A hybrid fuel cell system includes a fuel supply system including a fuel tank, a start-up subsystem, a reforming subsystem and a depressurization system. The reforming subsystem is to receive fuel and to reform fuel to generate a hydrogen enriched gases and steam mixture. The hybrid fuel cell system includes a water supply system that provides water for the steam generator. The water supply system includes a water condenser directly downstream from the reforming subsystem that is in fluid communication with the hydrogen enriched gases and steam mixture to condense the hydrogen enriched gases and steam mixture into water and hydrogen enriched gases. The depressurization system is to reduce a pressure of the hydrogen enriched gases. The hybrid fuel cell system includes a fuel cell stack downstream from the depressurization system and having an anode inlet in fluid communication with the depressurization system to receive the hydrogen enriched gases.

A proton-conducting solid oxide fuel cell system includes a proton-conducting solid oxide fuel cell including an anode through which a flow of fuel is directed, and a cathode through which a flow of air containing 9% to 100% oxygen is directed, and a water recovery portion. The water recovery portion includes an anode water recovery unit to recover anode water from anode products output from the anode, and a cathode water recovery unit to recover cathode water from cathode products output from the cathode.

A hybrid stationary power generator is provided. The system is fueled from natural gas and based on SOFCs and high efficiency, internal combustion (IC) engine technologies is conceived to generate electric power at 100-kW scale with an efficiency of 71% and a capital cost of <900 $/kW. This novel system integrates a solid oxide fuel cell (SOFC) stack with a high efficiency stationary engine and balance-of-plant (BOP) equipment to create a hybrid power system.

In a power generation system, exhausted fuel gas exhausted from a solid oxide fuel cell (SOFC) is used as a fuel of a first combustor or a second combustor of a gas turbine, and at the same time, a part of compressed air compressed by a compressor of the gas turbine is used to drive the SOFC. The gas turbine includes the first combustor for burning fuel gas which is different from the exhausted fuel gas, a first turbine configured to be driven by combustion gas supplied from the first combustor, the second combustor for burning at least a part of the exhausted fuel gas, and a second turbine coupled with the first turbine and configured to be driven by combustion gas supplied from the second combustor.

A micro-combustion device generating electrical power raises global performance of the system, is compact, and reduces losses by utilizing an induced helical path. The device includes: injection ducts inserting a combustion agent, a fuel and/or a mixture thereof wherein the injection of the combustion agent takes place tangentially to the internal cylindrical wall, inducing a helical combustion path, the internal cylindrical walls of the chamber having a deposition of catalytic material to accelerate the combustion reaction; a turbo compressor group, including a compressor, feeding under pressure the combustion chamber through the injection ducts, and a turbine, receiving the flue gases from the discharge duct, compressor and turbine being keyed on the same axis, whereon a generator of electrical power, in turn, is keyed; and a fuel cell, fed by the flue gases through the turbine and by an oxidizing agent, implementing an electrochemical process generating additional electrical power.

A power source for an aircraft including a solid oxide fuel cell and a proton exchange membrane fuel cell along with a solid oxide fuel cell multi-power source. At least one battery is electrically coupled to the solid oxide fuel cell, the proton exchange membrane fuel cell, and an aircraft distribution network to supply electricity to the aircraft and also for becoming recharged by the solid oxide fuel cell and the proton exchange membrane fuel cell.

Provided are: a power generation system that can generate electric power efficiently with a fuel cell; and a method for operating said power generation system. This power generation system comprises: a fuel cell including a plurality of unit fuel cell modules; a gas turbine; various lines for circulating fuel gas, air, discharged fuel gas, and discharged air between the fuel cell and the gas turbine; and a control device. The control device determines the number of said unit fuel cell modules to be operated on the basis of the required power generation amount, and operates the determined number of said unit fuel cell modules.

An integrated fuel cell and engine combustor assembly includes an engine combustor having a combustion chamber fluidly coupled with a compressor and a turbine. The assembly also includes a fuel cell stack circumferentially extending around the combustion chamber of the combustor. The fuel cell stack includes fuel cells configured to generate electric current. The fuel cell stack is positioned to receive discharged air from the compressor and fuel from a fuel manifold. The fuel cells in the fuel cell stack generate electric current using the discharged air and at least some of the fuel. The fuel cell stack is positioned to radially direct partially oxidized fuel from the fuel cells into the combustion chamber of the combustor. The combustor combusts the partially oxidized fuel into one or more gaseous combustion products that are directed into and drive the downstream turbine.

Vehicles, systems, and methods for the on-board, electrochemical upgrading of hydrocarbon fuels are provided. In one embodiment, a vehicle is provided where the reformed fuel subsystem comprises an electrochemical cell, a hydrocarbon fuel inlet, an oxidizing gas inlet, an unreacted gas outlet, and a reformed hydrocarbon fuel outlet. The hydrocarbon fuel inlet is configured to direct at least a portion of hydrocarbon fuel originating from the on-board point-of-sale fuel tank to the electrolyte of the electrochemical cell. The oxidizing gas inlet is configured to direct an oxidizing gas to the positive electrode of the electrochemical cell. The positive electrode of the electrochemical cell is configured to form a reduced mediator species from the oxidizing gas. The electrochemical cell is structurally configured to contact the reduced mediator species and hydrocarbon fuel from the hydrocarbon fuel inlet with the electrolyte of the electrochemical cell to upgrade a native octane rating of the hydrocarbon fuel.

In various aspects, systems and methods are provided for operating a molten carbonate fuel cell, such as a fuel cell assembly, with increased production of syngas while also reducing or minimizing the amount of CO.sub.2 exiting the fuel cell in the cathode exhaust stream. This can allow for improved efficiency of syngas production while also generating electrical power.