
Izabela Batista Henriques
Linhas de Pesquisa
- • Termodinâmica
- • Análise exergética
- • Sistemas energéticos
Publicações (26)
Simulation and performance analysis of thermoelectric coolers for aircraft electronics
de Paula, Thales Roger Alves , Salles, Everton Luiz , Henriques, Izabela Batista
Mostrar resumo Ocultar resumo
© 2025 Elsevier LtdThis work explores the use of thermoelectric coolers (TECs) for managing the temperature of aircraft electronics. TECs offer advantages over traditional compressor-based systems, including compactness, lower weight, and the capability to cool below ambient temperatures, making them ideal for aerospace applications. A novel method for estimating thermoelectric coefficients was developed, leveraging optimization to improve accuracy. Simulation models were created using Amesim to predict TEC performance under varying conditions and validated through laboratory experiments, achieving a maximum steady-state error of 1.97 °C. Simulations under flight conditions demonstrated the system's effectiveness in maintaining electronics enclosure temperatures well below limits. With a constant 12 V supply, the load temperature stayed under 40 °C during the flight, dropping below 30 °C by the end. However, heat dissipation increased significantly, averaging 573 W, with peaks up to six times the load's thermal dissipation when no voltage control was applied. These results confirm the feasibility of TECs for aerospace thermal management, particularly for electronics requiring strict temperature control.
Exergy-based assessment of airfoil drag
Gianei, Vitor Filipe Belan , Malatesta, Vinicius , Henriques, Izabela Batista
Mostrar resumo Ocultar resumo
© The Author(s), under exclusive licence to The Brazilian Society of Mechanical Sciences and Engineering 2025.Optimizing the energy conversion processes within aircraft and developing novel aircraft configurations have become imperative for fostering a more sustainable aviation sector. Exergy analysis emerges as a valuable tool in pinpointing areas for improvement and evaluating innovative configurations. The present work intends to expand upon the exergy concept in the assessment of airfoil aerodynamics. This is achieved through drag breakdown and flow field analysis utilizing the exergetic method. The study employs computational fluid dynamics analysis, utilizing the airfoil NACA 0012 for subsonic compressible flow and NACA 2315, NACA 2312, and NACA 2309 for transonic compressible flow as test cases to illustrate the concept. Rates of exergy destruction and a thorough flow field analysis are presented along the wake downstream of the airfoil, comparing four turbulence models. The theoretical exergy method is juxtaposed with the classical near-field method and validated through technical reports. Ultimately, the findings indicate a potential for improvement using the exergy method in aerodynamics, resulting in a 12% reduction in drag in a 2D flow field, translating into potential energy savings up to 31000 W. Furthermore, it is also demonstrated that the impact of airfoil thickness variation on exergy destruction in the transonic regime is found to be negligible.
Exergoenvironmental analysis of a hybrid electric soybeans column dryer
Rohden, Gerhard Egewarth , Henriques, Izabela Batista , Bringhenti, Cleverson
Mostrar resumo Ocultar resumo
© 2024 Elsevier LtdThe global increase in food demand drives the need for efficient and sustainable agricultural practices, particularly in the energy-intensive process of grain drying, which is crucial for maintaining product quality. This study proposes the exergetic and environmental analysis of a hybrid electric column dryer for soybeans, comparing its performance across four distinct national contexts: Paraguay, Brazil, the United States, and China. The aim is to explore how different energy matrices and degrees of hybridization influence the energy and environmental costs associated with soybean drying. In addition to considering different energy matrices, the present study advances beyond previous research by coupling the mathematical drying model with thermodynamic analysis. By integrating these aspects, it is possible to conduct thorough simulations and gain insights into the exergetic, environmental, and economic impacts of the drying process. For this, a computational model was developed capable of simulating the drying process of soybeans and determining the conditions of grains and air at the exit of the drying chamber and, thus, performing the First and Second Law analyses with different degrees of hybridization for four countries with different electricity mixes. Results reveal that for thin-layer soybean drying dynamics at T = 80 °C and v = 0.5 m/s, approximately 68.2 min were needed to reduce grain moisture content from 18% w.b (0.22 d.b) to 14% (0.163 d.b), with outlet temperatures of θ = 67.57 °C for grains and T = 71.7 °C for air. The final water content of the drying air was 0.021 kgw/kga. Exergetic cost analysis revealed significant variations among countries, with Paraguay exhibiting the greatest difference between completely fossil and purely electrical cases (433.5 kJ/kgg). Environmental cost analysis showed substantial differences in electrical energy use for drying, particularly in countries with predominantly renewable energy matrices. Paraguay showed the highest emissions variation with a purely electrical system, differing by 27.55 gCO2/kgg compared to the pure fossil case. Brazil, the United States, and China had differences of 25.33, 17.4, and 11.90 gCO2/kgg, respectively. From an economic standpoint, hybridization was found to be unfeasible in Brazil due to high electricity prices, while theoretically favorable in China, Paraguay, and the United States. Paraguay had the lowest drying cost at 2.63 US$/tong, followed by China, the United States, and Brazil with 3.92, 4.74, and 15.79 US$/tong, respectively. These analyses underscore the importance of comprehensive studies in evaluating process hybridization. Considering electricity mix composition and reliable life cycle analysis data is crucial for obtaining meaningful results. Integrated exergetic, environmental, and economic analyses are essential for guiding energy use decision-making processes.
