Early stall warning technique for axial-flow compressors

Nobuyuki Tahara, Masahiro Kurosaki, Yutaka Ohta, Eisuke Outa, Takurou Nakajima, Tomofumi Nakakita

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22 Citations (Scopus)

Abstract

This paper proposes a unique stall risk index based on pressure signals by high-response transducers on the casing wall at the rotor leading-edge location. The aim of the research is to explore the possibility of reducing current excessive stall margin requirement for compressor design based on the worst-case scenario. The index is generated by computing correlation degradation of pressure time histories of current and one revolution before over each blade pitch. Tests conducted on a single-stage low-speed compressor exhibits that the correlation diminishes significantly with proximity to stall, and the proposed technique might have the capability of generating a stall warning signal sufficiently in advance of spike inception. Extensive experiments on a research compressor show that the degree of the index degradation depends on various factors, such as flow coefficient, tip clearance, and rotor blade incidence. In order to obtain a reliable stall warning signal in practical use, these effects must be carefully examined.

Original languageEnglish
Pages (from-to)448-456
Number of pages9
JournalJournal of Turbomachinery
Volume129
Issue number3
DOIs
Publication statusPublished - 2007 Jul 1

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ASJC Scopus subject areas

  • Mechanical Engineering

Cite this

Tahara, N., Kurosaki, M., Ohta, Y., Outa, E., Nakajima, T., & Nakakita, T. (2007). Early stall warning technique for axial-flow compressors. Journal of Turbomachinery, 129(3), 448-456. https://doi.org/10.1115/1.2447948