The Role of Micro Gas Turbines in Energy Transition
Abstract
:1. Introduction
2. Energy Policy
2.1. Climate Change and the Future of the Energy Framework
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- At least 40% reduction in greenhouse gas emissions (from 1990 levels), by decreasing emissions and increasing removals;
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- At least 32.5% improvement in energy efficiency;
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- At least 32% share for renewable energy.
2.2. Option for Future Decentralized Microgrid Energy Structures
2.3. Changing Role of Electric Power
3. Cogeneration of Heat and Power
4. Micro Gas Turbines
5. History
6. Challenges and Opportunities
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- The simple cycle form of micro gas turbines is less efficient than larger industrial gas turbines since the cycle pressure ratio in MGTs is considerably lower. The small size constraint in micro gas turbines imposes manufacturing complications to potential improvements of cycle parameters, such as pressure ratio and turbine inlet temperature. A recuperator helps with compensating for these deficiencies in MGT cycles which makes them an essential element of micro gas turbines, unlike large-scale engines.
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- Micro gas turbines operate at significantly higher shaft speeds. With a smaller size, typical problems such as tip supersonic speeds or mechanical limits are delayed to even higher rotational speeds. Therefore, micro gas turbines can operate at speeds above 100,000 rpm whereas a larger gas turbine will typically operate in the range of 3000 to 20,000 rpm [6]. Moreover, with compensating generators connected to MGTs, the rotational speed can vary according to power demand, unlike most large-scale turbines that remain at a constant speed. This alteration of rotational speed leads to different optimization practices for performance improvements.
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- MGT cycles operate with lower pressure ratios (2~5) and turbine inlet temperatures (typically less than 1000 °C) which make the part-load operation span of these systems different from large-scale gas turbines (with pressure ratios up to 25 and turbine inlet temperatures up to 1700 °C). The span of cycle parameter variations, especially with altering rotational speed, is smaller compared to large-scale gas turbines.
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- Considering the low-pressure ratio as well as the small volumetric flow and small power rating, a single-stage radial compressor and turbine are usually used. Both components have different operational behavior from axial versions, which is the common configuration that is implemented in large-scale engines.
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- If the micro gas turbine operates as a CHP or CCHP unit, the system includes a second heat exchanger that uses the remaining exhaust thermal energy after the recuperator. The available exhaust gas, typically around 300 °C, provides energy for water and space heating, cooling systems such as absorption chillers, and process heat applications. The implementation of an economizer adds more application flexibility as well as constraints to the cycle.
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- The fuel flexibility of MGTs, although having environmental and financial advantages, poses certain challenges to MGT design and operation. For conventional cycles, the low calorific value of the fuels requires the implementation of a larger volumetric flow of fuel to achieve the design turbine inlet temperature. This will affect the original matching point with the compressor. Considering the common turbine choking condition, the larger fuel flow rate results in lower demand for air from the compressor and, in general, an increase in compressor back-pressure and, therefore, lowering the surge margin [6]. On the other hand, a high air–fuel ratio within the primary combustion zone is required for achieving low emission levels at full-load conditions. Lean premix operation requires a large amount of air to be thoroughly mixed with fuel before combustion. This premixing of air and fuel enables clean combustion to occur at a relatively low temperature that is tolerated in uncooled turbines [61]. Therefore, some operational limitations are imposed on the fuel–air flow ratio considering the type of fuel that is injected into the engine.
- higher electrical efficiency;
- increased flexibility for integration with other systems;
- increased flexibility towards the utilization of various sources of energy.
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- component level
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- system level
7. Conclusions
Author Contributions
Funding
Conflicts of Interest
References
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1950 | 1960 | 1970 | 1980 | 1990 | 2000 | 2010 | 2020 | 2030 | 2040 | |
---|---|---|---|---|---|---|---|---|---|---|
DC | 18.0 | 21.7 | 25.3 | 29.6 | 35.1 | 40.2 | 45.3 | 50.5 | 56.0 | 61.6 |