Assessment of Thermal Runaway propagation in lithium-ion battery modules with different separator materials
Silva, Gabriel Menezes da , Lima, Thiago José , Silva, Dayvis Dias da , Henriques, Izabela Batista
Mostrar resumo Ocultar resumo
© 2023 Elsevier Masson SASThe current work aims to understand and model thermal runaway (TR) events in lithium-ion (LIB) 18650 cells within the context of aircraft battery applications. The primary goal is to comprehend the phenomenon and discuss strategies for mitigating its consequences during aircraft operation. TR is modeled using Arrhenius kinetic equations and is implemented in both lumped parameters (Matlab SimulinkTM), and 3D CFD simulations (Ansys FluentTM) using User Defined Functions. To validate the thermochemical model, cells are initially simulated in an oven test, where a cell is exposed to a temperature-controlled atmosphere, triggering exothermic reactions. With a strong correlation between lumped parameters and 3D models, the latter is simulated under battery module installation conditions. An internal short-circuit is then implemented within the cell to observe how thermal runaway is triggered by an internal heat source. The trigger cell is subsequently placed in a battery module assembly to assess the dominant heat transfer modes and the likelihood of TR induction from one cell to its neighbors. This work's main objective and innovation are to compare different materials in which cells are immersed while observing the main heat transfer parameters for each material. Three conditions are tested: ceramic paper fiber and G7 as solid separators, and no separator material, where air fills the gaps between cells. The analysis of heat transfer modes reveals radiation's dominance in the case of air interstice, suggesting the possibility of using a special coating to reduce the cell surface emissivity as an alternative to decrease the likelihood of TR propagation. Thus, two values of surface emissivity were tested in the case of air. Considering a cell triggered by an internal short-circuit, a thermal runaway temperature spike is not observed in any of the four cases. However, the air interstice case with regular emissivity is the most critical one, with the closest cell reaching peak temperatures as high as 136 °C in 490 s. The ceramic paper fiber is considered the best separator material, as it postpones the temperature increase in the closest cell while also being lighter than G7. The results and discussions concerning heat propagation presented herein can serve as guidelines for developing strategies to mitigate thermal runaway in battery modules.
Assessment of different more-electric and hybrid-electric configurations for long-range multi-engine aircraft
Gimenez, Felipe Rivabem , Mady, Carlos Eduardo Keutenedjian , Henriques, Izabela Batista
Mostrar resumo Ocultar resumo
© 2023 Elsevier LtdIn this study, the characteristics, penalties, gains, and challenges in the electrification and hybridization process for long-range aircraft were investigated. A system and mission analysis was conducted on thermodynamics and cost. A reference aircraft was compared with other more-electric and hybrid-electric versions of the same type. These latter versions may carry batteries to supply the aircraft system and/or engine. A state-of-the-art propulsion and system architecture were also implemented in these innovative aircraft. A full factorial analysis was conducted to vary the battery energy density and the hybridization ratio for the hybrid configurations. A typical mission profile was developed to match the boundary conditions in all cases. The hybrid powertrains were confirmed in our results as exhibiting superior behavior compared to those of the other cases. The least efficient hybrid configuration, which employed an intermediate battery choice, reduced fuel consumption by 10.7% in the conventional aircraft and by 1% in the battery-powered more-electric type. Moreover, both baseline models were surpassed by the worst intermediate-battery hybrid aircraft by 3.6% and 1% in terms of overall mission exergy efficiency. Considering the actual low density of batteries available on the market, long-range hybrid-electric aircraft will require substantial time to become viable.
