M.R. Vogt
Please Note
15 records found
1
This research evaluates the impact of TenneT’s proposed distribution, determines the mathematically optimal siting and sizing of 10 GW of BESS to minimize short-run marginal costs, and assesses how this distribution adapts under three distinct 2030 grid scenarios defined by Netbeheer Nederland. The Dutch high-voltage grid was modeled using Python and the PyPSA framework. To overcome the computational burden of linear programming on a full-year dataset, time series aggregation via hierarchical clustering was utilized to condense the data into 12 representative days.
Simulations demonstrate that while TenneT’s proposed distribution successfully lowers grid costs and reduces renewable curtailment, a mathematically optimized distribution yields superior economic performance. By concentrating battery capacity in specific high-value locations, the optimized model generates an additional €20 million in annual savings compared to TenneT’s maximum deployment proposal. However, applying this optimization to the 2030 scenarios reveals that future grids will face much heavier constraints, necessitating a more granular and evenly dispersed battery distribution across the country.
Sensitivity analyses indicate that the highly meshed nature of the Dutch high-voltage grid renders the absolute financial differences between various geographic distributions extremely small—less than 0.1%. Consequently, while optimizing battery placement at the transmission level provides tangible economic benefits, extreme precision in geographic siting offers diminishing returns. Future research should incorporate multi-year weather dynamics, cross-border market integrations, and a shifted focus toward distribution-level grids to fully realize the potential of battery storage in the Netherlands. ...
This research evaluates the impact of TenneT’s proposed distribution, determines the mathematically optimal siting and sizing of 10 GW of BESS to minimize short-run marginal costs, and assesses how this distribution adapts under three distinct 2030 grid scenarios defined by Netbeheer Nederland. The Dutch high-voltage grid was modeled using Python and the PyPSA framework. To overcome the computational burden of linear programming on a full-year dataset, time series aggregation via hierarchical clustering was utilized to condense the data into 12 representative days.
Simulations demonstrate that while TenneT’s proposed distribution successfully lowers grid costs and reduces renewable curtailment, a mathematically optimized distribution yields superior economic performance. By concentrating battery capacity in specific high-value locations, the optimized model generates an additional €20 million in annual savings compared to TenneT’s maximum deployment proposal. However, applying this optimization to the 2030 scenarios reveals that future grids will face much heavier constraints, necessitating a more granular and evenly dispersed battery distribution across the country.
Sensitivity analyses indicate that the highly meshed nature of the Dutch high-voltage grid renders the absolute financial differences between various geographic distributions extremely small—less than 0.1%. Consequently, while optimizing battery placement at the transmission level provides tangible economic benefits, extreme precision in geographic siting offers diminishing returns. Future research should incorporate multi-year weather dynamics, cross-border market integrations, and a shifted focus toward distribution-level grids to fully realize the potential of battery storage in the Netherlands.
Design and Testing of Barrier Layers for Reliability Enhancement in High-Efficiency Flexible Thin-Film Solar Cells
Mitigating mechanical failure in thin-film solar cells through annealing and stack modifications
In this work, 29 samples were fabricated and evaluated to decouple and mitigate these failure mechanisms using laser scanning confocal profilometry and dark I-V characterization. Systematic investigations evaluated varying mid-etch annealing temperatures (100–140°C), pre- and post-etch thermal treatments, and stack architecture modifications, specifically introducing a continuous full-area aluminum back contact and an intrinsic Zinc Oxide (iZnO) interlayer.
Results demonstrate that stack architecture modifications yield the most significant improvements: a full-area aluminum back contact reduces average buckle height by 29–36% and markedly suppresses sample-to-sample scatter. The iZnO interlayer recovers roughly 43% of this benefit, demonstrating that both added mechanical stiffness and physical separation from the EVA encapsulant contribute to film stabilization. The most promising process configuration, combining a full-area back contact with a 70°C pre-anneal and a 120°C mid-anneal, provides a baseline for advancing mechanically robust, barrier-integrated flexible solar foils. ...
In this work, 29 samples were fabricated and evaluated to decouple and mitigate these failure mechanisms using laser scanning confocal profilometry and dark I-V characterization. Systematic investigations evaluated varying mid-etch annealing temperatures (100–140°C), pre- and post-etch thermal treatments, and stack architecture modifications, specifically introducing a continuous full-area aluminum back contact and an intrinsic Zinc Oxide (iZnO) interlayer.
Results demonstrate that stack architecture modifications yield the most significant improvements: a full-area aluminum back contact reduces average buckle height by 29–36% and markedly suppresses sample-to-sample scatter. The iZnO interlayer recovers roughly 43% of this benefit, demonstrating that both added mechanical stiffness and physical separation from the EVA encapsulant contribute to film stabilization. The most promising process configuration, combining a full-area back contact with a 70°C pre-anneal and a 120°C mid-anneal, provides a baseline for advancing mechanically robust, barrier-integrated flexible solar foils.
