avroenОмский научный вестник. Серия "Авиационно-ракетное и энергетическое машиностроение"Omsk Scientific Bulletin. Series Aviation-Rocket and Power Engineering2588-03732587-764XОмский государственный технический университет10.25206/2588-0373-2025-9-2-86-93JQDZTBavroen-85Research ArticleАВИАЦИОННАЯ И РАКЕТНО-КОСМИЧЕСКАЯ ТЕХНИКАAVIATION AND ROCKET-SPACE ENGINEERINGИсследование характеристик «безлопаточных» вентиляторов применительно к двигателям беспилотных летательных аппаратовStudy of the small multicopters bladeless propulsors characteristicshttps://orcid.org/0000-0003-3710-5116БрызгуновП. А.BryzgunovP. A.

Брызгунов Павел Александрович - ассистент кафедры инновационных технологий наукоемких отраслей Института энергоэффективности и водородных технологий НИУ «МЭИ».

111250, Москва, ул. Красноказарменная, д. 14, стр. 1

AuthorID (РИНЦ) 1069772

AuthorID (SCOPUS) 57844836600

Pavel A. Bryzgunov - Assistant of the Innovative Technologies for High-Tech Industries Department, Institute of Energy Efficiency and Hydrogen Technologies, National Research University “Moscow Power Engineering Institute” (MPEI).

Moscow, Krasnokazarmennaya st., 14, bld. 1, 111250

AuthorID (RSCI) 1069772

AuthorID (SCOPUS) 57844836600

pavel.bryzgunov@gmail.comГригоровВ. А.GrigorovV. A.

Григоров Владислав Алексеевич - инженер кафедры инновационных технологий наукоемких отраслей Института энергоэффективности и водородных технологий НИУ «МЭИ».

111250, Москва, ул. Красноказарменная, д. 14, стр. 1

Vladislav A. Grigorov - Engineer of the Innovative Technologies for High-Tech Industries Department, Institute of Energy Efficiency and Hydrogen Technologies, MPEI.

Moscow, Krasnokazarmennaya st., 14, bld. 1, 111250

grigorovva@mpei.ruГришинЛ. Е.GrishinL. E.

Гришин Леонид Евгеньевич - студент направления «Теплоэнергетика и теплотехника» кафедры инновационных технологий наукоемких отраслей Института энергоэффективности и водородных технологий НИУ «МЭИ».

111250, Москва, ул. Красноказарменная, д. 14, стр. 1

Leonid E. Grishin - Student in Thermal Engineering of the Innovative Technologies for High-Tech Industries Department, Institute of Energy Efficiency and Hydrogen Technologies, MPEI.

Moscow, Krasnokazarmennaya st., 14, bld. 1, 111250

grishinly@mpei.ruИвановаЕ. A.IvanovaE. A.

Иванова Евгения Александровна - студент направления «Энергетическое машиностроение» кафедры паровых и газовых турбин Института энергомашиностроения и механики НИУ «МЭИ».

111250, Москва, ул. Красноказарменная, д. 14, стр. 1

Evgenia A. Ivanova - Student in Power Engineering of the Steam and Gas Turbines Department, Institute of Power Engineering and Mechanics, MPEI.

Moscow, Krasnokazarmennaya st., 14, bld. 1, 111250

ivanovayeva@mpei.ruНациональный исследовательский университет «МЭИ»РоссияNational Research University “Moscow Power Engineering Institute”Russian Federation202530062025928693Copyright © Брызгунов П.А., Григоров В.А., Гришин Л.Е., Иванова Е.A., 20252025Брызгунов П.А., Григоров В.А., Гришин Л.Е., Иванова Е.A.Bryzgunov P.A., Grigorov V.A., Grishin L.E., Ivanova E.A.This work is licensed under a Creative Commons Attribution 4.0 License.https://ariem.omgtu.ru/jour/article/view/85