Thermodynamic-Dynamic coupling of a Stirling engine for space exploration
de Moura, Ermerson F. , Henriques, Izabela B. , Ribeiro, Guilherme B.
Mostrar resumo Ocultar resumo
© 2022 Elsevier LtdAs the new space era advances, there is an increasing demand for long-term missions beyond Earth's orbit, such as on Mars and the Moon. The level of complexity of these missions is higher than conventional missions in terms of duration, particularly the energy demand required. To become viable, power generation systems must have a high power density, that is, high power associated with low mass. From this perspective, dynamic nuclear power generation systems coupled with electric propulsion are considered the most promising systems for deep-space exploration and colonization missions. Thus, to provide valuable information for the development of a dynamic energy conversion system for space, this study carried out thermodynamic modeling of a nuclear-powered Stirling cycle coupled with a dynamic engine model for space purposes. By means of numerical modeling, the constructive parameters of the Stirling engine, such as regenerator efficiency, compression ratio, heat exchanger thermal conductance, engine frequency, piston stroke, and area, are varied to understand the impact of these parameters on the final system performance. The results show that the regenerator efficiency can provide significant gains in the engine efficiency. However, a very high regenerator efficiency reduces the power of the cycle. The engine compression ratio tends to increase the engine efficiency, but a compression ratio above six provides marginal gains for cycle efficiency. From the results obtained, the best parameters yielded a system with a power output of 260.5 kW and a power density of 35.38 kg∙kW-1. This study can serve as a theoretical guideline for the future design of nuclear-powered Stirling engines for space applications, providing insight into the constructive parameters that influence the overall performance of the system.
A novel design-point computational program for thermal power plants applications: energy, exergy and economic (3E) analysis
Costa, Fabíola Paula , Bringhenti, Cleverson , Henriques, Izabela Batista , Tomita, Jesuino Takachi , Kapat, Jayanta Sankar
Mostrar resumo Ocultar resumo
© 2022, The Author(s), under exclusive licence to The Brazilian Society of Mechanical Sciences and Engineering.For a long time, thermal power plants play important roles in world electricity and are expected to continue, at least, in the next decades. However, the finitude of fossil fuel sources leads to the crucial need for improving the existing power generation systems. In this study, an in-house computational code was developed and validated to evaluate the energy, exergy and economic performance for thermal power plants applications. Based on operating data of an actual lignite coal-fired steam power plant, two cycles were designed and compared. In the cycle in which more components were added, the fuel consumption was 9.44% lower to produce the same amount of power, making more effective use of the fuel resource. This substantial reduction in fuel consumption reflected lower electricity average costs for this plant. Comparing to the electricity price of a country using the same type of fuel, it was found that it could be lower by 1.62 percentage points for household consumers. Although the higher costs with capital investment and operational and maintenance (O&M) due to the addition of these components, the attractive economic performance of the cycle reduces the annual fuel costs and offsets the increase in capital and O&M costs.