Creating an Educational Integrated Sound Sculpture
Digital Signal Processing and Wave Generation
Safe Solar PV Integration in Hazardous-Classified Liquid Bulk Terminals
A Risk-Based Site Suitability and Energy Yield Assessment at Euro Tank Amsterdam
For the suitability assessment, seven main criteria and seventeen sub-criteria were constructed from a combination of industry standards (including the Seveso III, ISO, Omgevingswet, IEC, NEN-EN, ATEX, and PGS frameworks), expert experience, and academic literature, with an emphasis on the risks
introduced by PV installation in a hazardous-classified environment. Two multi-criteria decision-making (MCDM) methods, the Analytic Hierarchy Process (AHP) and the Technique for Order of Preference by Similarity to Ideal Solution (TOPSIS), were combined to weight the criteria and rank ten candidate
locations identified through a spatial inventory of the site. A safety hard-gate veto was introduced as a novel element of the framework; the AHP weighting independently confirmed safety as the most important criterion, consistent with industry practice. Of the ten candidate locations, six were found suitable, with the piping supports and tank shells identified as marginally suitable cases requiring further detailed engineering and risk assessment before deployment. A ten-percent sensitivity analysis on the closeness-coefficient thresholds confirmed the robustness of the ranking.
The tank shell was selected for detailed yield modelling on account of its large available surface area and the novel modelling questions posed by its curved, vertical geometry at the system level. The site was modelled to represent the installation as closely to reality as possible: a dedicated module placement algorithm was developed to populate the cylindrical wall, and a perovskite/perovskitetandem module was simulated with the PVMD Toolbox across a full year of Amsterdam weather data, for both landscape and portrait placement orientations and across the cardinal directions. The results show
that placement orientation (landscape versus portrait) has only a minor effect on yield (on the order of one to four percent), whereas the facing direction is decisive: east-, west-, and south-facing modules substantially outperform north-facing ones. Because the modules are vertically mounted, the plane of-array (POA) irradiance, which captures the azimuth-corrected angle of incidence governs the yield, rather than the global horizontal irradiance alone. A pronounced seasonal effect was identified in which monthly yield peaks in spring rather than mid-summer despite the higher summer irradiance; a highly
plausible cause of this offset which is shown in the in the POA-to-DC conversion efficiency is not to thermal derating, since module temperatures remain mild throughout the year, but mainly to inter-tank shading arising from the prevailing geometry and possibly angle of inscidence reflection. The performance across different tank arrangements was found to depend strongly on the number of unshaded cells, demonstrating the impact of inter-tank shading.
Aggregating the simulated yield across the full terminal with Benzolweg, chosen as the main site of interest demonstrated that PV installed on the tank shells alone, without the inclusion of storage or other demand-side measures could generate roughly 2.45 times the site’s annual electricity demand, yet owing to the strongly baseload-dominated and continuous nature of terminal operations and the intermittency of solar availability, could cover only about 38% of that demand directly. This reveals a fundamental trade-off between self-consumption and self-sufficiency that must be balanced when sizing the system and constructing a viable business case. The thesis concludes with recommendations for fuzzy MCDM extensions, broader expert elicitation, a curved-surface optical and electrical modelling capability for system-level applications, and the integration of energy storage to address the temporal mismatch between generation and demand. ...
For the suitability assessment, seven main criteria and seventeen sub-criteria were constructed from a combination of industry standards (including the Seveso III, ISO, Omgevingswet, IEC, NEN-EN, ATEX, and PGS frameworks), expert experience, and academic literature, with an emphasis on the risks
introduced by PV installation in a hazardous-classified environment. Two multi-criteria decision-making (MCDM) methods, the Analytic Hierarchy Process (AHP) and the Technique for Order of Preference by Similarity to Ideal Solution (TOPSIS), were combined to weight the criteria and rank ten candidate
locations identified through a spatial inventory of the site. A safety hard-gate veto was introduced as a novel element of the framework; the AHP weighting independently confirmed safety as the most important criterion, consistent with industry practice. Of the ten candidate locations, six were found suitable, with the piping supports and tank shells identified as marginally suitable cases requiring further detailed engineering and risk assessment before deployment. A ten-percent sensitivity analysis on the closeness-coefficient thresholds confirmed the robustness of the ranking.
The tank shell was selected for detailed yield modelling on account of its large available surface area and the novel modelling questions posed by its curved, vertical geometry at the system level. The site was modelled to represent the installation as closely to reality as possible: a dedicated module placement algorithm was developed to populate the cylindrical wall, and a perovskite/perovskitetandem module was simulated with the PVMD Toolbox across a full year of Amsterdam weather data, for both landscape and portrait placement orientations and across the cardinal directions. The results show
that placement orientation (landscape versus portrait) has only a minor effect on yield (on the order of one to four percent), whereas the facing direction is decisive: east-, west-, and south-facing modules substantially outperform north-facing ones. Because the modules are vertically mounted, the plane of-array (POA) irradiance, which captures the azimuth-corrected angle of incidence governs the yield, rather than the global horizontal irradiance alone. A pronounced seasonal effect was identified in which monthly yield peaks in spring rather than mid-summer despite the higher summer irradiance; a highly
plausible cause of this offset which is shown in the in the POA-to-DC conversion efficiency is not to thermal derating, since module temperatures remain mild throughout the year, but mainly to inter-tank shading arising from the prevailing geometry and possibly angle of inscidence reflection. The performance across different tank arrangements was found to depend strongly on the number of unshaded cells, demonstrating the impact of inter-tank shading.
