Novel Hybrid Ice Protection System Combining Thermoelectric System and Synthetic Jet Actuator

No AccessTechnical NotesNovel Hybrid Ice Protection System Combining Thermoelectric System and Synthetic Jet ActuatorShengke Yang, Xian Yi, Qiling Guo, Chunhua Xiao, Zhenbing Luo and Yan ZhouShengke YangChina Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China*Engineer, Key Laboratory of Icing and Anti/De-Icing; .Search for more papers by this author, Xian YiChina Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China†Professor, Key Laboratory of Icing and Anti/De-Icing; .Search for more papers by this author, Qiling GuoChina Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China‡Assistant Engineer, Key Laboratory of Icing and Anti/De-Icing; .Search for more papers by this author, Chunhua XiaoChina Aerodynamics Research and Development Center, 621000 Mianyang, People’s Republic of China§Professor, Key Laboratory of Icing and Anti/De-Icing; .Search for more papers by this author, Zhenbing LuoNational University of Defense Technology, 410073 Changsha, People’s Republic of China¶Professor, College of Aerospace Science and Engineering; .Search for more papers by this author and Yan ZhouNational University of Defense Technology, 410073 Changsha, People’s Republic of China**Lecturer, College of Aerospace Science and Engineering; .Search for more papers by this authorPublished Online:8 Dec 2020https://doi.org/10.2514/1.J059906SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Gent R. W., Dart N. P. and Cansdale J. T., “Aircraft Icing,” Philosophical Transactions of the Royal Society of London, Series A: Mathematical, Physical and Engineering Sciences, Vol. 358, No. 1776, 2000, pp. 2873–2911. https://doi.org/10.1098/rsta.2000.0689 CrossrefGoogle Scholar[2] Valarezo W. O., Lynch F. T. and McGhee R. J., “Aerodynamic Performance Effects due to Small Leading-Edge Ice(Roughness) on Wings and Tails,” Journal of Aircraft, Vol. 30, No. 6, 1993, pp. 807–812. https://doi.org/10.2514/3.46420 LinkGoogle Scholar[3] Gao T., Luo Z., Zhou Y., Liu Z., Peng W., Cheng P. and Den X., “Novel Deicing Method Based on Plasma Synthetic Jet Actuator,” AIAA Journal, Vol. 58, No. 9, 2020, pp. 4181–4188. https://doi.org/10.2514/1.J059352 LinkGoogle Scholar[4] Thomas S. K., Cassoni R. P. and MacArthur C. D., “Aircraft Anti-Icing and De-Icing Techniques and Modeling,” Journal of Aircraft, Vol. 33, No. 5, 1996, pp. 841–854. https://doi.org/10.2514/3.47027 LinkGoogle Scholar[5] Chang S. N., Yang B., Leng M. Y., Zhao Y. Y. and Liu M. Y., “Study on Bleed Air Anti-Icing System of Aircraft,” Journal of Aerospace Power, Vol. 32, No. 5, 2017, pp. 1025–1034. https://doi.org/10.13224/j.cnki.jasp.2017.05.001 Google Scholar[6] Venna S. V., Lin Y. and Botura G., “Piezoelectric Transducer Actuated Leading Edge De-Icing with Simultaneous Shear and Impulse Forces,” Journal of Aircraft, Vol. 44, No. 2, 2007, pp. 509–515. https://doi.org/10.2514/1.23996 LinkGoogle Scholar[7] Pourbagian M. and Habashi W. G., “Aero-Thermal Optimization of In-Flight Electro-Thermal Ice Protection Systems in Transient De-Icing Mode,” International Journal of Heat and Fluid Flow, Vol. 54, Aug. 2015, pp. 167–182. https://doi.org/10.1016/j.ijheatfluidflow.2015.05.012 CrossrefGoogle Scholar[8] Meng X., Hu H., Li C., Abbasi A. A., Cai J. and Hu H., “Mechanism Study of Coupled Aerodynamic and Thermal Effects Using Plasma Actuation for Anti-Icing,” Physics of Fluids, Vol. 31, No. 3, 2019, Paper 037103. https://doi.org/10.1063/1.5086884 CrossrefGoogle Scholar[9] Wei B., Wu Y., Liang H., Chen J., Zhao G., Tian M. and Xu H., “Performance and Mechanism Analysis of Nanosecond Pulsed Surface Dielectric Barrier Discharge Based Plasma