脉冲爆震发动机研究进展综述

IF 1.5 Q3 ENGINEERING, CHEMICAL
K. Pandey, Pinku Debnath
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引用次数: 35

摘要

脉冲爆震发动机(PDEs)是一种令人兴奋的新型推进技术。PDE的运行循环包括燃料-空气混合、燃烧、排污和净化。脉冲爆震发动机的燃烧过程是产生可靠、可重复爆震波的重要现象。在实际系统中,爆震管内爆震波起爆是多级燃烧现象的结合。爆震燃烧使燃料-空气混合物快速燃烧,比爆燃燃烧过程快一千倍。PDE利用重复的爆震波产生推进推力。本文对脉冲爆震发动机燃烧爆震模式的各种实验研究和计算分析进行了详细的综述。本文详细介绍了不同参数对脉冲爆震发动机推进性能提高的影响。可以看出,爆震管内爆震波流道的设计、爆震管出口段引射器的设计以及马赫数等工作参数的设计是提高PDE推进性能的主要原因。在本文的综述工作中,还提出了该领域的进一步研究范围。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Review on Recent Advances in Pulse Detonation Engines
Pulse detonation engines (PDEs) are new exciting propulsion technologies for future propulsion applications. The operating cycles of PDE consist of fuel-air mixture, combustion, blowdown, and purging. The combustion process in pulse detonation engine is the most important phenomenon as it produces reliable and repeatable detonation waves. The detonation wave initiation in detonation tube in practical system is a combination of multistage combustion phenomena. Detonation combustion causes rapid burning of fuel-air mixture, which is a thousand times faster than deflagration mode of combustion process. PDE utilizes repetitive detonation wave to produce propulsion thrust. In the present paper, detailed review of various experimental studies and computational analysis addressing the detonation mode of combustion in pulse detonation engines are discussed. The effect of different parameters on the improvement of propulsion performance of pulse detonation engine has been presented in detail in this research paper. It is observed that the design of detonation wave flow path in detonation tube, ejectors at exit section of detonation tube, and operating parameters such as Mach numbers are mainly responsible for improving the propulsion performance of PDE. In the present review work, further scope of research in this area has also been suggested.
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来源期刊
Journal of Combustion
Journal of Combustion ENGINEERING, CHEMICAL-
CiteScore
2.00
自引率
28.60%
发文量
8
审稿时长
20 weeks
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