F02C3/28

POWER MODULES WITH BLOW DOWN FUEL AND PROPELLANT DELIVERY SYSTEMS
20200325822 · 2020-10-15 ·

A power module includes a turbine, a first pressure vessel operatively connected to the turbine, and a second pressure vessel. The second pressure vessel is in fluid communication with the first pressure vessel and is fluidly connected to the first pressure vessel in series to drive a fuel or a propellant charge disposed within the first pressure vessel to a gas generator for generating electrical power using the turbine. Unmanned Aerial vehicles and methods or generating electrical power are also described.

POWER MODULES WITH BLOW DOWN FUEL AND PROPELLANT DELIVERY SYSTEMS
20200325822 · 2020-10-15 ·

A power module includes a turbine, a first pressure vessel operatively connected to the turbine, and a second pressure vessel. The second pressure vessel is in fluid communication with the first pressure vessel and is fluidly connected to the first pressure vessel in series to drive a fuel or a propellant charge disposed within the first pressure vessel to a gas generator for generating electrical power using the turbine. Unmanned Aerial vehicles and methods or generating electrical power are also described.

Turbine Powered Electricity Generation
20200277895 · 2020-09-03 ·

A process is provided for separating syngas fuel into a CO-rich stream for feeding to oxyfuel combustor means of CO.sub.2 turbine means and a H.sub.2-rich stream for feeding to air-fuel gas turbine means for generating power provides opportunity to realize operating and equipment advantages.

Turbine Powered Electricity Generation
20200277895 · 2020-09-03 ·

A process is provided for separating syngas fuel into a CO-rich stream for feeding to oxyfuel combustor means of CO.sub.2 turbine means and a H.sub.2-rich stream for feeding to air-fuel gas turbine means for generating power provides opportunity to realize operating and equipment advantages.

FILTER BACKWASHING UNIT, CHAR RECOVERY UNIT, METHOD OF FILTER BACKWASHING, AND INTEGRATED GASIFICATION COMBINED CYCLE

A filter backwashing unit is disposed in a path in which process gas flows to remove at least a part of trapped dust included in a process gas by backwashing an element of a filter device that traps the dust when a process gas passes. The filter backwashing unit includes a gas injection device disposed downstream of the element in a flow direction of a process gas to inject backwashing gas toward the element from downstream; a parameter detection device configured to detect a parameter used for determination of a state of dust adhering to the element; and a control device configured to estimate a thickness of dust deposited on a surface of the element upstream of a process gas based on a result of the detection, and determine an interval at which the element is backwashed based on the estimated thickness of the dust.

FILTER BACKWASHING UNIT, CHAR RECOVERY UNIT, METHOD OF FILTER BACKWASHING, AND INTEGRATED GASIFICATION COMBINED CYCLE

A filter backwashing unit is disposed in a path in which process gas flows to remove at least a part of trapped dust included in a process gas by backwashing an element of a filter device that traps the dust when a process gas passes. The filter backwashing unit includes a gas injection device disposed downstream of the element in a flow direction of a process gas to inject backwashing gas toward the element from downstream; a parameter detection device configured to detect a parameter used for determination of a state of dust adhering to the element; and a control device configured to estimate a thickness of dust deposited on a surface of the element upstream of a process gas based on a result of the detection, and determine an interval at which the element is backwashed based on the estimated thickness of the dust.

Gas turbine system

A gas turbine system has a source of ammonia and a source of an oxygen-containing gas, a first combustion chamber connected to receive ammonia, a hydrogen-rich gas stream and oxygen-containing gas, a turbine connected to receive an exhaust gas stream from the first combustion chamber; and a second combustion chamber connected to receive an exhaust gas from the turbine, ammonia and a hydrogen-rich gas stream.

Gas turbine system

A gas turbine system has a source of ammonia and a source of an oxygen-containing gas, a first combustion chamber connected to receive ammonia, a hydrogen-rich gas stream and oxygen-containing gas, a turbine connected to receive an exhaust gas stream from the first combustion chamber; and a second combustion chamber connected to receive an exhaust gas from the turbine, ammonia and a hydrogen-rich gas stream.

Control device and control method using fuel supply acceleration command value

A control device for a power generation system whereby power is generated by a first power source that operates by burning a fuel. The control device identifies, on the basis of a pressure difference in a prior-stage mechanism that supplies the fuel to the first power source, a fuel capacity that compensates for the pressure difference in the prior-stage mechanism. The pressure difference is the difference between a pressure set for the fuel before a load change in the prior-stage mechanism and a pressure set for the fuel after the load change in the prior-stage mechanism. The control device calculates a fuel supply command value, which is a command value for adjusting the amount of fuel supplied to a fuel supply device that supplies the fuel to the first power source, and is output to the fuel supply device using a fuel supply acceleration command value.

SYSTEM AND METHOD FOR POWER PRODUCTION INCLUDING METHANATION
20200224587 · 2020-07-16 ·

The present disclosure relates to a power production system that is adapted to achieve high efficiency power production with carbon capture when using a solid or liquid hydrocarbon or carbonaceous fuel. More particularly, the solid or liquid fuel first is partially oxidized in a partial oxidation reactor that is configured to provide an output stream that is enriched in methane content. The resulting partially oxidized stream can be cooled, filtered, additionally cooled, and then directed to a combustor of a power production system as the combustion fuel. The partially oxidized stream is combined with a compressed recycle CO.sub.2 stream and oxygen. The combustion stream is expanded across a turbine to produce power and passed through a recuperator heat exchanger. The recycle CO.sub.2 stream is compressed and passed through the recuperator heat exchanger and optionally the POX heat exchanger in a manner useful to provide increased efficiency to the combined systems.