Patent classifications
F02C6/00
High pressure liquid air power and storage
Apparatus, systems, and methods store energy by liquefying a gas such as air, for example, and then recover the energy by regasifying the liquid and combusting or otherwise reacting the gas with a fuel to drive a heat engine. The process of liquefying the gas may be powered with electric power from the grid, for example, and the heat engine may be used to generate electricity. Hence, in effect these apparatus, systems, and methods may provide for storing electric power from the grid and then subsequently delivering it back to the grid.
Resonance vibration control method and system
A bearing arrangement includes a shaft, at least one contact bearing and at least one non-contact bearing and a controller. The controller is configured to control a magnitude of a restoring force applied to the shaft by the non-contact bearing in accordance with a sensed parameter such that a stiffness of the shaft is modified such that one or more resonance frequencies of the shaft are moved away from one or more external forcing frequencies.
Resonance vibration control method and system
A bearing arrangement includes a shaft, at least one contact bearing and at least one non-contact bearing and a controller. The controller is configured to control a magnitude of a restoring force applied to the shaft by the non-contact bearing in accordance with a sensed parameter such that a stiffness of the shaft is modified such that one or more resonance frequencies of the shaft are moved away from one or more external forcing frequencies.
Gas turbine power generation device
A gas turbine power generation device includes: an inlet pipe (1), a compressor (2), an air storage compartment (3), a compressor rotor (4), a compressor gear shift (6), a compressor exhaust pipeline (8), a combustion chamber intake pipeline (10), a combustion chamber intake cone (11), a combustion chamber pneumatic valve (14), a spark plug (19), a combustion chamber (21), a Tesla turbine (22), a gas collection compartment (27), an outlet pipe (28), a turbine rotor (30), a generator gear shift (32) and a generator (33).
Gas turbine power generation device
A gas turbine power generation device includes: an inlet pipe (1), a compressor (2), an air storage compartment (3), a compressor rotor (4), a compressor gear shift (6), a compressor exhaust pipeline (8), a combustion chamber intake pipeline (10), a combustion chamber intake cone (11), a combustion chamber pneumatic valve (14), a spark plug (19), a combustion chamber (21), a Tesla turbine (22), a gas collection compartment (27), an outlet pipe (28), a turbine rotor (30), a generator gear shift (32) and a generator (33).
Combined cycle power plant with flue gas recirculation
An exemplary method for the operation of a CCPP with flue gas recirculation to reduce NOx emissions and/or to increase the CO2 concentration in the flue gases to facilitate CO2 capture from the flue gases as well as a plant designed to operate is disclosed. To allow a high flue gas recirculation ration (rFRG) an imposed combustion inhomogeneity ratio (ri) is used for flame stabilization. The imposed combustion inhomogeneity ratio (ri) is controlled as function of the flue gas recirculation rate (rFRG) and/or combustion pressure. Oxygen or oxygen enriched air to the gas turbine inlet gases or to the combustor is admixed to enhance operatability.
Systems and methods for hybrid electric turbine engines
A hybrid electric gas turbine engine includes a fan section having a fan, a turbine section having a turbine drivably connected to the fan through a main shaft that extends along a central longitudinal axis, a gas generating core extending along a first axis that is radially offset from the central longitudinal axis, a first electric motor drivably connected to the main shaft, wherein the electric motor is colinear with the main shaft, and an electric compressor extending along a second axis that is radially offset from the central longitudinal axis, the electric compressor in fluid communication with the second turbine section.
Power generation system having compressor creating excess air flow and turbo-expander to increase turbine exhaust gas mass flow
A power generation system may include: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied. The first integral compressor has a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A turbo-expander may be operatively coupled to the second gas turbine system. Control valves may control flow of the excess air flow from the first gas turbine system to at least one of the second gas turbine system and the turbo-expander, and flow of a discharge of the turbo-expander to an exhaust of at least one of the first turbine component and the second turbine component.
Power generation system having compressor creating excess air flow and turbo-expander to increase turbine exhaust gas mass flow
A power generation system may include: a first gas turbine system including a first turbine component, a first integral compressor and a first combustor to which air from the first integral compressor and fuel are supplied. The first integral compressor has a flow capacity greater than an intake capacity of the first combustor and/or the first turbine component, creating an excess air flow. A second gas turbine system may include similar components to the first except but without excess capacity in its compressor. A turbo-expander may be operatively coupled to the second gas turbine system. Control valves may control flow of the excess air flow from the first gas turbine system to at least one of the second gas turbine system and the turbo-expander, and flow of a discharge of the turbo-expander to an exhaust of at least one of the first turbine component and the second turbine component.
Fracturing device, firefighting method thereof and computer readable storage medium
A fracturing device, a firefighting method thereof, and a computer readable storage medium are disclosed. The fracturing device includes a power unit, the power unit includes a muffling compartment, a turbine engine, and a firefighting system; the firefighting system includes a firefighting material generator, at least one firefighting sprayer and at least one firefighting detector, the at least one firefighting sprayer and the at least one firefighting detector are located in the muffling compartment, each of the at least one firefighting sprayer is connected with the firefighting material generator and configured to spray out firefighting material generated by the firefighting material generator.