Abstract: Techniques for generating power are provided. Such techniques involve a thermodynamic system including a housing, a turbine positioned in a turbine cavity of the housing, a compressor positioned in a compressor cavity of the housing, and an alternator positioned in a rotor cavity between the turbine and compressor cavities. The compressor has a high-pressure face facing an inlet of the compressor cavity and a low-pressure face on an opposite side thereof. The alternator has a rotor shaft operatively connected to the turbine and compressor, and is supported in the housing by bearings. Ridges extending from the low-pressure face of the compressor may be provided for balancing thrust across the compressor. Seals may be positioned about the alternator for selectively leaking fluid into the rotor cavity to reduce the temperature therein.

Abstract: During an adiabatic compressed air energy storage (ACAES) system's operation, energy imbalances may arise between thermal energy storage (TES) in the system and the thermal energy required to raise the temperature of a given volume of compressed air to a desired turbine entry temperature after the air is discharged from compressed air storage of the ACAES system. To redress this energy imbalance it is proposed to selectively supply additional thermal energy to the given volume of compressed air after it received thermal energy from the TES and before it expands through the turbine. The additional thermal energy is supplied from an external source, i.e. fuel burnt in a combustor. The amount of thermal energy added to the given volume of compressed air after it received thermal energy from the TES is much smaller than the amount of useful work obtained from the given volume of compressed air by the turbine.

Abstract: Operating a vehicle includes receiving, by a central controller, positional data related to the vehicle and environmental data related to a current route of the vehicle. The central controller calculates a desired energy allocation based on the positional data and the environmental data, and transmits the desired energy allocation to the vehicle for use in controlling engine function.

Abstract: Systems for recovering heat from a biomass gasifier are provided. One gasification system includes a gasifier having an inlet section configured to receive a biomass feedstock and air, and a reactor section configured to gasify a mixture of the biomass feedstock and the air to generate a producer gas. The gasifier also has an outlet section configured to output the producer gas from the reactor section. The gasification system also includes a heat exchanger system coupled to the gasifier. The heat exchanger system is configured to recover heat from the gasifier by transferring heat to a fluid to create a heated fluid.

Abstract: A power generation system includes a compression unit which compresses a gas, a storage which stores the compressed gas output from the compression unit, a first expansion unit which generates first power and outputs a first exhaust gas, a heating unit which heats at least the stored gas output from the storage, a second expansion unit which generates second power and outputs a second exhaust gas, a first regenerator which performs a first heat exchange between the second exhaust gas and the stored gas output from the storage, to generate a first heat exchange gas used to generate the first power and a first regenerator gas, and a second regenerator which performs a second heat exchange between the first exhaust gas and the first regenerator gas to generate a second heat exchange gas used to generate the second power after heated at the heating unit.

Abstract: This invention is the use of a fuel cell for powering all the components of a jet engine, but especially heating elements used to heat the air moving through the engine, rather than burning jet fuel.

Abstract: In various embodiments, compressed-gas energy storage and recovery systems include a cylinder assembly for compression and/or expansion of gas, a reservoir for storage and/or supply of compressed gas, and a system for thermally conditioning gas within the reservoir.

Abstract: Described herein are gradual oxidation systems that receive and process solid, liquid, or gaseous fuels. The system can include a solid fuel gasifier that extracts and cleans gas fuel from a solid fuel. The system can also include a reaction chamber that receives the gas fuel and maintains a gradual oxidation process of the fuel. In some embodiments, liquids containing contaminants can be oxidized within the gradual oxidation chamber. Liquid fuels and gas fuels may be communicated to the oxidation chamber separately or in combination.

Abstract: Described herein are gradual oxidation systems that receive and process solid, liquid, or gaseous fuels. The system can include a solid fuel gasifier that extracts and cleans gas fuel from a solid fuel. The system can also include a reaction chamber that receives the gas fuel and maintains a gradual oxidation process of the fuel. In some embodiments, liquids containing contaminants can be oxidized within the gradual oxidation chamber. Liquid fuels and gas fuels may be communicated to the oxidation chamber separately or in combination.