Preface
Elmegaard, Brian , Sciubba, Enrico , Blanco-Marigorta, Ana Maria , de Gran Canaria, Palmas , Jensen, Jonas Kjær , Markussen, Wiebke Brix , Meesenburg, Wiebke , Kofler, René , Rasmussen, Mette Carmen , Amano, Yoshiharu , Arnas, Ozer , Ayalon, Ofira , Bazzo, Edson , Bedecarrats, Jean Pierre , Beyene, Asfaw , Marigorta, Ana María Blanco , Desideri, Umberto , Favrat, Daniel , Feidt, Michel , Frangopoulos, Christos , Franquet, Erwin , Gaggioli, Richard A. , Hernandez-Guerrero, Abel , Kalogirou, Soteris , Karellas, Sotirios , Kirova-Yordanova, Zornitza , Kolenda, Zygmund , Lazzaretto, Andrea , Lee, Young Duk , Lior, Noam , Lund, Henrik , Manfrida, Giampaolo , Maréchal, François , Morosuk, Tatiana , Nebra, Silvia , de Oliveira, Silvio , Poredoš, Alojz , Quoilin, Sylvain , Reini, Mauro , Stanek, Wojciech , Stefanovic, Gordana , Stevanovic, Vladimir , Stouffs, Pascal , Stougie, Lydia , Teixeira, José Carlos , Teixeira, Senhorinha F.C.F. , Tsatsaronis, George , Capilla, Antonio Valero , Verda, Vittorio , Yokoyama, Ryohei , Zevenhoven, Ron , Zhang, Na , Ziebik, Andrzej , Zoughaib, Assaad , Akisawa, Atsushi , Amano, Yoshiharu , Kermani, Nasrin Arjomand , Arkar, Ciril , Arteconi, Alessia , Henriques, Izabela Batista , Bella, Gino , Benato, Alberto , Kanbur, Baris Burak , Burin, Eduardo Konrad , Bühler, Fabian , Cabrera-Santana, Pedro Jesús , Capata, Roberto , Capone, Martina , Carraro, Gianluca , Charalampidis, Antonios , De Paepe, Michel , Desai, Nishith Babubhai , Ema, Carmen , Ferrari, Lorenzo , Ferreira, Ana C. , Florez-Orrego, Daniel , Fujii, Yasumasa , Försterling, Sven , Gallego, Antonio , Gallo, Waldyr , Gibout, Stephane , SÁnchez, Juan Manuel Gonzalez CaballÍn , Guelpa, Elisa , Gullo, Paride , Gutiérrez-Trashorras, Antonio José , Haglind, Fredrik , Hernandez-Gonzalez, Sergio Manuel , Höges, Christoph , Ilic, Milica , Juarez-Robles, Daniel
Thermal Modeling of Electric Motors Used in Very Small Size Soccer Robots
Miguel, Guilherme Reis , Maximo, Marcos R.O.A. , Henriques, Izabela Batista
Mostrar resumo Ocultar resumo
© 2022 IEEE.This paper presents a study of the thermophysical properties of electric motors and of the structure of the robots used by ITAndroids' Very Small Size (VSS) team. To perform the modeling of the robot structure, the General Lumped Capacitance Analysis was used, assuming that the motor's internal temperature can be considered approximately uniform. This hypothesis was validated by means of Biot's Number, and the heat source term was evaluated in order to define which energy dissipation sources would be considered in the modeling. The obtained model was evaluated through numerical simulations to analyze the motors' temperature profile for different current values. We compared the obtained results with similar experiments found in the literature, concluding that the model could predict the system's behavior in a satisfactory manner. Therefore, this work contributes to the research area by providing a model able to predict the temperature of the electric motor under different workloads, thus, allowing the team to anticipate its overheating and prevent its premature burnout.
Finite-time thermodynamics and exergy analysis of a Stirling engine for space power generation
de Moura, Ermerson F. , Henriques, Izabela B. , Ribeiro, Guilherme B.
Mostrar resumo Ocultar resumo
© 2021 Elsevier LtdIn recent years, the interest of space agencies and private companies in space exploration has increased, mainly in deep space missions. This type of mission poses great challenges due to the high energy level demanded from the power systems, requiring a more efficient and compact energy conversion system. Thus, this work carried out a finite-time thermodynamic model and exergy analysis of a Stirling cycle for nuclear space power generation. The thermodynamic model was coupled to a simple dynamic Stirling engine model and takes into account several aspects such as the thermal losses between the hot and cold side of the Stirling cycle, finite-time regeneration, temperature drop along heat pipes, and variable compression ratio. The system performance and component irreversibilities were evaluated by varying the nuclear core temperature and the cold side temperature of the cycle. Then, the figure of merit mass per power output (kg.kW-1) of the energy conversion system was computed, enabling the model to find temperature conditions for a system that aligns high efficiency and compactness. The results showed that the component with the greatest irreversibility is the reactor core with a value of 496.14 kJ, representing 68.18% of the total irreversibility. The exergy analysis showed that only 5.15% of the total exergy is used for power generation and 24.33% is rejected to space. Moreover, the cold side temperature of 352 K provided the system with the lowest value of mass per power output (87.69 kg.kW-1).
Nenhuma publicação encontrada
Orientações (4 mestrado, 0 doutorado)
Ramana Heringer Fernando Amaral (2025) Mestrado
Márcio Augusto Silveira Buratti (2022) Mestrado
Gerhard Egewarth Rohden (2022) Mestrado
Vitor Filipe Gianei Belan (2022) Mestrado
