Rotating stall suppression

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with...

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4152081, 415914, F04D 2940

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active

052979300

ABSTRACT:
Rotating stall in an axial-flow compressor is suppressed by the positioning of a fixed inlet flow divider in the annular inlet flow passage upstream of the compressor. The inlet flow divider is aligned with the flow of fluid through the duct and acts to block or interfere with any rotating wave in the inlet and thereby suppresses rotating stall in the compressor.

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Mechanics and Thermodynamics of Propulsion; Hill and Peterson; pp. 272-277; Copyright 1965.
Moore, F. K. "A Theory of Rotating Stall of Multistage Compressors: Part I--Small Disturbances," ASME J. Eng. for Power, 106, Apr. 1984, pp. 313-321.
Moore, F. K. "A Theory of Rotating Stall of Multistage Compressors: Part II--Finite Disturbances," ASME J. Eng. for Power, 106, Apr. 1984, pp. 321-326.
Moore, F. K. & Greitzer, E. M., "A Theory of Post-Stall Transients on Axial Compression Systems: Part I--Development of Equations," ASME J. Eng. for Gas Turb, and Power, 108, Jan. 1986; pp. 68-76.
Moore, F. K., "Stall Transients of Axial Compression Systems with Inlet Distortion," AIAA J. of Propulsion of Power, Nov./Dec. 2, 6, 1986; pp. 552-561.

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