Abstract: A solar-thermal gas turbine generator is equipped with a compressor, a heat receiver, and a turbine. Additionally, there is a generator that is driven by the solar-thermal gas turbine to generate power; and a steam power generation cycle in which high-temperature air exhausted from the turbine is introduced into a steam generator and in which a steam turbine that is operated with steam generated at the steam generator drives a generator to generator power, wherein a solar-thermal steam generator that generates steam by being heated with heat collected by the light collector is provided upstream of the steam turbine of the steam power generation cycle, and a distribution ratio for distributing the sunlight collected by the light collector to the heat receiver and the solar-thermal steam generator is adjusted in accordance with the sunlight intensity.

Abstract: A gas supply device includes a first flow channel connecting a heat-treating furnace and a power generation device, a pressure control valve arranged in the first flow channel for controlling a pressure of exhaust gas flowing through the first flow channel, and a furnace pressure gauge measuring a pressure within the heat-treating furnace. If the pressure within the heat-treating furnace measured by the furnace pressure gauge becomes lower than a predetermined value, the pressure control valve controls the pressure of the exhaust gas to increase the pressure of the exhaust gas within the first flow channel.

Abstract: A Rankine cycle apparatus includes a circuit having a pump for working fluid, a heat exchanger for causing heat exchange between the working fluid and fluid supplied from an exhaust heat source, and an expanding portion that expands the working fluid that has been exposed to the heat exchange to produce mechanical energy. The expanding portion includes a fixed scroll, a movable scroll that orbits with respect to the fixed scroll, and a back pressure chamber arranged at the side corresponding to a backside of the movable scroll opposite to the surface facing the fixed scroll. The Rankine cycle apparatus further includes an inlet mechanism for introducing the working fluid from a high pressure zone that extends from the outlet side of the pump to the inlet of the heat exchanger to the back pressure chamber to produce back pressure that presses the movable scroll against the fixed scroll.

Abstract: An apparatus can include a pressure vessel that defines an interior region that can contain a liquid and/or a gas. A piston is movably disposed within the interior region of the pressure vessel. A divider is fixedly disposed within the interior region of the pressure vessel and divides the interior region into a first interior region on a first side of the divider and a second interior region on a second, opposite side of the divider. The piston is movable between a first position in which fluid having a first pressure is disposed within the first interior region and the first interior region has a volume less than a volume of the second interior region, and a second position in which fluid having a second pressure is disposed within the second interior region and the second interior region has a volume less than a volume of the first interior region.

Abstract: A solar receiver for a solar thermal power system includes a silicon carbide body having a passage therethrough. A coating on an outer surface of the silicon carbide body may increase absorption of solar radiation relative to the silicon carbide body. A plurality of silicon carbide fins may extend outwardly from the silicon carbide body, the fins oriented such that when the receiver is placed on a tower of a solar thermal power system having a plurality of heliostats, the fins are substantially perpendicularly to solar radiation received on the silicon carbide body from the plurality of heliostats.

Abstract: In various embodiments, systems for providing a constant electrical output from a compressed gas energy storage and recovery system include a hydraulic-pneumatic energy storage and recovery system configured to provide a varying pressure profile at least at one outlet, a hydraulic motor-pump in fluid communication with the outlet, and a control system for enabling the constant electrical output by controlling at least one of pressure, piston position, power, flow rate, torque, RPM, current, voltage, frequency, or displacement per revolution.

Abstract: The present invention generally relates to power generation methods and secondary processes yielding a supply of carbon dioxide. In one embodiment, the present invention relates to a supercritical carbon dioxide cycle power generator utilizing at least a portion of waste heat from the secondary process that also provides at least a portion of carbon dioxide within the supercritical carbon dioxide cycle.

