Experimental Study on Restart Control of A Supersonic Air-Breathing Engine

Takayuki Kojima*, Tetsuya Sato, Shujiro Sawai, Nobuhiro Tanatsugu

*この研究の対応する著者

研究成果: Article査読

22 被引用数 (Scopus)

抄録

To study the dynamic response of a supersonic airbreathing engine and establish control logic for intake unstart, restart control tests were conducted at Mach 3 using a subscale engine model consisting of an axisymmetric intake (inlet) and a turbojet. Assuming that the combustion flame is blown out by intake unstart, restart control follows a sequence. First, after a flow is started the turbojet engine is ignited. Second, the intake is started while the rotational speed and the combustion gas temperature of the core engine are controlled. Third, the intake spike position and the terminal shock position are controlled, and the intake total pressure recovery achieves the design value (60%). The tests were successful, and engine thrust was recovered at approximately 30-40 s after engine start-up. A sudden increase in combustion gas temperature and rotational speed occurred after intake unstart. To reduce the sudden increase in the gas temperature, a new sequence that involved closing a fuel control valve after detection of intake unstart was implemented, and the increase in gas temperature was reduced. To avoid intake buzz, buzz margin control using a bypass door was successfully implemented.

本文言語English
ページ(範囲)273-279
ページ数7
ジャーナルJournal of Propulsion and Power
20
2
DOI
出版ステータスPublished - 2004
外部発表はい

ASJC Scopus subject areas

  • 航空宇宙工学
  • 燃料技術
  • 機械工学
  • 宇宙惑星科学

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