Deicer,” Physics of Fluids, Vol. 31, No. 9, 2019, Paper 091701. https://doi.org/10.1063/1.5115272 Google Scholar[10] Budinger M., Pommier-Budinger V., Bennani L., Rouset P., Bonaccurso E. and Dezitter F., “Electromechanical Resonant Ice Protection Systems: Analysis of Fracture Propagation Mechanisms,” AIAA Journal, Vol. 56, No. 11, 2018, pp. 4412–4422. https://doi.org/10.2514/1.J056663 LinkGoogle Scholar[11] Zhou W., Liu Y., Hu H., Hu H. and Meng X., “Utilization of Thermal Effect Induced by Plasma Generation for Aircraft Icing Mitigation,” AIAA Journal, Vol. 56, No. 3, 2018, pp. 1097–1104. https://doi.org/10.2514/1.J056358 LinkGoogle Scholar[12] Liu Y., Kolbakir C., Hu H. and Hu H., “A Comparison Study on the Thermal Effects in DBD Plasma Actuation and Electrical Heating for Aircraft Icing Mitigation,” International Journal of Heat and Mass Transfer, Vol. 124, Sept. 2018, pp. 319–330.https://doi.org/10.1016/j.ijheatmasstransfer.2018.03.076 CrossrefGoogle Scholar[13] Calay R. K., Holdo A. E., Mayman P. and Lun I., “Experimental Simulation of Runback Ice,” Journal of Aircraft, Vol. 34, No. 2, 1997, pp. 206–212. https://doi.org/10.2514/2.2173 LinkGoogle Scholar[14] Huang X., Tepylo N., Pommier-Budinger V., Budinger M., Bonaccurso E., Villedieu P. and Bennani L., “A Survey of Icephobic Coatings and Their Potential Use in a Hybrid Coating/Active Ice Protection System for Aerospace Applications,” Progress in Aerospace Sciences, Vol. 105, No. 1, 2019, pp. 74–97. https://doi.org/10.1016/j.paerosci.2019.01.002 Google Scholar[15] Al-Khalil K., Ferguson T. and Phillips D., “A Hybrid Anti-Icing Ice Protection System,” 35th Aerospace Sciences Meeting and Exhibit, AIAA Paper 1997-0302, 1997. https://doi.org/10.2514/6.1997-302 LinkGoogle Scholar[16] Al-Khalil K., “Thermo-Mechanical Expulsive Deicing System-TMEDS,” 45th AIAA Aerospace Sciences Meeting and Exhibit, AIAA Paper 2007-0692, 2007. https://doi.org/10.2514/6.2007-692 LinkGoogle Scholar[17] Fortin G., Adomou M. and Perron J., “Experimental Study of Hybrid Anti-Icing Systems Combining Thermoelectric and Hydrophobic Coatings,” SAE TP 2011-38-0003, Warrendale, PA, 2011. https://doi.org/10.4271/2011-38-0003 CrossrefGoogle Scholar[18] Strobl T., Adam R., Tuschter M., Tuschter D., Thompson D. and Hornung M., “Feasibility Study of a Hybrid Ice Protection System Based on Passive Removal of Residual Ice,” 53rd AIAA Aerospace Sciences Meeting, AIAA Paper 2015-0032, Jan. 2015. https://doi.org/10.2514/6.2015-0032 LinkGoogle Scholar[19] Strobl T., Storm S., Thompson D. and Hornung M., “Feasibility Study of a Hybrid Ice Protection System,” Journal of Aircraft, Vol. 52, No. 6, 2015, pp. 2064–2076. https://doi.org/10.2514/1.C033161 LinkGoogle Scholar[20] Wang J. and Wu J., “Aerodynamic Performance Improvement of a Pitching Airfoil via a Synthetic Jet,” European Journal of Mechanics—B/Fluids, Vol. 83, No. 4, 2020, pp. 73–85. https://doi.org/10.1016/j.euromechflu.2020.04.009 Google Scholar[21] Amitay M., Smith D. R., Kibens V., Parekh D. E. and Glezer A., “Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators,” AIAA Journal Vol. 39, No. 3, 2001, pp. 361–370. https://doi.org/10.2514/2.1323 LinkGoogle Scholar[22] Wang L., Feng L., Wang J. and Li T., “Characteristics and Mechanism of Mixing Enhancement for Noncircular Synthetic Jets at Low Reynolds Number,” Experimental Thermal and Fluid Science, Vol. 98, No. 11, 2018, pp. 731–743. https://doi.org/10.1016/j.expthermflusci.2018.06.021 Google Scholar[23] Luo Z., Deng X., Xia Z., Wang L. and Gong W., “Flow Field and Heat Transfer Characteristics of Impingement Based on a Vectoring Dual Synthetic Jet Actuator,” International Journal of Heat and Mass Transfer, Vol. 102, No. 