摘要:
Various embodiments of the present invention are operable to determine when to test an overspeed protection system of a powerplant machine (105, 145). As described herein, embodiments of the present invention may be applied to a wide variety of powerplant machines, each comprising a shaft (137). After determining that test of the overspeed protection system should be performed, embodiments of the present invention may allow for a variety of methods to test the overspeed protection system.
摘要:
A gasification power generation system provided with a carbon dioxide separation and recovery device (200) comprising: a carbon dioxide separation and recovery device (200) having: a shift reactor (5) to convert carbon monoxide contained in fuel gas into carbon dioxide; a carbon dioxide absorption tower (37) to produce fuel gas; and an absorption liquid recycling device (38) to recycle an absorption liquid; and a gasification power generation system having: a gas turbine device driven by burning the fuel gas; an exhaust heat recovery boiler (20) having a drum (30,31) to generate steam; and a steam turbine (23) driven by the steam generated by the drum (30,31); wherein an evaporator (6) to generate steam is disposed downstream of the shift reactor (5), a steam line to supply a steam mixer (4) disposed in a fuel gas line upstream of the shift reactor (5) with the heated steam generated by the evaporator (6) is provided, and the heated steam supplied through the steam line is allowed to flow from the steam mixer (4) into the shift reactor (5) as shift steam together with the fuel gas.
摘要:
The invention relates to a method for generating energy, in which an electropositive metal selected from the alkali metals, the alkaline earth metals, aluminium and zinc, as well as mixtures and/or alloys thereof, is atomised and/or sprayed and is combusted with a reaction gas comprising carbon dioxide and/or water, the reacted mixture of reaction gas and electropositive metal being mixed with water and/or an aqueous solution and/or suspension of a salt of said electropositive metal. The invention also relates to a device for carrying out said method.
摘要:
Solutions for clutching turbine wheels (6, 8) are disclosed. In one embodiment, an apparatus (22) includes: a turbine rotor shaft (4); a plurality of turbine wheels (6) affixed to the turbine rotor shaft (4); an independent turbine wheel (8) engagably attached to the turbine rotor shaft (4); and a clutch (10) operably connected to the turbine rotor shaft (4), the clutch (4) configured to couple and decouple the independent turbine wheel (8) from the turbine rotor shaft (4).
摘要:
A combined cycle power generating device in which the exhaust heat of the gas turbine reheats the steam discharged out of the high pressure chamber of the steam turbine so that the reheated steam is supplied to the intermediate-pressure chamber in order to increase the power output of the steam turbine, wherein the cooling steam that has cooled the gas turbine is supplied to the intermediate-pressure chamber via a cooling steam inlet different from the inlet of the reheat steam that is reheated by the exhaust heat of the gas turbine, so that the cooling steam is used for cooling purpose, the temperature of the cooling steam being higher than the temperature of the steam discharged out of the high pressure chamber.
摘要:
A method (300) for determining fuel splits includes monitoring (302) an airflow-related parameter of a gas turbine (100) and determining (304) first (212) and second reference values (214) for the airflow-related parameter based on a combustion reference temperature (CRT). The first reference value (212) is associated with a first load path (10) of the gas turbine (100) and the second reference value (214) is associated with a second load path (12) of the gas turbine (100). The method (300) also includes determining (310) first (252) and second fuel split commands (254) based on the combustion reference temperature (CRT). In addition, the method (300) includes determining a fuel split value (260) to be applied in association with a monitored value of the airflow-related parameter based at least in part on the reference values (212, 214) and the fuel split commands (252, 254) and applying the fuel split value (260) to regulate an amount of fuel supplied to one or more fuel circuits of the gas turbine (100).
摘要:
A fuel feed system (110) for use in a gasification system (50) including a gasifier (134) is provided. The fuel feed system (110) includes a feed preparation section (118) configured to grind a particulate fuel to a predetermined size and to adjust a moisture content within the particulate fuel, a pressurization and conveyance section (124) coupled in flow communication with the feed preparation section, the pressurization and conveyance section including at least one solids pump (340) configured to receive a flow of the particulate fuel at a first pressure and discharge the particulate fuel at a second pressure, a conduit (122) configured to channel the pressurized particulate fuel to the gasifier, and a slag additive section (152) configured to feed a slag mixture into the gasifier and substantially control a total water content of a quantity of feeds into the gasifier, and further control melting and flow characteristics of a quantity of particulate fuel ash within the gasification system.
摘要:
A method of operating an axial stage combustion system in a gas turbine engine (12) including an EGR system (14) that extracts a portion of exhaust gas produced by the gas turbine engine (12) to a second axial stage of a combustor (18). The extracted exhaust gas is provided at an elevated temperature to a group of injector nozzles (50) at the second axial stage (34) of the combustor (18). A secondary fuel supply line (34) extends to an inlet on each of the injector nozzles (50), and the fuel is mixed with the exhaust gas within the injector nozzles (50) and the mixture of fuel and exhaust gas is injected into the second axial stage (34) of the combustor (18).
摘要:
In one embodiment, a system includes a drive train starter system. The drive train starter system includes a generator mechanically coupled to a drive train of a gas turbine system and an exciter system electrically coupled to the generator and configured to provide a magnetic field. The drive train starter system additionally includes a load commutated inverter (LCI) electrically coupled to the generator and configured to provide electrical power to the generator and a controller communicatively coupled to the generator, the exciter system, and the LCI. The controller is configured to start up the drive train via the LCI and the generator up to less than a drive train operating speed, wherein the generator is converting electricity into mechanical motion; drive the drive train via a gas turbine up to the drive train operating speed; and to drive the drive train via the generator at the drive train operating speed.