Abstract: According to a first aspect of the invention there is provided a thermodynamic machine operating according to the Brayton cycle and including a closed loop fluid circuit for circulating working fluid. A fluid compressor (8) and a fluid expander (10) are independently controllable variable positive displacement machines. The variable positive displacement machines incorporate working chambers of cyclically varying volume, the net fluid displacement of each working chamber being selectable on a cycle by cycle basis. The compressor and expander axles are linked and the compressor and expander can be controlled to independently vary the displacement of the compressor, the displacement of the expander and the net torque exerted on the axle. The machine works efficiently with a wide range of heat source and heat sink temperatures and can respond to varying power demands, including transient changes to power demand.

Abstract: The present invention describes a novel integration between wind and solar thermal renewable energy technologies. An existing wind turbine consisting of a hub and blades is operated by the power generated from a waterless solar thermal system (using high pressure, high temperature air) during periods of low wind availability. The solar thermal system consist of a heliostat field, solar air receiver panels, a thermal energy storage tank and a Pelton wheel assembly system for converting thermal energy of air into kinetic energy of the power shaft of the wind turbine. The thermal energy converting system consists of a plurality of supersonic air nozzles acting as stator, producing supersonic air jets to interact with a rotating Pelton wheel. A thermal storage system provides means for energy dispatchability. The proposed integrated system is capable of generating a stable renewable energy with minimum intermittency.

Abstract: Waste heat energy conversion cycles, systems and devices use multiple waste heat exchangers arranged in series in a waste heat stream, and multiple thermodynamic cycles run in parallel with the waste heat exchangers in order to maximize thermal energy extraction from the waste heat stream by a working fluid. The parallel cycles operate in different temperature ranges with a lower temperature work output used to drive a working fluid pump. A working fluid mass management system is integrated into or connected to the cycles.

Abstract: Systems and methods are described herein to operate an air compression and/or expansion system in its most efficient regime, at a desired efficiency, and/or achieve a desired pressure ratio independent of discharge temperature, with little to no impact on thermal efficiency. For example, systems and methods are provided for controlling and operating hydraulic pumps/motors used within a hydraulically actuated device/system, such as, for example, a gas compression and/or expansion energy system, in its most efficient regime, continuously, substantially continuously, intermittently, or varied throughout an operating cycle or stroke of the system to achieve any desired pressure and temperature profile. Such systems and methods can achieve any desired pressure ratio independent of input or discharge temperature, and can also achieve any desired discharge temperature independent of pressure ratio, without altering any of the structural components of the device or system.

Abstract: A method of generating power from a heat source, said method including: compressing (10) a working fluid to increase its temperature; exchanging (11) heat between said working fluid and said heat source to superheat said working fluid; expanding (12) said superheated working fluid to drive a turbine, thereby reducing its temperature; condensing (13) said working fluid to further reduce its temperature: and returning said working fluid to said compressing step (10), the method further including the step (14) of regenerating the heat of said working fluid wherein working fluid passing between said compressing step (10) and said heat exchanging step (11) exchanges heat with working fluid passing between said expanding step (12) and said condensing step (13); wherein said steps are performed in a thermodynamic cycle (S1-S1?-S2-S3-S3?-S4) within a supercritical region (SC) above the saturation dome (A) of said working fluid, and wherein said heat regenerating step (14) is performed under isenthalpic conditions to

Abstract: A rotary engine comprising an engine block that is movable in rotation about an axle, said engine block including at least one blind cylinder mounted on a casing. Said blind cylinders are closed by respective movable pistons defining sealed chambers of variable volume inside the cylinders. Each piston is connected to a crank mechanism secured to the stub axle of the engine block. The variable-volume sealed chamber of each piston contains a fluid suitable for expanding under the effect of a rise in temperature, the engine further including heater means for raising the temperature of the fluid present in said chamber.

