Combined integrated waste heat recovery and inlet pressure boost system
The electrical power generation system including a micro-turbine alternator. The micro-turbine alternator including a combustor, at least one turbine configured to be driven by an exhaust from the combustor, at least one compressor operably connected to the combustor to provide a compressed airflow to the combustor, one or more shafts connecting the at least one turbine to the at least one compressor such that rotation of the at least one turbine drives rotation of the at least one compressor, and a recuperator configured to transfer heat from the exhaust exiting the at least one turbine to the compressed airflow from the at least one compressor entering the combustor.
1. An electrical power generation system, comprising:
a micro-turbine alternator, comprising:
a combustor;
at least one turbine configured to be driven by an exhaust from the combustor, including a first stage turbine; and a second stage turbine;
at least one compressor operably connected to the combustor to provide a compressed airflow to the combustor, including: a first stage compressor; a second stage compressor; and a third stage compressor
the turbines and compressors are oriented along a central longitudinal axis, and combustion products are exhausted from the second stage turbine through a turbine exit;
one or more shafts connecting the at least one turbine to the at least one compressor such that rotation of the at least one turbine drives rotation of the at least one compressor; and wherein at least one of the one or more shafts passes through the electric generator;
an electric generator disposed along the one or more shafts, between the first stage compressor and the second stage compressor measured along the central longitudinal axis A, such that electrical power is generated via rotation of the one or more shafts, wherein the electric generator is disposed along the one or more shafts between the first stage compressor and the second stage compressor; and
a recuperator configured to transfer heat from the exhaust exiting the at least one turbine to the compressed airflow from the at least one compressor entering the combustor;
a bottoming system located on the central longitudinal axis, comprising: a bottoming blower configured to deliver air to the at least one compressor; a bottoming drive shaft and a bottoming turbine located operably connected to the bottoming blower through the bottoming drive shaft, wherein the bottoming blower is configured to rotate when the bottoming turbine is rotated by the exhaust directed to it from the turbine exit via the recuperator; and the bottoming blower is configured to pull external airflow, through one or more air inlets in a frame of the system, into a bottoming compressor flow path C located between the first stage compressor and the bottoming system along the central longitudinal axis A.
2. The electrical power generation system of claim 1 , wherein the recuperator is configured to transfer heat from the exhaust exiting the at least one turbine to the compressed airflow from the third stage compressor entering the combustor.
3. The electrical power generation system of claim 1 , further comprising:
a thermal electric generator array comprising:
a hot side passageway configured to receive the exhaust from the recuperator;
a cold side passageway configured to transfer air to the at least one compressor;
a hot side heat transfer surface thermally connected to the hot side passageway;
a cold side heat transfer surface thermally connected to the cold side passageway; and
a thermo electric device interposed between the hot side heat transfer surface and the cold side heat transfer surface, the thermo electric device being configured to generate an electrical current based on a temperature difference between the cold side heat transfer surface and the hot side heat transfer surface.
4. An electrical power generation system, comprising:
a micro-turbine alternator, comprising:
a combustor;
at least one turbine configured to be driven by an exhaust from the combustor;
at least one compressor operably connected to the combustor to provide a compressed airflow to the combustor;
one or more shafts connecting the at least one turbine to the at least one compressor such that rotation of the at least one turbine drives rotation of the at least one compressor; and
a thermal electric generator array comprising:
a hot side passageway configured to receive the exhaust from the at least one turbine;
a cold side passageway configured to transfer air to the at least one compressor;
a hot side heat transfer surface thermally connected to the hot side passageway;
a cold side heat transfer surface thermally connected to the cold side passageway; and
a thermo electric device interposed between the hot side heat transfer surface and the cold side heat transfer surface, the thermo electric device being configured to generate an electrical current based on a temperature difference between the cold side heat transfer surface and the hot side heat transfer surface,
wherein the at least one compressor comprises:
a first stage compressor;
a second stage compressor; and
a third stage compressor,
wherein the cold side passageway configured to transfer air to the first stage compressor.
5. The electrical power generation system of claim 4 , wherein the at least one turbine comprises:
a first stage turbine; and
a second stage turbine, wherein the hot side passageway is configured to receive the exhaust from the second stage turbine.
6. The electrical power generation system of claim 4 , further comprising:
a bottoming system comprising:
a bottoming blower configured to deliver air to the at least one compressor;
a bottoming drive shaft; and
a bottoming turbine operably connected to the bottoming blower through the bottoming drive shaft, wherein the bottoming blower is configured to rotate when the bottoming turbine is rotated by the exhaust.
7. The electrical power generation system of claim 4 , further comprising:
an electric generator disposed along the one or more shafts such that electrical power is generated via rotation of the one or more shafts, wherein the electric generator is disposed along the one or more shafts between the first stage compressor and the second stage compressor.
8. The electrical power generation system of claim 7 , wherein at least one of the one or more shafts passes through the electric generator.
9. An electrical power generation system, comprising:
a micro-turbine alternator, comprising:
a combustor;
at least one turbine configured to be driven by an exhaust from the combustor;
at least one compressor operably connected to the combustor to provide a compressed airflow to the combustor;
one or more shafts connecting the at least one turbine to the at least one compressor such that rotation of the at least one turbine drives rotation of the at least one compressor; and
a bottoming system comprising:
a bottoming blower configured to deliver air to the at least one compressor;
a bottoming drive shaft; and
a bottoming turbine operably connected to the bottoming blower through the bottoming drive shaft, wherein the bottoming blower is configured to rotate when the bottoming turbine is rotated by the exhaust;
wherein the at least one compressor comprises:
a first stage compressor;
a second stage compressor; and
a third stage compressor,
wherein the bottoming blower is configured to provide air to the first stage compressor.
10. The electrical power generation system of claim 9 , wherein the at least one turbine comprises:
a first stage turbine; and
a second stage turbine, wherein the bottoming turbine is configured to receive the exhaust from the second stage turbine.
11. The electrical power generation system of claim 9 , further comprising:
an electric generator disposed along the one or more shafts such that electrical power is generated via rotation of the one or more shafts, wherein the electric generator is disposed along the one or more shafts between the first stage compressor and the second stage compressor.
12. The electrical power generation system of claim 11 , wherein at least one of the one or more shafts passes through the electric generator.