Aggregating the simulated yield across the full terminal with Benzolweg, chosen as the main site of interest demonstrated that PV installed on the tank shells alone, without the inclusion of storage or other demand-side measures could generate roughly 2.45 times the site’s annual electricity demand, yet owing to the strongly baseload-dominated and continuous nature of terminal operations and the intermittency of solar availability, could cover only about 38% of that demand directly. This reveals a fundamental trade-off between self-consumption and self-sufficiency that must be balanced when sizing the system and constructing a viable business case. The thesis concludes with recommendations for fuzzy MCDM extensions, broader expert elicitation, a curved-surface optical and electrical modelling capability for system-level applications, and the integration of energy storage to address the temporal mismatch between generation and demand.
The transition to renewable energy, led by photovoltaic (PV) energy, is critical for a sustainable future. However, the current linear ”take-make-waste” economy, also used for PV modules, presents a significant challenge to long-term sustainability, creating a massive future waste stream and reliance on virgin materials. The primary obstacle to achieving a circular economy for solar modules is the use of permanently cross-linked solid encapsulants like Ethylene Vinyl Acetate (EVA), which bond all components together and severely hinder repair, reuse, and high-value recycling. This thesis examines liquid encapsulation as a promising alternative design-for-recycling concept, enabling simple disassembly and material recovery. The primary objective was to determine if liquid encapsulation is a viable alternative from an optical perceptive, compared to conventional solid (EVA) and gas-filled (air) module designs. To achieve this, three sub-goals were formulated and completed. First, a comprehensive selection strategy was developed based on critical optical, electrical, chemical, and thermal criteria, identifying seven candidate liquids for analysis: deionised water, glycerol, SolaPro Ennogreen glycol, Polydimethylsiloxane (PDMS), and three industrial dielectric oils (Shell Diala S4 XZI, Midel 7131, Mivolt). Material compatibility tests with polyisobutylene (PIB) immersed in Midel 7131 and Shell Diala, confirmed that Shell, and therefore mineral oils in general, are incompatible with the use of PIB as a sealant. Second, the complex refractive index (n and k) of these liquids was experimentally measured over the 300–1200 nm solar spectrum using a novel hybrid method. This involved a specialised ellipsometer and dual cuvette measurements with spectrophotometry, generating the nk data needed for detailed optical modelling. Measurements made by Semilab’s liquid-specialised ellipsometer using a 2-term Cauchy model yielded excellent fits (R2 > 0.97) for all liquids, in good agreement with literature values. The dual cuvette method revealed extremely high transparency for all liquids, even slightly yellowish fluids Midel and Shell Diala. A SNR analysis established a confidence threshold at k ≈ 5 ∗ 10−8. Finally, these optical properties were used as inputs for detailed optical modelling and simulation, in GenPro4, to quantify and compare the photocurrent generated by liquid encapsulation compared to standard EVA and air, in various solar module configurations. The optical model and its simulated output are validated through experiments and datasheets, showing excellent agreement around the Δ Jph = 0.2 mA/cm2. The results revealed a fundamental trade-off: while the liquids have lower refractive indices, leading to higher initial reflection losses compared to conventional EVA with UV blockers, their superior transparency resulted in lower parasitic absorption. This balance allowed top-performing liquids, notably Mivolt (highest photocurrent and lowest reflector, Jph = 40.90 41.81 mA/cm2) and PDMS (lowest absorber, Jph = 40.85 41.75 mA/cm2), to generate a photocurrent comparable to, and in some cases higher than, UV-transparent EVA (Jph = 40.92 41.81 mA/cm2). However, the optical performance of the other liquids was very close (especially Midel and Shell, but also glycerol and glycol, followed within 0.17 mA/cm2), meaning that based on optics alone, they should not be excluded, as other design benefits might justify their selection. A critical insight emerged from annual energy yield simulations, which demonstrated that PDMS delivered the highest yearly energy output (0.07% higher than EVA-UVT, 0.086% to Mivolt), due to its extremely low absorption. The simulations showed that mitigating reflection losses through tailored Anti-Reflection Coatings (ARCs) or glass texturing can further unlock the full potential of liquid-encapsulated modules. In conclusion, this thesis provides the first comprehensive optical validation for liquid encapsulation in standard silicon PV modules. It successfully demonstrates that, from an optical standpoint, liquids are a highly viable technology, worthy of further research. Their primary drawback of higher reflection is compensated by superior transparency and can also be further mitigated with existing ARC and glass texturing technologies. This work establishes a robust foundation for future research, confirming that liquid encapsulation is not only a promising pathway toward a circular economy for PV but is also an optically competitive alternative to established solid encapsulants. ...