В работе исследованы ключевые технические характеристики «безлопаточных» движителей перспективных силовых турбовентиляторных установок для мультикоптерных беспилотных летательных аппаратов. Выявлены аспектные соотношения, обеспечивающие наибольшую тягу и тяговый КПД, проведены исследования влияния радиуса вентилятора и толщины кольцевого зазора в нем на показатели его эффективности как движителя при фиксированном расходе и длине. Установлено, что наибольшей эффективностью обладает конфигурация с радиусом 175 мм при длине 150 мм и расходе воздуха 0,3 кг/с, что обеспечивает число Маха на выходе, равное 0,42. Данная конфигурация обеспечивает тягу 44 Н, сохранение импульса скоростной струи на уровне 92 % при полном давлении на входе 17 800 Па.

The study examines the fundamental technical characteristics of bladeless propulsors intended for advanced turbofan propulsion systems in multicopter unmanned aerial vehicles. The research identifies optimal aspect ratios that maximize thrust and thrust efficiency while analyzing the impact of fan radius and annular gap thickness on propulsion efficiency under constant flow rate and length conditions. The findings indicate that the most efficient configuration features a fan radius of 175 mm, a length of 150 mm, and an air mass flow rate of 0,3 kg/s, yielding an exit Mach number of 0,42. This configuration generates a thrust of 44 N while maintaining high-speed jet momentum conservation at 92 %, under a total inlet pressure of 17,800 Pa.

