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Publishing Language: Chinese | Open Access

Test verification of multi-point injection air and ethanol gas generator

Fang ZHAO1,2Zebin REN1,2Fei WANG1Yu SHI1Xianfeng LI1( )Zhifeng LUO3
Facility Design and Instrumentation Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, China
AECC Sichuan Gas Turbine Establishment, Mianyang 621300, China
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Abstract

In order to effectively solve the shortcomings of the existing gas ejection source, as well as meet the needs of large mass flowrate and miniaturization of an injection system, a gas generator with multi-point injection structure using air and alcohol as propellants was developed based on the comprehensive analysis of various gas injection source schemes, and the experimental research under various working conditions was carried out. Research results show as bellows: the multi-point injection scheme greatly improves the space utilization rate, which effectively meets the miniaturization requirements of ejection system. Spray performance is good, and the spray cone angle and particle diameter are superior to the index requirements. Ignition reliability is high, which solves the shortcomings of low ignition reliability of the existing gas generator in the field. The operation curve indicates a rapid ignition, stable combustion and uniform temperature field of gas generator. The excess air coefficient range for stable operation is 2.52~4.34, showing a wide mass flow-rate range. In addition, efficient film cooling on the combustion liner inner wall effectively ensures the long time operation of the gas generator.

CLC number: V231.2; TK223.2 Document code: A Article ID: 1001-2486(2023)02-045-08

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Journal of National University of Defense Technology
Pages 45-52

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Cite this article:
ZHAO F, REN Z, WANG F, et al. Test verification of multi-point injection air and ethanol gas generator. Journal of National University of Defense Technology, 2023, 45(3): 45-52. https://doi.org/10.11887/j.cn.202303005

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Received: 16 June 2021
Published: 28 June 2023
© 2023 Journal of National University of Defense Technology

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).