Micro Gas Turbine Engine for Unmanned Aerial Vehicles

V. A. Sychenkov; A. S. Limanskii; W. M. Yousef; V. V. Ankudimov; S. S. Seyid Jafari

doi:10.3103/S1068799819040160

Micro Gas Turbine Engine for Unmanned Aerial Vehicles

Авторы: Sychenkov V.¹, Limanskii A.¹, Yousef W.¹, Ankudimov V.¹, Seyid Jafari S.¹
Учреждения:
1. Tupolev Kazan National Research Technical University
Выпуск: Том 62, № 4 (2019)
Страницы: 651-660
Раздел: Aircraft and Rocket Engine Design and Development
URL: https://journals.rcsi.science/1068-7998/article/view/231176
DOI: https://doi.org/10.3103/S1068799819040160
ID: 231176

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Аннотация

The results of development and manufacture of a micro gas turbine engine for an unmanned aerial vehicle are presented. The calculation features of the main elements of the engine blading section, namely, a centrifugal compressor, a reverse-flow combustor, and a radial-axial turbine are considered. The design of the inlet and output duct, rotor bearings, and lubrication system is described.