Transient Stability Improvement of Large-Scale Photovoltaic Grid Using a Flywheel as a Synchronous Machine
Abstract
:1. Introduction
- Retrofit current synchronous generators to be decommissioned with a flywheel to enhance system inertia and strength using a prevailing excitation control circuit for voltage regulation. The device works as an unloaded synchronous motor deprived of the governor and load detached. In transient situations, the synchronous motor operates like a generator to supply a fault current, using the kinetic energy kept in the flywheel.
- Modeling of the synchronous-type machine with the integration of flywheel for a power grid led by photovoltaic energy at a large scale, and thus, to improve the fault riding through the system.
- Enhance power grid security and the dependability of supply.
- Software simulation is performed in PowerWorld software to attain the results of a flywheel integration into a synchronous machine to increase system fault ride and inertia through of the system. Then the results are compared to the IEE1547 standard to validate network code compliance.
2. Methodology and Research Design
- The load impedances have an insignificant influence on fault impedance as they are short-circuited in a fault.
- The impedance of the source is not accessible, and, in the worst scenarios, entire generators, lines, and transformers are supposed to be operational to produce extreme fault levels.
- A driving voltage of 1.1 per unit behind an impedance of sub-transient is expected to produce an extreme fault level to provide adequate system strength.
2.1. PV Inverter Grid Code Compliance (IEE1547)
2.2. Analysis of Synchronous Machine and Flywheel Shaft Torque
Mathematical Modeling of Flywheel Shaft
2.3. Data Input Model
2.4. Software Model Configuration and Validation
- (a)
- Generator;
- (b)
- Exciter;
- (c)
- Governor (not applicable to PV).
Newton-Raphson Algorithm
3. Simulation Results and Analysis
- The available software for carrying out dynamic model mapping is helpful and can save time when creating a practical model, as well as validation and analysis.
- The successful creation of expected failure schedules and running them in simulation times.
- Ease in terms of plotting and graphically displaying the attained results.
3.1. Case Study 1: 3-ϕ Fault Simulation without Flywheel at 30% PV
3.2. Case Study 2: 3-ϕ Fault Simulation without Flywheel at 50% PV
3.3. Case Study 3: 3-ϕ Fault Simulation at 50%-with Flywheel
3.4. Case Study 4: Asymmetrical Fault L-G Fault with Consideration of 50% PV
4. Conclusions
- Enhanced LVRT for power grids with high photovoltaic penetration.
- Provides quick, dynamic reactive support to aid voltage retrieval.
- Provides stability of frequency by regulating the rapid RoCoF during a disturbance.
Author Contributions
Funding
Data Availability Statement
Conflicts of Interest
Nomenclature
BESS | Battery Energy Storage Systems |
Hz | Hertz (cycles per seconds) |
IBR | Inverter-based energy resources |
L-G | Line to Ground |
LSPV | Large Scale Photovoltaic |
LVRT | Lower Voltage Ride Through |
MVAR | Mega volt amps reactive |
MW | Megawatts |
pu | Per unit |
PV | Photovoltaic |
RoCOF | Rate of Change of system frequency |
sec | Seconds |
STATCOMs | Static Compensators |
SVCs | Static Var Compensators |
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Ref. | Techniques | Parameters to be Controlled | Comments | ||||
---|---|---|---|---|---|---|---|
Inertia | Increase Inertia Range | System Strength | Voltage | Frequency | |||
[17] | Synchronous Condenser | Yes | Fixed | Yes | Yes | Yes | Extensive, narrow, control range-Rotor Only |
[19] | SVC | No | No | No | Yes | No | |