эффект Коандавентилятор Дайсонабеспилотные летательные аппараты (БПЛА)тягамалая авиациягазотурбинный двигательдвижительCoanda effectDyson fanunmanned aerial vehicles (UAVs)thrustsmall aircraftenginebladeless propulsionРабота выполнена в рамках проекта «Разработка технических решений, обеспечивающих повышение эффективности авиационных газотурбинных двигателей» при поддержке гранта Национального исследовательского университета «МЭИ» на реализацию программы научных исследований «Приоритет 2030: Технологии будущего» в 2024–2026 гг.The investigation has been carried out within the framework of project “Development of technical solutions to improve the efficiency of aircraft gas turbine engines” with the support of a subvention from the National Research University “Moscow Power Engineering Institute” for implementation of the internal research program “Priority 2030: Future Technologies” in 2024–2026.ReferencesМамедов Б. Ш. Основы единой теории движителей на непрерывных потоках. Вывод формулы тяги, полетного (тягового) КПД турбореактивных двигателей // Восточно-европейский журнал передовых технологий. 2011. № 7 (52). C. 15–20. EDN: QCUGSH.Mamedov B. Sh. Osnovy edinoy teorii dvizhiteley na nepreryvnykh potokakh. Vyvod formuly tyagi, poletnogo (tyagovogo) KPD turboreaktivnykh dvigateley [Foundations of the common theory of movers on the continuous flows. calculation the formulars of thrust, flying (thrust) coefficient of usefull action of turbojet engines]. Vostochno-evropeyskiy zhurnal peredovykh tekhnologiy. Eastern-European Journal of Enterprise Technologies. 2011. No. 7 (52). P. 15–20. EDN: QCUGSH. (In Russ.).JetCat P1000-PRO – JetCat. URL: https://www.jetcat.de/en/productdetails/produkte/jetcat/produkte/Professionell/P1000 (accessed: 11.03.2025).JetCat P1000-PRO – JetCat. URL: https://www.jetcat.de/en/productdetails/produkte/jetcat/produkte/Professionell/P1000 (accessed: 11.03.2025).Gammack P. D., Frederic N., Simmonds K. J. Bladeless fan. US patent GB2452490 A; filed September 04th, 2007; published March 11th, 2009.Gammack P. D., Frederic N., Simmonds K. J. Bladeless fan. US patent GB2452490 A; filed September 04th, 2007; published March 11th, 2009.Capunay A., Valdenegro D., Masso D. A. G., Carrillo L. R. G. Bladeless unmanned aerial vehicle. US patent 20190127065A1; filed June 13th, 2018; published May 02nd, 2019.Capunay A., Valdenegro D., Masso D. A. G., Carrillo L. R. G. Bladeless unmanned aerial vehicle. US patent 20190127065A1; filed June 13th, 2018; published May 02nd, 2019.Seungjae Lee. Drone. Korean patent KR101804328B1; filed June 24th, 2016; published December 04th, 2017.Seungjae Lee. Drone. Korean patent KR101804328B1; filed June 24th, 2016; published December 04th, 2017.Lin Song. Bladeless propeller for unmanned aerial vehicle. Chinese patent CN118894253A; filed July 15th, 2024; published November 05th, 2024.Lin Song. Bladeless propeller for unmanned aerial vehicle. Chinese patent CN118894253A; filed July 15th, 2024; published November 05th, 2024.Sandeep Kumar Chintala, Sriranjan Rasakatra. Aircraft with bladeless propellers. Chinese patent CN110914151A; filed March 13th, 2018; published March 24th, 2020.Sandeep Kumar Chintala, Sriranjan Rasakatra. Aircraft with bladeless propellers. Chinese patent CN110914151A; filed March 13th, 2018; published March 24th, 2020.Weimeng C. A kind of bladeless fan-powered vertical take-off and landing drone. Chinese patent CN108263594B; filed January 31st, 2018; published May 10th, 2019.Weimeng C. A kind of bladeless fan-powered vertical take-off and landing drone. Chinese patent CN108263594B; filed January 31st, 2018; published May 10th, 2019.Sureshkumar A., Jailani H. S. A. K., Siddarth R. [et al.]. Design and analysis of bladeless thruster for an UAV applications at three different profile configurations. International Journal of Vehicle Structures and Systems. 2023. Vol. 15, no. 5. 2024. DOI: 10.22214/IJRASET.2024.62531.Sureshkumar A., Jailani H. S. A. K., Siddarth R. [et al.]. Design and analysis of bladeless thruster for an UAV applications at three different profile configurations. International Journal of Vehicle Structures and Systems. 2023. Vol. 15, no. 5. 2024. DOI: 10.22214/IJRASET.2024.62531.Xu H., Jiang L., Cao Z., Bao X. Design study of a rotorless unmanned aerial vehicle. 2023 4th International Seminar on Artificial Intelligence, Networking and Information Technology (AINIT). 2023. P. 58–62. DOI: 10.1109/AINIT59027.2023.10210723.Xu H., Jiang L., Cao Z., Bao X. Design study of a rotorless unmanned aerial vehicle. 2023 4th International Seminar on Artificial Intelligence, Networking and Information Technology (AINIT). 