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

页码：651 / 660

页数：9

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