Micro gas turbine systems and uses thereof
The present disclosure describes a micro gas turbine flameless heater, in which the heat is generated by burning fuel in a gas turbine engine, and the heater output air mixture is generated by transferring the heat in the gas turbine exhaust to the cold air drawn from the ambient environment. The present disclosure also describes component geometries and system layout for a gas turbine power generation unit that is designed for simple assembly, disassembly, and component replacement. The present disclosure also allows for quick removal of the rotating components of the gas turbine engine in order to reduce assembly and maintenance time. Furthermore, the present disclosure describes features that help to maintain safe operating temperatures for the bearings and structures of the gas turbine engine power turbine. Lastly, the present disclosure describes features of a fuel capture system that allow the injection of wellhead gas, which typically is a mixture of gaseous and liquid fuels, into the combustion chamber, and also describes methods of incorporating afterburners in the gas turbine engine, such that the gas turbine engine system can use wellhead gas to power equipment and reduce emissions from flaring in oil and gas applications.
1. A method of operating a gas turbine heater, wherein the gas turbine heater comprises a gas turbine comprising i) an air starter; ii) a compressor; iii) a turbine; and iv) a combustion chamber configured to receive compressed air for combustion from the compressor, to receive a fuel from a source, to burn the fuel to produce a combustion gas, and to supply the combustion gas to the turbine, wherein the gas turbine is configured to heat an external environment directly or indirectly using the combustion gas exhausted from the turbine, the method comprising:
operating a fan to pump air through an enclosure of the gas turbine heater such that the air passes from an ambient air inlet of the enclosure to an outlet of the enclosure,
terminating fluid communication between the ambient air and the compressor,
then establishing fluid communication between the air starter and the compressor of the gas turbine heater before operating the air starter, such that substantially all of the air from the air starter flows into the compressor during startup,
operating the air starter to pump air into the compressor,
delivering the fuel into the combustion chamber in an amount that is sufficient for ignition,
igniting an air fuel mixture to begin combustion,
increasing a flow rate of fuel into the combustion chamber until the gas turbine engine idles,
establishing fluid communication between ambient air and the compressor such that the compressor draws in air from the ambient air,
turning off the air starter,
increasing the amount of fuel into the combustion chamber to increase the amount of heat produced by the gas turbine heater.
2. The method of claim 1 , wherein the fuel is a gaseous fuel.