| 2016, 02 February |
|
DOI: 10.14489/td.2016.02.pp.040-045 Posadov V.V., Slobodskoy D.A., Posadova O.L., Kuchin V.A. Abstract. Modern gas turbine engines often contain lowemission combustion chambers with lean airfuel mixtures. It can cause vibratory combustion that is accompanied by thermal and vibrational loads on combustion chamber elements. Therefore, diagnostics of vibratory combustion is an urgent problem. This paper presents diagnostics of vibratory combustion in combustion chamber of aircraft gas turbine engine during bench tests by recording of vibration and airflow pressure pulsations. Computational and experimental methods are used for diagnostics. Modal analysis shows that it is necessary to shift natural frequencies of flame tube parts out of rotor operational speed range. Keywords: vibratory combustion, combustion chamber, gas turbine engine, natural frequency.
V. V. Posadov, D. A. Slobodskoy, O. L. Posadova, V. A. Kuchin
1. Gerasimenko V. P., Nalesnyi N. B. (2006). Mechanisms of vibration combustion in the combustion chambers. Aviatsionno-kosmicheskaia tekhnika i tekhnologiia. KhAI, 29(3), pp. 48-52.
This article is available in electronic format (PDF). DOI: 10.14489/td.2016.02.pp.040-045 Copy the article DOI and follow the link https://id-spektr.ru/product/pokupka-elektronnoy-stati-iz-zhurnala-kontrol-diagnostika Please specify the article DOI in the order comments.
|

Разработка концепции и создание сайта - ООО «Издательский дом «СПЕКТР»