Pneumatic Damper Multicriteria Optimization in the Free-Piston Stirling Engine Displacer
Авторы: Bobylev A.V., Zenkin V.A. | Опубликовано: 01.07.2022 |
Опубликовано в выпуске: #2(141)/2022 | |
Раздел: Энергетическое машиностроение | Рубрика: Тепловые двигатели | |
Ключевые слова: stirling engine, Beale engine, free-piston engines, mathematical model, thermodynamic model, pneumatic damper, multicriteria optimization |
Abstract
The free-piston Stirling engine is a complex self-oscillating system, which parameters should be strictly coordinated with each other to ensure the unit operability. One of such coordination tasks is to ensure the balance of energy input to and output from the engine displacer. In this case, energy output depends on the dissipative forces, and energy output is provided by the displacer rod and depends on its diameter. The need to select rod diameter complicates and slows down the engine design. In addition, the system possible instability could lead to the engine racing. To solve this problem, it is proposed to install a pneumatic damper on the displacer rod ensuring the dissipative forces growth with an increase in the displacer amplitude above its nominal value. Thermodynamic model was created to evaluate the damper characteristics and select its parameters. MATLAB software package was used as the development environment. The system of differential equations was integrated using the Runge --- Kutta family method. The damper multicriteria optimization problem was formalized, and two objective functions with five independent parameters were compiled. Optimization was performed using the genetic algorithm, and the Pareto front was built. To evaluate results of the work performed, the damper mathematical model was integrated into the Stirling engine mathematical model, and the working process was calculated with selected damper parameters. It is demonstrated that the developed pneumatic damper prevents an increase in the displacer oscillation amplitude ensuring system stability and reducing time for the unit design
Please cite this article as:
Bobylev A.V., Zenkin V.A. Pneumatic damper multicriteria optimization in the free-piston Stirling engine displacer. Herald of the Bauman Moscow State Technical University, Series Mechanical Engineering, 2022, no. 2 (141), pp. 89--100. DOI: https://doi.org/10.18698/0236-3941-2022-2-89-100
Литература
[1] Oriti S.M. Performance measurement of Advanced Stirling Convertors (ASC-E3). AIAA, 2013, art. 2013-3813. DOI: https://doi.org/10.2514/6.2013-3813
[2] Wilson S. Overview of heat addition and efficiency predictions for an Advanced Stirling Convertor. AIAA, 2011, art. 2011-5576. DOI: https://doi.org/10.2514/6.2011-5576
[3] Loktionov Yu.V., Myagkov L.L., Obolonnyy I.V., et al. [Prospects for using of free-piston power linear units for energy conversion in aerospace systems]. Aktual’nye voprosy proektirovaniya avtomaticheskikh kosmicheskikh apparatov dlya fundamental’nykh i prikladnykh nauchnykh issledovaniy [Actual Problems of Designing Automatic Spacecraft for Fundamental and Applied Scientific Research]. Khimki, NPO im. S.A. Lavochkina Publ., 2017, pp. 504--511 (in Russ.).
[4] Loktionov Yu.V., Myagkov L.L., Obolonnyy I.V., et al. [Linear free-piston units and new critically technologies for piston engines]. Dvigatel’-2017 [Engine-2017]. Moscow, Bauman MSTU Publ., 2017, pp. 53--54 (in Russ.).
[5] Valenti G., Silva P., Fergnani N., et al. Experimental and numerical study of a micro-cogeneration Stirling engine for residential applications. Energy Procedia, 2014, vol. 45, pp. 1235--1244. DOI: https://doi.org/10.1016/j.egypro.2014.01.129
[6] Masato K., Keiichiro Y., Teruyuki A. Development of zero emission generating system "Stirling Engine". Yanmar Technical Review, 2017.
[7] Holliday E., Keiter D. Sunpower non-dissipative free piston Stirling engine control electronics for dual-opposed 130We power system for army battery charger. AIAA, 2006, art. 2006-4188. DOI: https://doi.org/10.2514/6.2006-4188
[8] Hendrickson M., Podlesak T.F., Huth J., et al. Stirling engines for military applications. AIAA, 2005, art. 2005-5519. DOI: https://doi.org/10.2514/6.2005-5519
[9] Lyons V., Scott J. An overview of space power systems for NASA missions. AIAA, 2007, art. 2007-4734. DOI: https://doi.org/10.2514/6.2007-4734
[10] De la Bat J. G., Dobson R. Theoretical simulation, design and manufacture, and experimental evaluation of a free piston Stirling engine electric generator. AIAA, 2018, art. 2018-4502. DOI: https://doi.org/10.2514/6.2018-4502
[11] Walker G., Senft J.R. Free Piston Stirling Engines XIV. Lecture Notes in Engineering, vol. 12. Springer-Verlag Berlin Heidelberg, 1985.
[12] Wood J.G., Buffalino A., Holliday E., et al. Free-piston Stirling power conversion unit for fission surface power, phase I final report. NASA, 2010.
[13] Brakhman T.R. Mnogokriterial’nost’ i vybor al’ternativy v tekhnike [Multi-criteria and choice of alternatives in technology]. Moscow, Radio i svyaz’ Publ., 1984.
[14] Fourman M.P. Compaction of symbolic layout using genetic algorithms. Proc. 1st Int. Conf. on Genetic Algorithms, 1985, pp. 141--153.
[15] Hajela P., Lin C.Y. Genetic search strategies in multicriterion optimal design. Struct. Optim., 1992, vol. 4, no. 2, pp. 99--107. DOI: https://doi.org/10.1007/BF01759923
[16] Horn J., Nafpliotis N., Goldberg D.E. A niched Pareto genetic algorithm for multiobjective optimization. Proc. First IEEE Conf. on Evolutionary Computation, 1994, pp. 82--87. DOI: https://doi.org/10.1109/ICEC.1994.350037
[17] Srinivas N., Deb K. Muiltiobjective optimization using nondominated sorting in genetic algorithms. Evol. Comput., 1994, vol. 2, no. 3, pp. 221--248. DOI: https://doi.org/10.1162/evco.1994.2.3.221
[18] Lotov A.V., Pospelova I.I. Mnogokriterial’nye zadachi prinyatiya resheniy [Multi-criteria decision-making problems]. Moscow, Maks-Press Publ., 2008.
[19] MATLAB software. mathworks.com: website. Available at: https://www.mathworks.com/products/matlab.html (accessed: 01.01.2021).
[20] Zenkin V.A., Valiullin A.N., Bobylev A.V. Dynamic model of the external heat engine of the spacecraft power system. AIP Conf. Proc., 2019, vol. 2171, no. 1, art. 040004. DOI: https://doi.org/10.1063/1.5133190