source to receive fuel, the fuel being injected into the combustor to mix with the compressed air to generate a fuel and air mixture, the fuel and air mixture being combusted in the combustor to generate combustion gases;
• a core shaft;
• and
• a turbine located downstream of the combustor to receive the combustion gases and to cause the turbine to rotate, the turbine coupled to the core shaft to rotate the core shaft when the turbine rotates;
• a fan coupled to the core turbine engine to be rotated by the core turbine engine;
• a steam system fluidly coupled to the combustor to provide reheated steam to the core air flow path to add mass flow to the core air, the steam system including:
• a boiler positioned downstream of the combustor, the boiler receiving water and being fluidly connected to the combustor to receive the combustion gases and to boil the water to generate steam, the boiler including an initial steam flow path to receive the water and generate the steam;
• a steam turbine fluidly coupled to the initial steam flow path of the boiler to receive the steam from the boiler and to cause the steam turbine to rotate, the steam turbine being coupled to the core shaft to rotate the core shaft when the steam turbine rotates;
• and
• a reheat boiler fluidly coupled to the steam turbine to receive the steam from the steam turbine and to reheat the steam, the reheat boiler including a reheat steam flow path to receive the steam and increase a temperature of the steam, the reheat steam flow path being a separate flow path from the initial steam flow path, wherein the combustor is fluidly coupled to the reheat steam flow path of the reheat boiler to receive the reheated steam.