In a combined steam and gas
turbine engine cycle, a
combustion chamber is made durable against
high pressure and enlarged in length to increase the operation pressure ratio, without exceeding the heat durability temperature of the
system while increasing the fuel
combustion gas
mass flow four times as much as the conventional
turbine system and simultaneously for greatly raising the
thermal efficiency of the
system and specific power of the combined steam and gas
turbine engine.Water pipes and steam pipes are arranged inside the
combustion chamber so that the
combustion chamber can function as a
heat exchanger and thereby convert most of the combustion
thermal energy into super-critical steam energy for driving a
steam turbine and subsequently raising the operation pressure ratio and the thermal efficiencies of the
steam turbine cycle and gas turbine cycle. The combustion gas
mass flow can be also increased by four times as much as the conventional turbine system (up to the theoretical air to fuel ratio) and the
thermal efficiency and the specific power of the gas turbine cycle are considerably increased.Further, the
thermal efficiency of the combined system is improved by installing a magnetic friction
power transmission system to transmit the power of the system to outer loads.