Improvement of aircraft GTE emission characteristics by using the microflame fuel combustion in a shortened combustion chamber

被引：0

作者：

Markushin A.N. ^{[1
]}

Baklanov A.V. ^{[1
]}

Tsyganov N.E. ^{[2
]}

机构：

[1] OAO KMPO, Kazan

[2] Tupolev Kazan National Research Technical University, Kazan

来源：

Russian Aeronautics (Iz VUZ) | 2013年 / 56卷 / 4期

关键词：

combustion chamber; design; microflame combustion; toxicity;

D O I：

10.3103/S1068799813040132

中图分类号：

学科分类号：

摘要：

We present the design of an upgraded shortened combustion chamber with the reduced emission of NOx and CO. Also shown are the results of experimental studies of the developed design effect on main characteristics of the GTE combustion chamber. © 2013 Allerton Press, Inc.

引用

页码：401 / 406

页数：5

共 5 条

[1]

Gritsenko E.A., Lavrov V.N., Postnikov A.M., Tsybizov Y., Basic Lines in Improving GTE Combustion Chambers, Vestnik SGAU. Ser. Protsessy Goreniya, Teploobmena i Ekologii Teplovykh Dvigatelei (Processes of Combustion, Heat Exchange and Ecology of Heat Engines), 2, pp. 5-9, (1999)

[2]

Markushin A.N., Merkushin N.A., Byshin V.M., Baklanov A.V., Arrangement of Low-Emission Combustion in the Annular GTE Combustion Chamber, Izv. Vuz. Av. Tekhnika, 52, 3, pp. 70-72, (2009)

[3]

Markushin A.N., Baklanov A.V., Some Features of Burning Process Organization in the Shortened Combustion Chambers of Converted Aircraft Gas Turbine Engines, Vestnik Dvigatelestroeniya, pp. 170-173, (2012)

[4]

Danil'Chenko V.P., Lukachev S.V., Kovylov Y., Proekrirovanie Aviatsionnykh Gazoturbinnykh Dvigatelei (Design of Aircraft Gas Turbine Engines), (2008)

[5]

Lefebvre A.H., Gas Turbine Combustion, (1983)

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