Abstract: A closed cycle heat transfer device comprising a boiler (10) and a condenser (13), the condenser being used to recover useful heat by latent heat evaporation. A circuit defined by the boiler (10), condenser (13) and ducts (12, 15) is to be liquid-filled at a pressure just above atmospheric pressure. An expansion device (16) maintains the working pressure in the circuit but will receive excess condensate in a liquid phase to compensate for expansion of the working fluid vapor which passes from the boiler (10) to the condenser (13). The expansion chamber contains a movable or flexible member which, when working liquid is received in the chamber, is displaced to compress a gas in the chamber.

Abstract: A solar thermal powered aircraft powered by heat energy from the sun. A Rankine-Brayton hybrid cycle heat engine is carried by the aircraft body for producing power for a propulsion mechanism, such as a propeller or other mechanism for enabling sustained free flight. The Rankine-Brayton engine has a thermal battery, preferably containing a lithium-hydride and lithium mixture, operably connected to it so that heat is supplied from the thermal battery to a working fluid. A solar concentrator, such as reflective parabolic trough, is movably connected to an optically transparent section of the aircraft body for receiving and concentrating solar energy from within the aircraft. Concentrated solar energy is collected by a heat collection and transport conduit, and heat transported to the thermal battery. A solar tracker includes a heliostat for determining optimal alignment with the sun, and a drive motor actuating the solar concentrator into optimal alignment with the sun based on a determination by the heliostat.

Abstract: An apparatus and a method, for converting fluid heat energy to motive force by the heating and pressurization of air, and for storing and delivering motive force to motive force users, which includes at least one air pressurizer. The air pressurizer facilitates the transfer of heat energy contained in a hot fluid to air confined within the air pressurizer, thus pressurizing the air to provide motive force.

Abstract: A process of generating power utilizing a low level heat from a raw syngas produced in a quench gasifier is disclosed. The process includes a first stage that includes: producing raw syngas at the quench gasifier, making 150 psi saturated steam from the produced raw syngas, superheating the saturated steam, and using the superheated saturated steam in a low pressure steam turbine to generate power. The process includes a second stage that includes: providing the raw syngas and a process condensate stream to a thermal fluid vaporizer to vaporize an organic thermal fluid, and using the vaporized organic thermal fluid in an expander turbine to generate power via an organic Rankine cycle.

Abstract: A compressed air energy storage system including a compressor adapted to receive a process gas and output a compressed process gas. A heat transfer unit may be coupled to the compressor and adapted to receive the compressed process gas and a heat transfer medium and to output a cooled process gas and a heated heat transfer medium. A compressed gas storage unit may be coupled to the heat transfer unit and adapted to receive and store the cooled process gas. A waste heat recovery unit may be coupled to the heat transfer unit and adapted to receive the heated heat transfer medium.

Abstract: A waste heat recovery system, method and device executes a thermodynamic cycle using a working fluid in a working fluid circuit which has a high pressure side and a low pressure side.

Abstract: An engine/heat pump is shown. Most of its parts rotate around the same central axis. It comprises two doubly connected chambers. Blades in each chamber substantially rotate with the chamber and may be firmly attached to the walls of the chamber, thus forming a modified centrifugal pump with axial input and discharge. An expandable fluid is rotated outward by one of the pumps and then heat is added for an engine or removed for a heat pump as the fluid is being sent to the outer part of the second pump. The fluid travels toward the center of the second pump, thus impelling the pump in the rotation direction. Then heat is removed for an engine or added for a heat pump as the fluid leaves the second pump and travels back to the first pump near the center of rotation. Rotation energy of the fluid is typically much larger than the circulation energy. A modified centrifugal pump with axial discharge having a casing rotating with the blades is also claimed.

Abstract: A switchable solar heating device for a gas turbine with a compressor, having a valve for electively bypassing a solar heater which is arranged between a compressor stage and a turbine stage of the gas turbine. The valve is constructed as a 4-way valve with a compressor port that can be connected to the compressor stage, a turbine port that can be connected to the turbine stage, a solar input port that can be connected to an input of the solar heater, and a solar output port that can be connected to an output of the solar heater.