The transition to renewable energy, led by photovoltaic (PV) energy, is critical for a sustainable future. However, the current linear ”take-make-waste” economy, also used for PV modules, presents a significant challenge to long-term sustainability, creating a massive future waste stream and reliance on virgin materials. The primary obstacle to achieving a circular economy for solar modules is the use of permanently cross-linked solid encapsulants like Ethylene Vinyl Acetate (EVA), which bond all components together and severely hinder repair, reuse, and high-value recycling. This thesis examines liquid encapsulation as a promising alternative design-for-recycling concept, enabling simple disassembly and material recovery. The primary objective was to determine if liquid encapsulation is a viable alternative from an optical perceptive, compared to conventional solid (EVA) and gas-filled (air) module designs. To achieve this, three sub-goals were formulated and completed. First, a comprehensive selection strategy was developed based on critical optical, electrical, chemical, and thermal criteria, identifying seven candidate liquids for analysis: deionised water, glycerol, SolaPro Ennogreen glycol, Polydimethylsiloxane (PDMS), and three industrial dielectric oils (Shell Diala S4 XZI, Midel 7131, Mivolt). Material compatibility tests with polyisobutylene (PIB) immersed in Midel 7131 and Shell Diala, confirmed that Shell, and therefore mineral oils in general, are incompatible with the use of PIB as a sealant. Second, the complex refractive index (n and k) of these liquids was experimentally measured over the 300–1200 nm solar spectrum using a novel hybrid method. This involved a specialised ellipsometer and dual cuvette measurements with spectrophotometry, generating the nk data needed for detailed optical modelling. Measurements made by Semilab’s liquid-specialised ellipsometer using a 2-term Cauchy model yielded excellent fits (R2 > 0.97) for all liquids, in good agreement with literature values. The dual cuvette method revealed extremely high transparency for all liquids, even slightly yellowish fluids Midel and Shell Diala. A SNR analysis established a confidence threshold at k ≈ 5 ∗ 10−8. Finally, these optical properties were used as inputs for detailed optical modelling and simulation, in GenPro4, to quantify and compare the photocurrent generated by liquid encapsulation compared to standard EVA and air, in various solar module configurations. The optical model and its simulated output are validated through experiments and datasheets, showing excellent agreement around the Δ Jph = 0.2 mA/cm2. The results revealed a fundamental trade-off: while the liquids have lower refractive indices, leading to higher initial reflection losses compared to conventional EVA with UV blockers, their superior transparency resulted in lower parasitic absorption. This balance allowed top-performing liquids, notably Mivolt (highest photocurrent and lowest reflector, Jph = 40.90 41.81 mA/cm2) and PDMS (lowest absorber, Jph = 40.85 41.75 mA/cm2), to generate a photocurrent comparable to, and in some cases higher than, UV-transparent EVA (Jph = 40.92 41.81 mA/cm2). However, the optical performance of the other liquids was very close (especially Midel and Shell, but also glycerol and glycol, followed within 0.17 mA/cm2), meaning that based on optics alone, they should not be excluded, as other design benefits might justify their selection. A critical insight emerged from annual energy yield simulations, which demonstrated that PDMS delivered the highest yearly energy output (0.07% higher than EVA-UVT, 0.086% to Mivolt), due to its extremely low absorption. The simulations showed that mitigating reflection losses through tailored Anti-Reflection Coatings (ARCs) or glass texturing can further unlock the full potential of liquid-encapsulated modules. In conclusion, this thesis provides the first comprehensive optical validation for liquid encapsulation in standard silicon PV modules. It successfully demonstrates that, from an optical standpoint, liquids are a highly viable technology, worthy of further research. Their primary drawback of higher reflection is compensated by superior transparency and can also be further mitigated with existing ARC and glass texturing technologies. This work establishes a robust foundation for future research, confirming that liquid encapsulation is not only a promising pathway toward a circular economy for PV but is also an optically competitive alternative to established solid encapsulants.
Optimising and Controlling Isolated DC-DC Power Converter Topology for Sustainable Energy Technology Applications
Can power converter topologies become even more efficient?
Life Cycle Assessment of a PV System with Silicon Heterojunction modules
Current and Prospective scenarios based on manufacturing in the Netherlands
Furthermore, a laboratory setup will be constructed to validate the charging behaviors that need to be incorporated into smart charging algorithms and to explore new EV charging behaviors in an experiment. The charging phenomena identified as significant will be integrated into the smart charging algorithm, with a lookup table, to assess their influence on the overall system performance.
The results of this investigation provide valuable insights regarding the charging behaviors and the impact of incorporating these behaviors into a smart charging algorithm. A degradation of the charging efficiency was noted at low charging currents, with the significance of the degradation varying between EV types. Additionally, a voltage discrepancy of the pulse width modulation (PWM) signal of the EVSE was observed, causing an offset between the setpoint of the charging current and the real charging current transmitted by the EVSE.
When these results were incorporated into a smart charging algorithm with a lookup table, clear improvements were seen in the total charged capacity compared to a smart charging algorithm that did not include the lookup table. At a grid capacity of 125 A, the smart charging algorithm with the lookup table provided an increase in charging capacity of 5.23% and an increase of 1.40% for a grid capacity of 175 A. Furthermore, it was observed that the smart charging algorithm with the lookup table could increase the total charged capacity for the low grid capacity of 125 A by 3.97% compared to the charging algorithm that performed immediate charging and DPM.
Both smart charging algorithms, with and without lookup table, show the same reduction in cost compared to the base case algorithm that performs DPM and immediate charging. A decrease in the average charging cost to 4.88% at a grid capacity of 125 A was noted. When the grid capacity is increased, the charging cost could be further decreased to 12.23%, as the increased capacity allows for greater flexibility in scheduling EVs during periods of lowest prices, optimizing the utilization of available power.