11, 2016, pp. 18–25. https://doi.org/10.1016/j.ijheatmasstransfer.2016.06.003 Google Scholar[24] Nikisha N., Golubev V. and Nakhla H., “On Icing Control Using Thermally Activated Synthetic Jets,” AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, AIAA Paper 2013-0093, 2013. https://doi.org/10.2514/6.2013-93 Google Scholar[25] FAA, “Part 25 Airworthiness Standards: Transport Category Airplanes,” Federal Aviation Regulations, 2003. Google Scholar[26] FAA, “Pilot Guide: Flight in Icing Conditions,” Federal Aviation Regulations, 2007. Google Scholar[27] Shinkafi A. and Lawson C., “Enhanced Method of Conceptual Sizing of Aircraft Electro-Thermal De-Icing System,” International Journal of Aerospace and Mechanical Engineering, Vol. 8, No. 6, 2014, pp. 1065–1072. https://doi.org/10.5281/zenodo.2661308 Google Scholar[28] Goodfellow S., Yarusevych S. and Sullivan P., “Momentum Coefficient as a Parameter for Aerodynamic Flow Control with Synthetic Jets,” AIAA Journal, Vol. 51, No. 3, 2013, pp. 623–631. https://doi.org/10.2514/1.J051935 LinkGoogle Scholar[29] Amitay M., Smith D., Kibens V., Parekh D. E. and Glezer A., “Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators,” AIAA Journal, Vol. 39, No. 3, 2001, pp. 361–370.https://doi.org/10.2514/2.1323 LinkGoogle Scholar[30] Chiatto M., Palumbo A. and de Luca L., “Design Approach to Predict Synthetic Jet Formation and Resonance Amplifications,” Experimental Thermal and Fluid Science, Vol. 107, No. 10, 2019, pp. 79–87. https://doi.org/10.1016/j.expthermflusci.2019.05.013 Google Scholar[31] He W., Luo Z., Deng X. and Xia Z., “Experimental Investigation on the Performance of a Novel Dual Synthetic Jet Actuator-Based Atomization Device,” International Journal of Heat and Mass Transfer, Vol. 142, No. 10, 2019, pp. 1–14. https://doi.org/10.1016/j.ijheatmasstransfer.2019.07.056 Google Scholar[32] Gallas Q., Holman R., Nishida T., Carroll B., Shelplak M. and Cattafesta L., “Lumped Element Modeling of Piezoelectric-Driven Synthetic Jet Actuators,” AIAA Journal, Vol. 41, No. 2, 2003, pp. 240–247. https://doi.org/10.2514/2.1936 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byThe Potential of Using Vortex Tube to Ameliorate Aircraft Environmental Control SystemWeiwei Chen, Zibing Luo, Xinjun Li, Xiaoming Tan, Jingzhou Zhang , Xiande Fang and Yevhenii Shkvar21 February 2023 | AIAA Journal, Vol. 0, No. 0Determining Region of Installation of Flat-Ended Piezoelectric De-Icing Actuators on Curved SurfacesBo Miao , Wen Li, Lang Yuan and Chunling Zhu6 July 2022 | Journal of Aircraft, Vol. 60, No. 1Design of the Thermoelectric Ice Protection System for a Tiltrotor ApplicationAlessandro Zanon and Michele De Gennaro21 April 2022 | Journal of Aircraft, Vol. 59, No. 5 What's Popular Volume 59, Number 4April 2021 CrossmarkInformationCopyright © 2020 by the American Institute of Aeronautics and Astronautics, Inc. 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TopicsActuatorsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsAviationAviation SafetyAviation Weather HazardsAvionicsGuidance, Navigation, and Control SystemsThermal EffectsThermoelectric EffectThermophysics and Heat TransferWind Tunnels KeywordsPiezoelectric ActuatorsIce Protection SystemThermoelectric SystemAnti Icing SystemAerodynamic CharacteristicsIcing ConditionsEnergy ConsumptionSupercoolingResonance FrequenciesIcing Wind TunnelAcknowledgmentsThis work was supported by the National Natural Science Foundation of China (grant numbers 11572338, 11872374, 12002377, and 51809271) and the Open Fund of the Key Laboratory of Icing and Anti/De-Icing (grant number 1901IADL20190401).PDF Received20 June 2020Accepted2 November 2020Published online8 December 2020