[19] | STATCOM | No | No | No | Yes | No | |
[25] | Batteries | No | No | Yes | Yes | Limited Capability | |
[26] | Inverters | Virtual Inertia | No | Yes (Limited) | Yes | No | |
This Paper | Synchronous Machine With Flywheel | Yes | Yes-Wide Range | Yes | Yes | Yes | Cheap Use existing infrastructure dynamic range: Rotor + Flywheel |
IEEE 1547 | |||
---|---|---|---|
Range of Voltage (%) | Disconnection Time (s) | Range of Frequency (Hz) | Disconnection Time (s) |
V < 50 | 0.16 | 59.3 < V < 60.5 | 0.16 |
50 ≤ V < 88 | 2.00 | ||
110 < V < 120 | 1.00 | ||
V ≥ 120 | 0.16 |
Generator 1 and 2 Parameters | |||
---|---|---|---|
Ra (pu) | 2.7153 × | Xd ″ (pu) | 0.250 |
X1 (pu) | 0.171 | Xq ″ (pu) | 0.240 |
Xd (pu) | 1.204 | Td ′ | 1.01 |
Xq (pu) | 0.437 | Td ″ (s) | 0.052 |
Xd ′ (pu) | 0.294 | Tq ″ (s) | 0.13 |
Parameters | Bus#1 (Slack/Infinite) | Bus#2 | Bus#3 (Photovoltaic) |
---|---|---|---|
Initialisation of Model Load Flow (Steady State Value) | |||
Voltage (p.u) | 1 | 1.05 | 1.05 |
Frequency (Hz) | 50 | 50 | 50 |
Voltage angle (degree) | 0 | 0.6 | 0.85 |
Case Study 1 and 2 | Values of before-fault with no flywheel | ||
Voltage p.u (case#1) Voltage p.u (case#2) | 1.04 1.03 | 1.02 1.03 | 1.02 1.02 |
Frequency Hz (case#1) Frequency Hz (case#2) | 50 50 | 50 50 | 50 50 |
Case Study 1 and 2 | Worst situation values in disturbance with no flywheel | ||
Voltage p.u (case#1) Voltage p.u (case#2) | 0.91 0.85 | 0.2 0.32 | 0.65 0.25 |
Frequency Hz (case#1) Frequency Hz (case#2) | 49.9 47 | 50.45 53 | 50.15 70 |
Case Study 1 and 2 | Values of after-fault with no flywheel | ||
Voltage p.u (case#2) | 1.03 | 1.02 | 0.98 |
Frequency Hz (case#2) | 50.1 | 50.1 | 50.1 |
Case Study 3 | Parameter values for before fault condition using flywheel | ||
Rotor Speed (p.u) | 1 | 1 | Not valid for PV |
Angle of rotor (degree) | 3.0 | 62.1 | Not valid |
Voltage attained (p.u) | 1.02 | 1.03 | 1.02 |
Frequency (Hz) | 50 | 50 | 50 |
Reactive power (MVAR) | 100.0 | 48.0 | 0 |
Case Study 3 | Parameter values in worst condition with disturbance using flywheel | ||
Speed of rotor (p.u) | 0.99 | 1.012 | Not valid for PV |
Angle of rotor (degree) | 15 | 85 | Not valid for PV |
Voltage (p.u) | 0.89 | 0.3 | 0.59 |
Frequency (Hz) | 50.3 | 50.9 | 50.35 |
Reactive power (MVAR) | 560 | 250 | 55 |
Case Study 3 | Values of after-fault using a flywheel | ||
Speed of rotor (p.u) | 1 | 1.01 | Not valid |
Angle of rotor (degree) | 1 | 63.1 | Not valid |
Voltage (p.u) | 1 | 1.03 | 1.01 |
Frequency (Hz) | 50.1 | 50.1 | 50.1 |
Reactive power (MVAR) | 20 | 45 | 0 |
Case study 4 | Values of before-Fault using Flywheel | ||
Voltage (p.u) | 1.04 | 1.04 | 1.03 |
Frequency (Hz) | 50 | 50 | 50 |
Case study 4 | Worst Condition Values in Disturbance Using a Flywheel | ||
Voltage (p.u) | 1.1 | 1.23 | 1.15 |
Frequency (Hz) | 49.85 | 49 | 49.25 |
Case study 4 | Values of after Fault using a Flywheel | ||
Frequency (Hz) | 50.04 | 50.04 | 50.4 |
Voltage (p.u) | 1.04 | 1.02 | 0.95 |
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Marupi, M.; Batool, M.; Alizadeh, M.; Zanib, N. Transient Stability Improvement of Large-Scale Photovoltaic Grid Using a Flywheel as a Synchronous Machine. Energies 2023, 16, 689. https://doi.org/10.3390/en16020689
Marupi M, Batool M, Alizadeh M, Zanib N. Transient Stability Improvement of Large-Scale Photovoltaic Grid Using a Flywheel as a Synchronous Machine. Energies. 2023; 16(2):689. https://doi.org/10.3390/en16020689
Chicago/Turabian StyleMarupi, Masilu, Munira Batool, Morteza Alizadeh, and Noor Zanib. 2023. "Transient Stability Improvement of Large-Scale Photovoltaic Grid Using a Flywheel as a Synchronous Machine" Energies 16, no. 2: 689. https://doi.org/10.3390/en16020689