Abstract: High temperature energy can be provided using a containment vessel, a heat retention matrix contained within the containment vessel, a volume of a working fluid contained within the containment vessel and in contact with the heat retention matrix, and, optionally, a reactive compound removal system that removes reactive compounds from the working fluid. The heat retention matrix can optionally include an allotropic form of carbon. The working fluid can optionally include nitrogen gas and one or more noble gases. Related systems, methods, articles of manufacture, and the like are also described.

Abstract: A power plant including an apparatus for regasification of liquefied natural gas (LNG) is provided. The apparatus includes a compressor configured to pressurize a working fluid and a heat recovery system configured to provide heat to a working fluid. A turbine is configured to generate work utilizing the heated working fluid. One or more heat exchangers are configured to transfer heat from the working fluid to a first stage liquefied natural gas at a first pressure and at least one of a second stage liquefied natural gas at a second pressure, and a compressed working fluid.

Abstract: Various embodiments of a converter for use in a combustion engine having a discharge conduit for discharging exhaust combustion gases are disclosed. In one exemplary embodiment, the converter may include a heating chamber being in thermal contact with the discharge conduit and defining a hydraulic channel through which a fluid passes. The converter may also include an inlet port disposed in the heating chamber for receiving the fluid into the heating chamber, and an outlet port disposed in the heating chamber for discharging the fluid from the heating chamber. The heat energy from the exhaust combustion gases is transferred to the fluid while the fluid passes through the hydraulic channel.

Abstract: Provided is a concentrated solar power gas turbine that enables efficient operation to allow a reduction in capacity of the start-up driving source used for compensating for the shortage of solar heat quantity at the start-up/acceleration. The concentrated solar power gas turbine (GT1) includes a compressor (1) for taking in air and increasing the pressure thereof, the compressor (1) being provided with a start-up driving source for start-up/acceleration; a solar central receiver (2) for heating the high-pressure air, the pressure of which has been increased by the compressor (1), by the heat of sunlight collected by a heliostat to increase the temperature thereof; and a turbine (3) for converting thermal energy possessed by the high-temperature/high-pressure air to mechanical energy, wherein the fluid flow in the solar central receiver (2) is shut off to store heat in the period from the shutdown of the turbine (3) to the start-up thereof.

Abstract: The invention relates to a device for the conversion of heat energy into another energy form provided with at least one heat input and pressure reservoir module, each comprising a heat-input transmitting device and a pressure reservoir, whereby said device and pressure reservoir are connected to each other for the exchange of fluid and an energy conversion device, connected to the pressure reservoir of the heat input and pressure reservoir module for the exchange of fluid, by means of which the energy built up in the form of fluid pressure in the heat input and pressure reservoir module may be converted into said other energy form.

Abstract: Heat transfer pipes uniformly heat a compressible working fluid passing there through with a simplified supporting structure and reduced manufacturing costs. A solar central receiver (3) on top of a tower on the ground includes heat transfer pipes (16) arranged in the south-north direction; and a casing (14) accommodating the pipes (16) and has a solar radiation inlet (15) through which sunlight reflected by heliostats on the ground is transmitted to the lower surface side of the pipes (16). The pipes (16) are at equal intervals on a solar radiation receiving surface (11) parallel to a heliostat field on which the collectors are, or inclined with respect to the heliostat field on which the collectors are, and the diameters of the pipes (16) are substantially inversely proportional to the shortest distance from the inlet (15) to the central axes of the respective pipes (16) in the longitudinal direction.

Abstract: The present invention is directed to power generation systems and methods for converting naturally occurring moist air into power and water, enabling generation of power without carbon combustion and without the release of green-house gasses which usually accompany thermodynamic power generation. According to one embodiment, a compressor module is used to greatly compress enriched water vapor drawn from the surrounding moist air. The compressed water vapor is then condensed into output water by a working fluid, while the heated working fluid is used in a Rankine-cycle power generation loop to turn a turbine and thereby create transmittable electrical power.