...
Furthermore, a laboratory setup will be constructed to validate the charging behaviors that need to be incorporated into smart charging algorithms and to explore new EV charging behaviors in an experiment. The charging phenomena identified as significant will be integrated into the smart charging algorithm, with a lookup table, to assess their influence on the overall system performance.
The results of this investigation provide valuable insights regarding the charging behaviors and the impact of incorporating these behaviors into a smart charging algorithm. A degradation of the charging efficiency was noted at low charging currents, with the significance of the degradation varying between EV types. Additionally, a voltage discrepancy of the pulse width modulation (PWM) signal of the EVSE was observed, causing an offset between the setpoint of the charging current and the real charging current transmitted by the EVSE.
When these results were incorporated into a smart charging algorithm with a lookup table, clear improvements were seen in the total charged capacity compared to a smart charging algorithm that did not include the lookup table. At a grid capacity of 125 A, the smart charging algorithm with the lookup table provided an increase in charging capacity of 5.23% and an increase of 1.40% for a grid capacity of 175 A. Furthermore, it was observed that the smart charging algorithm with the lookup table could increase the total charged capacity for the low grid capacity of 125 A by 3.97% compared to the charging algorithm that performed immediate charging and DPM.
Both smart charging algorithms, with and without lookup table, show the same reduction in cost compared to the base case algorithm that performs DPM and immediate charging. A decrease in the average charging cost to 4.88% at a grid capacity of 125 A was noted. When the grid capacity is increased, the charging cost could be further decreased to 12.23%, as the increased capacity allows for greater flexibility in scheduling EVs during periods of lowest prices, optimizing the utilization of available power.
The concept of reconfigurable battery packs involves using power switches to modify the arrangement of connected battery cells based on specific requirements. This innovative technique can potentially significantly reduce the weight of battery packs. The primary objective of this thesis was to conduct a comprehensive analysis and comparison between fixed configuration and reconfigurable battery packs in the context of electric aviation. It was imperative first to design these battery packs to facilitate this comparison. Given the limited availability of open data on electric aircraft designs, the power profile was estimated using available reference aircraft specifications and reasonable assumptions. The literature review on power systems in aircraft revealed a significant correlation between system-level voltage and the weight of power cables. This discovery led to estimating an optimal system-level voltage, a critical constraint in battery sizing. For the fixed configuration battery pack, sizing was conducted using both a high-specific energy cell and a high-specific power cell. The design of a reconfigurable battery pack involved strategically leveraging both cell types. This innovative approach created a reconfigurable battery pack capable of dynamically connecting and disconnecting an internal high-specific energy battery pack called the 'primary battery pack' and a high-specific power battery pack known as the 'secondary battery pack' through power switches, allowing them to complement each other during high-power demand phases of flight, such as take-off and climbing.
Software simulations were conducted for the validation of this technique. These simulations revealed that the reconfigurable battery pack experienced higher C-rates than the fixed configuration battery pack. Given that higher C-rates can impact battery health by inducing capacity loss over multiple cycles, a preliminary ageing analysis was performed to quantitatively assess the adverse effects of higher C-rates on the reconfigurable battery pack.
The results quantified that around 400 kg of potential weight savings is possible by employing reconfigurable battery packs over fixed configuration battery packs at only 0.4% more capacity loss over 500 charging-discharging cycles. The weight savings can be translated into three different scenarios. Firstly, payload weight capacity can be enhanced. Secondly, flying with lesser weight will offset the power profile, saving energy. Lastly, an additional number of cells equivalent to the mass saved can realise the range extension of the electric aircraft.
...
The concept of reconfigurable battery packs involves using power switches to modify the arrangement of connected battery cells based on specific requirements. This innovative technique can potentially significantly reduce the weight of battery packs. The primary objective of this thesis was to conduct a comprehensive analysis and comparison between fixed configuration and reconfigurable battery packs in the context of electric aviation. It was imperative first to design these battery packs to facilitate this comparison. Given the limited availability of open data on electric aircraft designs, the power profile was estimated using available reference aircraft specifications and reasonable assumptions. The literature review on power systems in aircraft revealed a significant correlation between system-level voltage and the weight of power cables. This discovery led to estimating an optimal system-level voltage, a critical constraint in battery sizing. For the fixed configuration battery pack, sizing was conducted using both a high-specific energy cell and a high-specific power cell. The design of a reconfigurable battery pack involved strategically leveraging both cell types. This innovative approach created a reconfigurable battery pack capable of dynamically connecting and disconnecting an internal high-specific energy battery pack called the 'primary battery pack' and a high-specific power battery pack known as the 'secondary battery pack' through power switches, allowing them to complement each other during high-power demand phases of flight, such as take-off and climbing.
Software simulations were conducted for the validation of this technique. These simulations revealed that the reconfigurable battery pack experienced higher C-rates than the fixed configuration battery pack. Given that higher C-rates can impact battery health by inducing capacity loss over multiple cycles, a preliminary ageing analysis was performed to quantitatively assess the adverse effects of higher C-rates on the reconfigurable battery pack.
