• Title/Summary/Keyword: 저압축회전수

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Effects of Axial Flow Compressor Surge on the Performance in Turbofan Engine (터보팬 엔진의 축류압축기 서지가 엔진성능에 미치는 영향)

  • Oh, Chang-Yong;Koo, Ja-Ye
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.05a
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    • pp.236-239
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    • 2008
  • This thesis has analyzed the effect of the surge happening in flight on the engine performance of the PW4000 turbofan engine. EPR is judged to be the most highly sensitive parameter responding when surge occurs. Both N1 rpm and N2 rpm decreases almost simultaneously just like an EPR. During the take-off rolling, the N1 vibration is more sensitive than the N2 vibration. Consequently, the surge can be detected by EGT increase, while the other parameters decrease.

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