Abstract: An apparatus and method for converting a differential in thermal energy between a first thermal source having a thermal conducting fluid and a second thermal source having a thermal conducting fluid is provided. The apparatus employs a first vessel and a second vessel. Each of the vessels contain a gas under pressure The vessels contain heat exchanging coils that are connected to the thermal sources by fluid lines. A plurality of cooperating valves regulate the flow of the thermal conducting fluid from the first and second thermal sources to the first and second vessels. The valves alternate between first and second operating positions. In the first position, the valves permit a flow of thermal conducting fluid from the first thermal source to the first vessel and from the second thermal source to the second vessel and prevent a flow of thermal conducting fluid from the first thermal source to the second vessel and from the second thermal source to the first vessel.

Abstract: A system is provided for separating carbon dioxide emitted in exhaust gas from nitrogen gas. A compressor may be used for compressing the emitted exhaust gas and a heat exchanger may be used for cooling the compressed exhaust gas to liquid carbon dioxide temperatures. The liquid carbon dioxide may be separated from the compressed nitrogen gas and stored. A turbine may use the compressed nitrogen gas to drive the compressor, while further cooling the compressed nitrogen to cryo-temperatures. Heat exchangers may be used for transferring heat energy from emitted exhaust and the compressed exhaust to the cold compressed nitrogen, thus, conserving energy of the system.

Abstract: A high-efficiency heat cycle system including a compressor, a first turbine, first and second heat exchangers 7 and 8, a first pump, and an expander, and a composite heat cycle power generator using the high-efficiency heat cycle system. Working gas Fg compressed in the compressor (C) drives a first turbine (S) and is thereafter cooled by passing through a heat dissipating side of a first heat exchanger (7) and then raised in pressure by a first pump (P) to form high-pressure working liquid Fe, the high-pressure working liquid is expanded and evaporated in an expander (K) to form working gas Fg, said working gas Fg is heated by passing through a heat receiving side 82 of the second heat exchanger before being introduced into the compressor C. A heat dissipating side 81 of the second heat exchanger comprises a heat dissipating portion of a refrigerating machine or a heat dissipating portion for waste heat from a heating machine.

Abstract: An energy regeneration system comprises a heat pump, a bioreactor, a combustor, and a temperature difference electricity generation device. The heat pump is provided for thermally regulating the bioreactor and can be used for air-condition, dehumidification, refrigeration, chilling, heating and/or supplying hot water for bath. The bioreactor accommodates an organic material. The organic material is converted into a biomass fuel and other materials by microbial action. The chemical energy of the biomass fuel is converted into a heat energy by the combustor for actuating the temperature difference electricity generation device, thereby generating electrical energy.

Abstract: A recuperator includes a heating gas duct; an inlet manifold; a discharge manifold; and a once-through heating area disposed in the heating-gas duct through which a heating gas flow is conducted. The once-through heating area is formed from a plurality of first single-row header-and-tube assemblies and a plurality of second single-row header-and-tube assemblies. Each of the plurality of first single-row header-and-tube assemblies including a plurality of first heat exchanger generator tubes is connected in parallel for a through flow of a flow medium therethrough and further includes an inlet header connected to the inlet manifold. Each of the plurality of second single-row header-and-tube assemblies including a plurality of second heat exchanger generator tubes is connected in parallel for a through flow of the flow medium therethrough from respective first heat exchanger generator tubes, and further includes a discharge header connected to the discharge manifold.

Abstract: In various embodiments, systems for providing a constant electrical output from a compressed gas energy storage and recovery system include a hydraulic-pneumatic energy storage and recovery system configured to provide a varying pressure profile at least at one outlet, a hydraulic motor-pump in fluid communication with the outlet, and a control system for enabling the constant electrical output by controlling at least one of pressure, piston position, power, flow rate, torque, RPM, current, voltage, frequency, or displacement per revolution.

