Abstract: A compact rotating separator apparatus to which a fluid stream containing gas, two liquids of different density, and solids is supplied via nozzles or exhaust from a process component; and which employs high centrifugal forces to produce pure streams of the gas, each of the liquids, and a waste stream containing the solids. The energy in the fluid stream is converted to shaft power in the rotating separator apparatus and can be used to generate power. Oil, gas, water and solids from a production well can be directly separated into the constituent streams while producing useful power.

Abstract: A compact rotating separator apparatus to which a fluid stream containing gas, two liquids of different density, and solids is supplied via nozzles or exhaust from a process component; and which employs high centrifugal forces to produce pure streams of the gas, each of the liquids, and a waste stream containing the solids. The energy in the fluid stream is converted to shaft power in the rotating separator apparatus and can be used to generate power. Oil, gas, water and solids from a production well can be directly separated into the constituent streams while producing useful power.

Abstract: A turbine is operatively connected to load structure, to transmit rotary drive thereto, with two-phase flow nozzle receiving pressurized flow to rotate the turbine, the nozzle structure configured to expand flow consisting of two or more of the following phases: i) gas ii) liquid iii) gas and liquid mixture iv) supercritical gas and liquid mixture, and with efficient conversion of enthalpy.

Abstract: A multi-component apparatus characterized as performing a two-phase thermodynamic cycle, for conversion of heat energy to useful power comprises: fluid means consisting to two or more chemical components to absorb heat energy, the fluid means providing an increasing temperature and increasing fraction of gas phase as increasing amounts of heat are absorbed, expander means operating to convert the enthalpy in a received mixture of gas and liquid, formed in said fluid means, as a result of the said heat energy absorbed by the fluid means, to mechanical, shaft power, heat exchanger means operating to transfer the heat energy to be absorbed by the fluid means, condenser means operating to reject the unconverted enthalpy, by the expander means, in the fluid means, thereby condensing any gas to convert the fluid means to liquid, and pump means operating to pressurize liquid fluid means leaving the condenser means, in order to return the fluid means to the heat exchanger means, closing the thermodynamic cycle.

Abstract: Variable phase turbine apparatus comprising, in combination a rotatably driven load structure, defining an axis, confinement means forming a fluid flow passage extending generally axially and adjacent said load structure, a turbine operatively connected to said load structure, to transmit rotary drive thereto, two-phase flow nozzle means receiving pressurized flow via said passage, and directing flow of fluid from said passage, expanded in the nozzle means, at the turbine to rotate the turbine, the nozzle means configured to expand flow consisting of two or more of the following phases: v) gas vi) liquid vii) gas and liquid mixture viii) supercritical gas and liquid mixture, and with efficient conversion of enthalpy.

Abstract: A turbine, including a rotor on a shaft, and having in combination stationary nozzles discharging steam at a first pressure or pressures thereby producing impulse forces on the rotor; internal passages in the rotor producing a pressure head increase in the discharged steam, while simultaneously accelerating the steam, the steam discharged to a second pressure lower than the first pressure, producing reaction forces on the rotor; seal means between the stationary nozzles and the rotor, maintaining the pressure difference between the first pressure and the second pressure while minimizing steam leakage past the internal passages, turbine operations producing shaft power.

Abstract: An axial flow turbine configured to accept different nozzles which are respectively compatible with different fluids (gas, liquid or mixture thereof). The turbine is compatible with different rotating loads, which can be cooled or lubricated using liquid derived from the fluid.

Abstract: A high temperature heat pump comprising a low temperature heat exchanger to produce vapor of a first fluid from heat transferred from a second fluid to a mixture of liquid and vapor of the first fluid; a compressor to increase the pressure and temperature of the produced vapor; a high temperature heat exchanger to heat the second fluid to useful, high temperatures from the condensation of the first fluid; and an expander to lower the pressure and temperature of the first fluid producing a mixture of vapor and liquid.

Abstract: A waste heat recovery system comprising ducting to which hot gas is communicated, means to supply lower temperature diluent gas to the ducting, to mix with the hot gas, and produce a reduced temperature mixed gas stream, a vaporizer in communication with the ducting, to receive the stream and to transfer heat from the stream to a working fluid in the vaporizer to vaporize said fluid, and a blower operating to displace the stream through the vaporizer.

Abstract: A gas centrifuge operating to separate gases of differing chemical composition and molecular weight by a centrifugal force field. Such a centrifuge is operable to separate methane and carbon dioxide, and to produce torque, and a cascade of such centrifuges is operable to concentrate produced streams of carbon dioxide and methane, and to produce torque. A compact centrifugal gas processing system incorporating the gas centrifuge with other centrifugal components, is also provided.