The results quantified that around 400 kg of potential weight savings is possible by employing reconfigurable battery packs over fixed configuration battery packs at only 0.4% more capacity loss over 500 charging-discharging cycles. The weight savings can be translated into three different scenarios. Firstly, payload weight capacity can be enhanced. Secondly, flying with lesser weight will offset the power profile, saving energy. Lastly, an additional number of cells equivalent to the mass saved can realise the range extension of the electric aircraft.
The art of texturing glass for Photovoltaics
Processing and optical characterisation
This work introduces a comprehensive model for quantifying the different loss mechanisms in a PV system with tandem cells. The loss analysis model will be added to the PVMD Toolbox, which is a software developed at Photovoltaic Materials and Devices group at Delft University of Technology.
This software can be used to simulate the energy yield of a PV system at any given location. In the loss analysis model, 17 losses are defined and divided into four categories (fundamental, optical, electrical and system losses).
The developed model will be used to analyse the loss distribution under different operating conditions for four different PV modules. These different modules are a mono-facial crystalline silicon, a bifacial crystalline silicon, a two-terminal perovskite/silicon tandem, and a three-terminal perovskite/silicon tandem module. The design of these modules is based on a >29% efficient perovskite/silicon tandem cell, fabricated by HZB.
The loss distribution of every module is simulated for Standard Test Conditions (STC) and for real word conditions at four geographical locations. Generally, we find that modules operating in tropical high irradiance climates have the lowest efficiency. For all locations, the difference in losses compared to STC follow similar trends. When the two-terminal perovskite/silicon module is simulated at STC, the loss distribution of the fundamental, optical, electrical, and system losses are 54.8%, 8.9%, 8.5%, and 0.1%, leaving a DC module efficiency of 27.7%.
At real-world operating conditions, various differences can be found. The most significant differences are the thermalization, reflection, and recombination losses, which increase with 1.4%, 1.1%, and 0.5% respectively for the two terminal perovskite/silicon tandem module. Furthermore, the simulated two-terminal module has a higher efficiency than the three-terminal modules for all operating
conditions due to lower mismatch losses.
Additionally, this study was able to quantify the fill factor gain for two-terminal devices. Due to spectral variations, there can be a mismatch between the absorbed current in the top cell and bottom cell, which can lead to losses. However, this loss is partially compensated by an increase in fill factor. For example, a current mismatch of 7.0% is reduced to a power mismatch loss of 1.2%, due to an increase in fill factor. Therefore, the power mismatch should be used as an indicator for mismatch losses instead of the current mismatch.
Finally, this study simulated different improvements on operating conditions. The results show that solar tracking does not only increase the in-plane irradiance of the PV system, but can also increase the efficiency. For example, dual-axis tracking can increase the efficiency with 1.1%. Also, the gain of active cooling is simulated and quantified. The increase of efficiency when cooling at 20oC
compared to a PV system without cooling is around 0.4%, mostly caused by decrease in emission and recombination losses. Furthermore, the optimal perovskite thickness for real world conditions is found, by simulating different thicknesses for the perovskite layer. The results shows that the optimal
thickness under STC (575 nm) is also optimal under real-world operating conditions. Finally, the optimal bandgap energies for reducing the fundamental losses are found for tandem cells. For all conditions (including STC), the optimal bandgap energies for the top and bottom cell are 1.73 and 0.94 eV respectively.
...
This work introduces a comprehensive model for quantifying the different loss mechanisms in a PV system with tandem cells. The loss analysis model will be added to the PVMD Toolbox, which is a software developed at Photovoltaic Materials and Devices group at Delft University of Technology.
This software can be used to simulate the energy yield of a PV system at any given location. In the loss analysis model, 17 losses are defined and divided into four categories (fundamental, optical, electrical and system losses).
The developed model will be used to analyse the loss distribution under different operating conditions for four different PV modules. These different modules are a mono-facial crystalline silicon, a bifacial crystalline silicon, a two-terminal perovskite/silicon tandem, and a three-terminal perovskite/silicon tandem module. The design of these modules is based on a >29% efficient perovskite/silicon tandem cell, fabricated by HZB.
The loss distribution of every module is simulated for Standard Test Conditions (STC) and for real word conditions at four geographical locations. Generally, we find that modules operating in tropical high irradiance climates have the lowest efficiency. For all locations, the difference in losses compared to STC follow similar trends. When the two-terminal perovskite/silicon module is simulated at STC, the loss distribution of the fundamental, optical, electrical, and system losses are 54.8%, 8.9%, 8.5%, and 0.1%, leaving a DC module efficiency of 27.7%.
At real-world operating conditions, various differences can be found. The most significant differences are the thermalization, reflection, and recombination losses, which increase with 1.4%, 1.1%, and 0.5% respectively for the two terminal perovskite/silicon tandem module. Furthermore, the simulated two-terminal module has a higher efficiency than the three-terminal modules for all operating
conditions due to lower mismatch losses.
Additionally, this study was able to quantify the fill factor gain for two-terminal devices. Due to spectral variations, there can be a mismatch between the absorbed current in the top cell and bottom cell, which can lead to losses. However, this loss is partially compensated by an increase in fill factor. For example, a current mismatch of 7.0% is reduced to a power mismatch loss of 1.2%, due to an increase in fill factor. Therefore, the power mismatch should be used as an indicator for mismatch losses instead of the current mismatch.