IC | 52.5 | 58.7 | 64.6 | 68.8 | 71.2 | 73.1 | 75.0 | 77.5 | 80.6 | 83.5 |
Capstone | Ansaldo | FlexEnergy | MTT | |
---|---|---|---|---|
NOx [@ 15% O2] | <9 ppm | <15 ppm | <5 ppm | <27 ppm (10 ppm with FLOX) |
CO [@ 15% O2] | <40 ppm | <15 ppm | <5 ppm | <50 ppm (10 ppm with FLOX) |
UHC [@ 15% O2] | <9 ppm | N/A | <5 ppm | N/A |
Technology | Steam Turbine | Gas Turbine | Microturbine | |
---|---|---|---|---|
Capacity | MW | 0.5 to several hundred | 0.5–300 | 0.03–0.25 |
Power efficiency | Based on HHV | 5–40+% | 24–36% | 25–35% |
Overall efficiency | Based on HHV | near 80% | 66–71% | 63–85% |
Typical power–heat ratio | - | 0.07–0.1 | 0.6–1.1 | 0.5–0.7 |
Part-load | - | ok | poor | ok |
CHP installed costs | $/kWe | 670–1100 | 1200–3300 | 2500–4300 |
O&M cost | $/kWe | 0.006–0.01 | 0.009–0.013 | 0.009–0.013 |
Availability | 72–99% | 93–96% | 98–99% | |
Hours to overhauls | >50,000 | 25,000–50,000 | 40,000–80,000 | |
Start-up time | 1 h–1 day | 10 min–1 h | 60 s | |
Fuels | all | natural gas, synthetic gas, landfill gas, fuel oils | natural gas, biogas, sour gas, liquid fuels | |
Noise | high | moderate | moderate | |
Uses of thermal output | process steam, district heating, hot water, chilled water | direct heat, hot water, LP & HP steam | direct heat, hot water, chiller | |
Power density | kW/m2 | >100 | 20–500 | 5–70 |
NOx | lb/MMBtU | gas 0.1–0.2 wood 0.2–0.5 coal 0.3–1.2 | 0.036–0.05 | 0.015–0.036 |
NOx | lb/MWh total output | gas 0.4–0.8 wood 0.9–1.4 coal 1.2–5.0 | 0.52–1.31 | 0.14–0.49 |
Advantages | high overall efficiency, high temperature, high-quality heat any type of fuel may be used ability to meet more than one site heat grade requirement long working life and high reliability power–heat ratio can be varied | high reliability low emissions high-grade heat available no cooling required high-cost effectiveness | small number of moving parts compact size and light weight low emissions no cooling required | |
Disadvantages | slow start-up low power to heat ratio | require high-pressure gas or in-house gas compressor poor efficiency at low loading output falls as ambient temperature rises | high costs relatively low mechanical efficiency limited to lower temperature cogeneration applications |
Technology | Reciprocating Engine | Fuel Cell | |
---|---|---|---|
Capacity | MW | 0.005–10 | 200–2.8 commercial CHP |
Power efficiency | Based on HHV | 27–41% | 30–63% |
Overall efficiency | Based on HHV | 77–80% | 55–80% |
Typical power–heat ratio | - | 0.5–1.2 | 1–2 |
Part-load | - | ok | good |
CHP installed costs | $/kWe | 1500–29,000 | 5000–6500 |
O&M cost | $/kWe | 0.009–0.025 | 0.032–0.038 |
Availability | 96–98% | >95% | |
Hours to overhauls | 30,000–60,000 | 32,000–64,000 | |
Start-up time | 10 s | 3 h–2 days | |
Fuels | natural gas, biogas, propane, LPG, sour gas, industrial waste gas, manufactured gas | hydrogen, natural gas, propane, methanol | |
Noise | high | low | |
Uses of thermal output | space heating, hot water, cooling, LP steam | hot water, LP-HP steam | |
Power density | kW/m2 | 35–50 | 5–20 |
NOx | lb/MMBtU | 0.013 rich burn 3-way cat. 0.17 lean burn | 0.0025–0.0040 |
NOx | lb/MWh total output | 0.06 rich burn 3-way cat. 0.8 lean burn | 0.011–0.016 |
Advantages | high power efficiency with part-load operational flexibility fast start-up relatively low investment cost can be used in standalone mode and have good load following capability can be overhauled on-site with normal operators operate on low-pressure gas | low emissions low noise high efficiency good part-load behavior low maintenance | |
Disadvantages | low electrical efficiency | high costs low durability fuels requiring processing unless pure hydrogen is used start-up time |
Model | Manufacturers | Power Output | Set | Total Efficiency 1 | PR | TIT | NS |
---|---|---|---|---|---|---|---|
kW | % | - | rpm | ||||
- | AlliedSignal | 75 | single shaft | 30 (HHV) | 3.8 | 871 | 85,000 |
TA45 | Elliott Energy System | 45 | single shaft | 30 | - | 871 | - |
TA80 | Elliott Energy System | 80 | single shaft | 30 | - | 871 | 68,000 |
TA200 | Elliott Energy System | 200 | single shaft | 30 | - | 871 | 43,000 |
C30 | Capstone | 30 | single shaft | 28 | - | 871 | 96,000 |
C65 | Capstone | 65 | single shaft | 29 | - | 871 | 85,000 |
C200 HP | Capstone | 200 | single shaft | 33 | - | 870 | 45,000 |
- | Power WorksTM | 70 | dual shaft | 30 (HHV) | 3 | 704 | - |
T100 | Turbec | 100 | single shaft | 30 | 4.5 | 950 | 70,000 |
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Banihabib, R.; Assadi, M. The Role of Micro Gas Turbines in Energy Transition. Energies 2022, 15, 8084. https://doi.org/10.3390/en15218084
Banihabib R, Assadi M. The Role of Micro Gas Turbines in Energy Transition. Energies. 2022; 15(21):8084. https://doi.org/10.3390/en15218084
Chicago/Turabian StyleBanihabib, Reyhaneh, and Mohsen Assadi. 2022. "The Role of Micro Gas Turbines in Energy Transition" Energies 15, no. 21: 8084. https://doi.org/10.3390/en15218084
APA StyleBanihabib, R., & Assadi, M. (2022). The Role of Micro Gas Turbines in Energy Transition. Energies, 15(21), 8084. https://doi.org/10.3390/en15218084