Experiments in active control of stall on an aeroengine gas turbine

Journal of Turbomachinery

Volumn 120, Issue 4, 1998, Pages 637-647

  Freeman, C ^a   Wilson, A G ^a   Day, I J ^b   Swinbanks, M A ^c  

^a ROLLS ROYCE PLC   (United Kingdom)

^b UNIVERSITY OF CAMBRIDGE   (United Kingdom)

^c MAS Research Ltd   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

ACTIVE STALL CONTROL;

COMPRESSORS; CONTROL SYSTEM ANALYSIS; PRESSURE TRANSDUCERS; SCADA SYSTEMS; TURBOJET ENGINES;

GAS TURBINES;

COMPRESSOR; CONTROL METHOD; GAS TURBINE; STALL;

EID: 0032194381     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.2841773     Document Type: Article

References (10)

1. Day, I. J., 1993, “Active Suppression of Rotating Stall and Surge in Axial Compressors,” ASME Journal of Turbomachinery, Vol. 115, pp. 40-47.
2. Day, I. J., and Freeman, C., 1994, “The Unstable Behavior of Low and HighSpeed Compressors,” ASME Journal of Turbomachinery, Vol. 116, pp. 194201.
3. Eveker, K. M., Gysling, D. L., Nett, C. N., and Sharma, O. P., 1995, “Integrated Control of Rotating Stall and Surge in Aeroengines,” SPIE Vol. 2494 (Proc. Conference "Sensing, Actuation and ControlOrlando, FL, Apr. 17-18), pp. 21-35.
4. Ffowcs Williams, J. E., and Huang, X. Y., 1989, “Active Stabilisation of Compressor Surge,” Journal of Fluid Mechanics, Vol. 204, pp. 245-262.
5. Freeman, C., and Wilson, A. G., 1993, “Stall Inception and Post Stall Transients in an Aero Engine Axial Flow Compressor,” presented at IMechE Seminar on Turbo Compressor and Fan Stability, London, Apr. 8.
6. Hynes, T. P., and Greitzer, E. M., 1987, “A Method for Assessing the Effects of Inlet Flow Field Distortion on Compressor Stability,” ASME Journal of Turbomachinery, Vol. 109, pp. 371-379.
7. Ludwig, G. R., and Nenni, J. P., 1978, “A Rotating Stall Control System of Turbojet Engines,” ASME Paper No. 78-GT-115.
8. Paduano, J., Epstein, A. H., Valavani, L., Longley, J. P., Greitzer, E. M., and Guenette, G. R., 1993, “Active Control of Rotating Stall in a Low-Speed Axial Compressor,” ASME Journal of Turbomachinery, Vol. 115, pp. 48-56.
9. Wilson, A. G., and Freeman, C., 1994, “Stall Inception and Development in an Axial Flow Aeroengine,” ASME Journal of Turbomachinery, Vol. 116, pp. 217-225.
10. Wilson, A. G., 1996, “Stall and Surge in Axial Flow Compressors,” PhD Thesis submitted to Cranfield University.