Finally, this study simulated different improvements on operating conditions. The results show that solar tracking does not only increase the in-plane irradiance of the PV system, but can also increase the efficiency. For example, dual-axis tracking can increase the efficiency with 1.1%. Also, the gain of active cooling is simulated and quantified. The increase of efficiency when cooling at 20oC
compared to a PV system without cooling is around 0.4%, mostly caused by decrease in emission and recombination losses. Furthermore, the optimal perovskite thickness for real world conditions is found, by simulating different thicknesses for the perovskite layer. The results shows that the optimal
thickness under STC (575 nm) is also optimal under real-world operating conditions. Finally, the optimal bandgap energies for reducing the fundamental losses are found for tandem cells. For all conditions (including STC), the optimal bandgap energies for the top and bottom cell are 1.73 and 0.94 eV respectively.
the module leading to higher energy generation. This, combined with the prediction that bifacial modules will dominate the market in less than 6 years, a parameter used for the evaluation of PV modules performance in different climates needs to be defined namely ”energy rating”.
Energy ratings have been developed only for monofacial modules as described in IEC61853 standard and this work focuses on the extension of this standard to bifacial modules. For the calculation of the energy rating the energy yield and the irradiance incidence on both faces of the module have to be obtained. For this reason, an irradiance model is developed in MATLAB to calculate the irradiance on the rear side of the module using the data given in the standard IEC61853. Note that the front side irradiance is available in the existing data and as a result no further calculations for the front side of the module are required. The irradiance on the rear side of the module is obtained using 2D view factors taking into consideration the shading of the ground which can substantially affect the results. Also, the effect of the elevation of the module from the ground surface is examined and found that at sufficient height (≥ 1푚) the impact of ground clearance on the rear side irradiance is minimised. Finally, the ground reflected irradiance is obtained using the spectral reflectivity of different ground materials where it is shown that the use of improper albedo values can lead to inaccurate results.
The next step is the calculation of the energy yield of the bifacial module. For this, a similar methodology used to obtain the energy yield of monofacial modules in the standard IEC61853 is used. More specifically, the incident irradiance on the rear side of the module is corrected for the angle of incidence and spectrum effects to generate similar conditions as in the STC. Additionally, the operating module temperature is obtained and using the total irradiance on the front and the rear side of the module the energy yield is calculated. Finally, the energy rating of bifacial modules is determined using two different approaches. In the first approach, CSER of bifacial modules is obtained using the energy yield and the total irradiance on bifacial modules. This approach results in lower energy rating than unity but needs re-scaling of the monofacial module energy rating compared to the standard. The second approach use the energy generated from both sides of the module but only the irradiation on the front side of the module is taken into account leading to CSER values higher than one, while the energy rating of monofacial modules as obtained in the standard is used. In both approaches the energy rating of bifacial modules found to be up to 17% higher than that of monofacial depending on the bifaciality of the module and the climate conditions.
The developed model is validated using real outdoor measurements for a system located in Weurt, Eastern Netherlands. First, the in-plane irradiance on both sides of the module is obtained from the model and then, the simulated energy yield is calculated and compared to the measured energy yield of bifacial modules. The results show a small difference between the simulated and measured energy yield for the time period between October 2019 and June 2020 with a total variation of 4.65% in the total energy yield. ...
the module leading to higher energy generation. This, combined with the prediction that bifacial modules will dominate the market in less than 6 years, a parameter used for the evaluation of PV modules performance in different climates needs to be defined namely ”energy rating”.
Energy ratings have been developed only for monofacial modules as described in IEC61853 standard and this work focuses on the extension of this standard to bifacial modules. For the calculation of the energy rating the energy yield and the irradiance incidence on both faces of the module have to be obtained. For this reason, an irradiance model is developed in MATLAB to calculate the irradiance on the rear side of the module using the data given in the standard IEC61853. Note that the front side irradiance is available in the existing data and as a result no further calculations for the front side of the module are required. The irradiance on the rear side of the module is obtained using 2D view factors taking into consideration the shading of the ground which can substantially affect the results. Also, the effect of the elevation of the module from the ground surface is examined and found that at sufficient height (≥ 1푚) the impact of ground clearance on the rear side irradiance is minimised. Finally, the ground reflected irradiance is obtained using the spectral reflectivity of different ground materials where it is shown that the use of improper albedo values can lead to inaccurate results.
The next step is the calculation of the energy yield of the bifacial module. For this, a similar methodology used to obtain the energy yield of monofacial modules in the standard IEC61853 is used. More specifically, the incident irradiance on the rear side of the module is corrected for the angle of incidence and spectrum effects to generate similar conditions as in the STC. Additionally, the operating module temperature is obtained and using the total irradiance on the front and the rear side of the module the energy yield is calculated. Finally, the energy rating of bifacial modules is determined using two different approaches. In the first approach, CSER of bifacial modules is obtained using the energy yield and the total irradiance on bifacial modules. This approach results in lower energy rating than unity but needs re-scaling of the monofacial module energy rating compared to the standard. The second approach use the energy generated from both sides of the module but only the irradiation on the front side of the module is taken into account leading to CSER values higher than one, while the energy rating of monofacial modules as obtained in the standard is used. In both approaches the energy rating of bifacial modules found to be up to 17% higher than that of monofacial depending on the bifaciality of the module and the climate conditions.
