摘要
A six-tube air-breathing two phase pulse detonation engine (PDE) model has been developed with diameter of 200 mm and a total length of 1500 mm. Under nearly atmospheric pressure, a proof-of-principle experiment on the engine model was successfully performed by using liquid gasoline/air mixture. Each tube in the PDE model can operate at a repetition frequency up to 35 Hz with all the tubes running at the same time experimentally. Therefore a frequency up to 210 Hz was reached in the PDE model. Several ignition control strategies were developed for the multi-tube air-breathing PDE model. Some rules of how different ignition control strategies affect the engine operation have been explored. The results in the investigation supplied a technology preparation to bring PDE to production.
源语言 | 英语 |
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页(从-至) | 1935-1938 |
页数 | 4 |
期刊 | Hangkong Dongli Xuebao/Journal of Aerospace Power |
卷 | 27 |
期 | 9 |
出版状态 | 已出版 - 9月 2012 |