Transient characteristics as well as unsteady cascade flow fields of a three-stage axial flow compressor with compression plane wave injection from the compressor downstream were experimentally investigated by detail measurements of casing wall pressure fluctuations and unsteady velocity. The main feature of tested compressor is a shock tube facility connected in series to the compressor outlet duct in order to supply a compression plane wave which simulates the sudden rise of the compressor back pressure in a gas turbine system. Research attention is mainly focused on the unsteady behavior of surge and rotating stall coexistence phenomenon, and influence of the compression plane wave injection on the compressor operating conditions. When the compressor is connected to the capacity tank, surge and rotating stall occur simultaneously according to the capacitance increment of the whole compression system. The surge cycle changes irregularly with a throttling of the valve installed just behind the compressor and several different types of surge behaviors are observed. Furthermore, even though the compressor is operating under the stable condition, it goes into surge by injecting the compression plane wave.
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ASME-JSME-KSME 2011 Joint Fluids Engineering Conference
July 24–29, 2011
Hamamatsu, Japan
Conference Sponsors:
- Fluids Engineering Division
ISBN:
978-0-7918-4440-3
PROCEEDINGS PAPER
Characteristics of Surge and Rotating Stall in a Three-Stage Axial Flow Compressor Using Shock Tube
Daisuke Morita,
Daisuke Morita
Waseda University, Tokyo, Japan
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Yutaka Fujita,
Yutaka Fujita
Waseda University, Tokyo, Japan
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Eisuke Outa
Eisuke Outa
Waseda University, Tokyo, Japan
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Daisuke Morita
Waseda University, Tokyo, Japan
Yutaka Fujita
Waseda University, Tokyo, Japan
Yutaka Ohta
Waseda University, Tokyo, Japan
Eisuke Outa
Waseda University, Tokyo, Japan
Paper No:
AJK2011-22015, pp. 595-602; 8 pages
Published Online:
May 25, 2012
Citation
Morita, D, Fujita, Y, Ohta, Y, & Outa, E. "Characteristics of Surge and Rotating Stall in a Three-Stage Axial Flow Compressor Using Shock Tube." Proceedings of the ASME-JSME-KSME 2011 Joint Fluids Engineering Conference. ASME-JSME-KSME 2011 Joint Fluids Engineering Conference: Volume 1, Symposia – Parts A, B, C, and D. Hamamatsu, Japan. July 24–29, 2011. pp. 595-602. ASME. https://doi.org/10.1115/AJK2011-22015
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