Integration of a High-Pressure Gas Turbine of the Gas Turbine Engine with a Gas-Dynamic Laser

被引：0

作者：

Perel’shtein B.K. ^{[1
]}

Osipov B.M. ^{[1
]}

Titov A.V. ^{[1
]}

机构：

[1] Kazan State Power Engineering University, ul. Krasnosel’skaya 51, Kazan

来源：

Russian Aeronautics | 2018年 / 61卷 / 4期

关键词：

aircraft gas turbine engine; gas-dynamic laser; integration; super-reaction turbine;

D O I：

10.3103/S1068799818040293

中图分类号：

学科分类号：

摘要：

引用

页码：687 / 691

页数：4

共 12 条

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[3] Vovk M.Y., Marchukov E.Y., Petrienko V.G., Perel'shtein B.K., RU Patent 2587509, Byul. Izobr., (2016)
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[5] Perel'shtein B.K., New Energy Systems, (2015)
[6] Osipov B.M., Kopelevich L.A., Perel'shtein B.K., To Creating of Integrated Laser Systems for Civil Aircraft Protection from Terrorist Attacks, Sbornik trudov 5i nauchno-tekhnicheskoi konf. prepodavatelei, nauchnykh rabotnikov i aspirantov s mezhdunarodnym uchastiem “Aktual’nye problemy i perspektivy razvitiya grazhdanskoy aviatsii (Proc. 5th Scien.-Tech. Conf. of Academicians, Scientists, and Postgraduate Students “Actual Problems and Prospects of the Civil Aviation Development”), (2016)
[7] Osipov B.M., Titov A.V., Perel'shtein B.K., Investigation of Performance of the Turboshaft Gas Turbine Engine With the Working Medium Bleeding for the Gas-Dynamic Laser Functioning, Vestnik KGTU im. A.N.Tupoleva, 3, pp. 65-68, (2016)
[8] Osipov B.M., Kopelevich L.A., Perel'shtein B.K., Study of Performance of the Aircraft Gas Turbine Engine Integrated with a Gas Dynamic Laser, Izv. Vuz. Av. Tekhnika, 60, 3, pp. 143-146, (2017)
[9] Apollonov V., Laser Weapon in the US and Russia: Science and Defense
[10] Makarov V.N., Losev S.A., Gas-Dynamic Lasers at Low Initial Temperatures, Pis’ma v Zhurnal Tekhnicheskoi Fiziki, pp. 78-81, (1996)

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