Abstract: A method and apparatus for extracting useful energy from biomass fuels as part of a hybrid electricity generating thermal power plant, utilising both a primary heat source, such as coal, gas, oil or nuclear power, and a secondary heat source in the form of biomass, whereby the biomass is oxidised in aqueous solution in a supercritical water oxidation (SCWO) process utilising energy from the primary heat source to heat and compress a feed stream of water to a temperature and pressure at or beyond its critical point.

Abstract: In various embodiments, pneumatic cylinder assemblies are coupled in series pneumatically, thereby reducing a range of force produced by or acting on the pneumatic cylinder assemblies during expansion or compression of a gas.

Abstract: An adiabatic compressed air energy storage (ACAES) system includes a compressor system, an air storage unit, and a turbine system. The ACAES system further includes a thermal energy storage (TES) system that includes a container, a plurality of heat exchangers, a liquid TES medium conduit system fluidly coupling the container to the plurality of heat exchangers, and a liquid TES medium stored within the container. The TES system also includes a plurality of pumps coupled to the liquid TES medium conduit system and configured to transport the liquid TES medium between the plurality of heat exchangers and the container, and a thermal separation system positioned within the container configured to thermally isolate a first portion of the liquid TES medium at a lower temperature from a second portion of the liquid TES medium at a higher temperature.

Abstract: A system and method for transmitting thermal energy. The system includes an intake for introducing air at a first temperature; an exhaust for exhausting the air, the exhaust being provided at a higher vertical elevation than intake; and a thermal energy source provided at second temperature higher than the first temperature, the waste thermal energy source being provided between the intake and the exhaust. The air introduced via the intake, passes the thermal energy source, and is exhausted via the exhaust due to a difference in elevation between the intake and the exhaust. The thermal energy source can be a waste thermal industrial energy source. The system can include a first ambient energy chamber configured to pass the air through the thermal energy source and an insulated, and a second ambient energy chamber provided between the ambient energy chamber and the exhaust, wherein the second ambient energy chamber is a made of a slow-loading thermal material.

Abstract: An air aspirated hybrid heat pump and heat engine system (20) for selectively heating and cooling a space (22) having an flow path (24) including a compressor (76), a heat exchanger (32), an expander (78), and a generator (68). A combustion chamber (62) is in the flow path (24) for combusting a fuel in the air during a high heating mode. The heat exchanger (32) dissipates the heat from the air, and the expander (78) depressurizes the air while powering the generator (68). Also included is a positive displacement rotating vane-type device (36) having a stator housing (38) extending between longitudinal ends (40). A compression chamber inlet (52) and an expansion chamber outlet (58) are located on opposite longitudinal ends (40) of the stator housing (38) to be in simultaneous communication with the same chamber (48, 50)). A fluid enters the device through the compression chamber inlet (52) and pushes fluid out of the expansion chamber outlet (58).

Abstract: A liquid metal fueled Brayton cycle power system with a direct contact heat exchanger. In this invention, a compressor compresses the working gas. A regenerator preheats the compressed working gas and passes the working gas to a reactor/storage tank with liquid metal fuel stored therein. An oxidant is injected into the reactor/storage tank to react with the liquid metal fuel. The compressed working gas bubbles through the liquid metal fuel in the reactor/storage tank and is heated by direct contact with the fuel-oxidant mixture. A turbine expands the heated working gas and thereby withdraws power from the system. The spent working gas exits to the regenerator where it warms the compressed gas. A cooler reduces the working gas temperature and recirculates the gas to the compressor.

Abstract: A closed cycle Brayton direct contact reactor/storage tank uses a chemical scrubber to assist in removing metal vapors from the working fluid. The direct contact reactor/storage tank operates by bubbling an inert gas through liquid metal fuel. The inert gas picks up metal vapors from the fuel. The chemical scrubber is comprised of a reducible material contained within a filter at the top of the reactor/storage tank. The reducible material on reacting with the metal vapor forms components that are solids at the operating temperature and pressure, thereby preventing metal vapor from circulating throughout the system as part of the working fluid and causing damage to system components.