The developed model is validated using real outdoor measurements for a system located in Weurt, Eastern Netherlands. First, the in-plane irradiance on both sides of the module is obtained from the model and then, the simulated energy yield is calculated and compared to the measured energy yield of bifacial modules. The results show a small difference between the simulated and measured energy yield for the time period between October 2019 and June 2020 with a total variation of 4.65% in the total energy yield.
Modelling alkaline silicon-air batteries
A finite element model
uneconomical for this use compared to traditional hydrocarbon fired power plants. Furthermore, many battery technologies depend on scarce and expensive minerals. Recently, a battery utilizing silicon as its anode and oxygen from the air at the cathode has been proposed. This socalled silicon-air battery utilizes mainly silicon and oxygen, which are the two most common elements on earth. Furthermore, the theoretical energy density of this battery type was shown to be significantly higher than the energy density of lithium-ion batteries. Because of this, the silicon-air battery has been a growing area of research in the last years.
Battery models help to simulate batteries based on empirical data and electrochemical systems. These models are a powerful tool in the evaluation of the performance of batteries. Parameters of the battery can be altered quickly and specifically. This can provide a powerful analysis tool to determine weaknesses in a batteries. They can also help in further developing an understanding of the operating principles of the battery technology. A specific type of model is the finite element model. In this type of model the object that is modeled is divided into small pieces and for each piece a set of (partial) differential equations is evaluated. Different electrochemical, chemical, physical and mathematical models can be modelled and combined in this tool. For this thesis a finite element model of an alkaline silicon-air battery is developed in COMSOL. The model is based on an earlier model that was developed in 2020.
Besides the discharge mechanism, alkaline silicon-air batteries are subject to two secondary reactions that hinder the performance of the battery: corrosion and passivation. Corrosion consumes a large part of the silicon without contributing to the discharge. Passivation creates an oxide layer on the surface of the silicon electrode, stopping the discharge reaction. Both these reactions have been implemented in the model. Besides that, a metal contact on the silicon anode is implemented in the model. The parameters used in this model are supported by empirical values for these parameters. Finally, the model was compared to experimental results.
The simulation of the discharge of the alkaline siliconair battery was improved in several ways compared to the pre-existing model. The corrosion was shown in the simulations, although the mechanism is somewhat simplified because of the 1D nature of the model. The passivation reaction was shown in the simulations as well, and was improved on compared to the previous model by breaking it up into two steps. Using this model, experimentally observed trends could be simulated reasonably well. The simulated discharge potential was a close representation of the experimental data, although the open circuit potential was somewhat higher, and for higher current densities the potential was somewhat lower. For different electrolyte concentrations the model showed results similar to what was found in experiments. ...
uneconomical for this use compared to traditional hydrocarbon fired power plants. Furthermore, many battery technologies depend on scarce and expensive minerals. Recently, a battery utilizing silicon as its anode and oxygen from the air at the cathode has been proposed. This socalled silicon-air battery utilizes mainly silicon and oxygen, which are the two most common elements on earth. Furthermore, the theoretical energy density of this battery type was shown to be significantly higher than the energy density of lithium-ion batteries. Because of this, the silicon-air battery has been a growing area of research in the last years.
Battery models help to simulate batteries based on empirical data and electrochemical systems. These models are a powerful tool in the evaluation of the performance of batteries. Parameters of the battery can be altered quickly and specifically. This can provide a powerful analysis tool to determine weaknesses in a batteries. They can also help in further developing an understanding of the operating principles of the battery technology. A specific type of model is the finite element model. In this type of model the object that is modeled is divided into small pieces and for each piece a set of (partial) differential equations is evaluated. Different electrochemical, chemical, physical and mathematical models can be modelled and combined in this tool. For this thesis a finite element model of an alkaline silicon-air battery is developed in COMSOL. The model is based on an earlier model that was developed in 2020.
Besides the discharge mechanism, alkaline silicon-air batteries are subject to two secondary reactions that hinder the performance of the battery: corrosion and passivation. Corrosion consumes a large part of the silicon without contributing to the discharge. Passivation creates an oxide layer on the surface of the silicon electrode, stopping the discharge reaction. Both these reactions have been implemented in the model. Besides that, a metal contact on the silicon anode is implemented in the model. The parameters used in this model are supported by empirical values for these parameters. Finally, the model was compared to experimental results.
The simulation of the discharge of the alkaline siliconair battery was improved in several ways compared to the pre-existing model. The corrosion was shown in the simulations, although the mechanism is somewhat simplified because of the 1D nature of the model. The passivation reaction was shown in the simulations as well, and was improved on compared to the previous model by breaking it up into two steps. Using this model, experimentally observed trends could be simulated reasonably well. The simulated discharge potential was a close representation of the experimental data, although the open circuit potential was somewhat higher, and for higher current densities the potential was somewhat lower. For different electrolyte concentrations the model showed results similar to what was found in experiments.