Micro Gas Turbine Engine for Unmanned Aerial Vehicles

被引：0
|
作者：
Sychenkov V.A. [1 ]
Limanskii A.S. [1 ]
Yousef W.M. [1 ]
Ankudimov V.V. [1 ]
Seyid Jafari S.S. [1 ]
机构：
[1] Tupolev Kazan National Research Technical University, ul. Karla Marksa 10, Kazan, 420111, Tatarstan
来源：
Russian Aeronautics | 2019年 / 62卷 / 04期
关键词：
centrifugal compressor; micro gas turbine engine; radial-axial turbine; reverse-flow combustor; turbocharger; unmanned aerial vehicle;
D O I：
10.3103/S1068799819040160
中图分类号：
学科分类号：
摘要：
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. © 2019, Allerton Press, Inc.
引用
收藏
页码：651 / 660
页数：9
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