2023. P. 58–62. DOI: 10.1109/AINIT59027.2023.10210723.Valdenegro D., Capunay A., Gonzalez D. [et al.]. Improving safety: design and development of a bladeless thruster for autonomous multicopters. 2018 International Conference on Unmanned Aircraft Systems (ICUAS). 2018. P. 158–167. DOI: 10.1109/ICUAS.2018.8453474.Valdenegro D., Capunay A., Gonzalez D. [et al.]. Improving safety: design and development of a bladeless thruster for autonomous multicopters. 2018 International Conference on Unmanned Aircraft Systems (ICUAS). 2018. P. 158–167. DOI: 10.1109/ICUAS.2018.8453474.Mehmood K., Shahzad A., Masud J. [et al.]. Numerical analysis of bladeless ceiling fan: an effective alternative to conventional ceiling fan. Journal of Wind Engineering and Industrial Aerodynamics. 2022. Vol. 221. P. 104905. DOI: 10.1016/j.jweia.2022.104905. EDN: DIRNLG.Mehmood K., Shahzad A., Masud J. [et al.]. Numerical analysis of bladeless ceiling fan: an effective alternative to conventional ceiling fan. Journal of Wind Engineering and Industrial Aerodynamics. 2022. Vol. 221. P. 104905. DOI: 10.1016/j.jweia.2022.104905. EDN: DIRNLG.Jafari M., Afshin H., Farhanieh B., Sojoudi A. Numerical investigation of geometric parameter effects on the aerodynamic performance of a bladeless fan. Alexandria Engineering Journal. 2016. Vol. 55 (1). P. 223–233. DOI: 10.1016/J.AEJ.2015.11.001.Jafari M., Afshin H., Farhanieh B., Sojoudi A. Numerical investigation of geometric parameter effects on the aerodynamic performance of a bladeless fan. Alexandria Engineering Journal. 2016. Vol. 55 (1). P. 223–233. DOI: 10.1016/J.AEJ.2015.11.001.Aslam H., Arif M. Z., Ali M., Javed A. Design and CFD Analysis of bladeless ceiling fan. 2021 International Bhurban Conference on Applied Sciences and Technologies (IBCAST). 2021. P. 782–787. DOI: 10.1109/IBCAST51254.2021.9393254.Aslam H., Arif M. Z., Ali M., Javed A. Design and CFD Analysis of bladeless ceiling fan. 2021 International Bhurban Conference on Applied Sciences and Technologies (IBCAST). 2021. P. 782–787. DOI: 10.1109/IBCAST51254.2021.9393254.Ravi D., Rajagopal T. K. R. Numerical investigation on the effect of geometric shape and outlet angle of a bladeless fan for flow optimization using CFD techniques. International Journal of Thermofluids. 2022. Vol. 15 (28). P. 100174. DOI: 10.1016/j.ijft.2022.100174.Ravi D., Rajagopal T. K. R. Numerical investigation on the effect of geometric shape and outlet angle of a bladeless fan for flow optimization using CFD techniques. International Journal of Thermofluids. 2022. Vol. 15 (28). P. 100174. DOI: 10.1016/j.ijft.2022.100174.Jafari M., Afshin H., Farhanieh B., Bozorgasareh H. Numerical aerodynamic evaluation and noise investigation of a bladeless fan. Journal of Applied Fluid Mechanics. 2015. Vol. 8 (1). P. 133–142.Jafari M., Afshin H., Farhanieh B., Bozorgasareh H. Numerical aerodynamic evaluation and noise investigation of a bladeless fan. Journal of Applied Fluid Mechanics. 2015. Vol. 8 (1). P. 133–142.Li G., Hu Y., Jin Y. [et al.]. Influence of Coanda surface curvature on performance of bladeless fan. Journal of Thermal Science. 2014. Vol. 23 (5). P. 422–431. DOI: 10.1007/s11630-014-0725-3.Li G., Hu Y., Jin Y. [et al.]. Influence of Coanda surface curvature on performance of bladeless fan. Journal of Thermal Science. 2014. Vol. 23 (5). P. 422–431. DOI: 10.1007/s11630-014-0725-3.Joshi V., Noronha W., Ganesan V. [et al.]. Determination of optimum outlet slit thickness and outlet angle for the bladeless fan using the CFD approach. Energies. 2023. Vol. 16 (4). P. 1633. DOI: 10.3390/en16041633.Joshi V., Noronha W., Ganesan V. [et al.]. Determination of optimum outlet slit thickness and outlet angle for the bladeless fan using the CFD approach. Energies. 2023. Vol. 16 (4). P. 1633. DOI: 10.3390/en16041633.Maîtrejean G., Kempf M., Antoniali L. [et al.]. Parametric study of a bladeless fan geometry: investigating the influence of geometry parameters on discharge ratio and thrust force. DOI: 10.48550/arXiv.2406.03305.Maîtrejean G., Kempf M., Antoniali L. [et al.]. Parametric study of a bladeless fan geometry: investigating the influence of geometry parameters on discharge ratio and thrust force. DOI: 10.48550/arXiv.2406.03305.Menter F. R. Two-equation eddy-viscosity turbulence models for engineering applications. AIAA Journal. 1994. Vol. 32 (8). P. 1598–1605.Menter F. R. Two-equation eddy-viscosity turbulence models for engineering applications. AIAA Journal. 1994. Vol. 32 (8). P. 1598–1605.

The authors declare that there are no conflicts of interest present.