Abstract: A hot exhaust heat recovery system comprising, in combination a chamber having inlet and outlet porting for flow through of hot exhaust gas, in the chamber interior, separate heat exchanger structures in separate sequential segments said chamber interior, to receive heat transferred from said exhaust gas, said structures receiving pressurized liquid for flow in different paths there-through, to develop vapor streams at different pressures and temperatures without use of boiler drums, the structures having outlets to communicate with a vapor driven turbine or turbines having inlet ports at different inlet fluid pressure zones.

Abstract: A process employing a rotary axial turbine, and a nozzle, that includes providing a working fluid expansible from a characteristic supercritical region into the wet region, expanding the fluid from said supercritical region into the wet region via the nozzle and turbine blades, and providing an output shaft driven by the turbine.

Abstract: A turbine including a rotor on a shaft and comprising in combination stationary nozzles discharging fluid, thereby producing impulse forces on a rotor; internal passages in the rotor producing compression of the fluid; nozzles on the rotor discharging fluid to a pressure lower than the discharge pressure of the stationary nozzles, thereby producing reaction forces on the rotor whereby shaft power is produced.

Abstract: A multistage two-phase turbine having multiple stages to receive fluid, each stage having an inlet and outlet comprising nozzles at the inlet to each stage to accelerate the fluid that consists of a mixture of gas and liquid, to form two-phase jets; a rotating separator structure to receive and separate the two-phase jets into gas streams and liquid stream in each stage; the turbine having a rotating output shaft, and there being structure to convert the kinetic energy of the liquid streams into shaft power; structure to remove the separated liquid from at least one stage and transfer it to nozzles at the next stage; structure to remove the separated liquid from the last stage and transfer it to primary outlet structure; and structure to remove the separated gas from at least one stage and transfer it to a secondary outlet structure.

Abstract: A multistage two-phase turbine having multiple stages to receive fluid, each stage having an inlet and outlet comprising nozzles at the inlet to each stage to accelerate the fluid that consists of a mixture of gas and liquid, to form two-phase jets; a rotating separator structure to receive and separate the two-phase jets into gas streams and liquid stream in each stage; the turbine having a rotating output shaft, and there being structure to convert the kinetic energy of the liquid streams into shaft power; structure to remove the separated liquid from at least one stage and transfer it to nozzles at the next stage; structure to remove the separated liquid from the last stage and transfer it to primary outlet structure; and structure to remove the separated gas from at least one stage and transfer it to a secondary outlet structure.

Abstract: The method of operating rotating separator apparatus, to which fluid, including gas and liquids is supplied in a fluid jet via a nozzle, which includes separating the liquids from the gas in the stream, at a first zone within the rotating apparatus, and separating the liquids into liquids of differing density at a second zone within the apparatus. The separated liquids are removed via two open weirs which isolate the liquids in the separating zones from the shear forces from scoops within the weir passages. Longitudinal ribs may be provided for structural support, coalescence promotion and fluid recirculation inhibition.

Abstract: A multistage two-phase turbine having multiple stages to receive fluid, each stage having an inlet and outlet comprising nozzles at the inlet to each stage to accelerate the fluid that consists of a mixture of gas and liquid, to form two-phase jets; a rotating separator structure to receive and separate the two-phase jets into gas streams and liquid stream in each stage; the turbine having a rotating output shaft, and there being structure to convert the kinetic energy of the liquid streams into shaft power; structure to remove the separated liquid from at least one stage and transfer it to nozzles at the next stage; structure to remove the separated liquid from the last stage and transfer it to primary outlet structure; and structure to remove the separated gas from at least one stage and transfer it to a secondary outlet structure.

Abstract: The method of operating rotating separator apparatus, to which fluid, including gas and liquids is supplied in a fluid jet at via a nozzle, which includes separating the liquids from the gas in the stream, at a first zone within the rotating apparatus, and separating the liquids into liquids of differing density at a second zone within the apparatus.

Abstract: A multistage two-phase turbine having multiple stages to receive fluid, each stage having an inlet and outlet including nozzles at the inlet to each stage to accelerate the fluid that consists of a mixture of gas and liquid, to form two-phase jets; a rotating separator structure to receive and separate the two-phase jets into gas streams and liquid streams in each stage; the turbine having a rotating output shaft, and there being structure to convert the kinetic energy of the liquid streams into shaft power; structure to remove the separated liquid from at least one stage and transfer it to nozzles at the next stage; structure to remove the separated liquid from the last stage and transfer it to primary outlet structure; and structure to remove the separated gas from at least one stage and transfer it to a secondary outlet structure.

Abstract: A rotary turbine apparatus which includes a separator having a rotating cylindrical wall receiving a stream of liquid and gas for separating gas from liquid, the liquid collecting in a rotating ring on the wall, and comprising a scoop having an inlet immersed in the rotating liquid ring to receive liquid from the ring; and barrier structure located proximate the scoop inlet to block gas entry to the scoop.