Passive structural and aerodynamic control of compressor surge

Pumps – With muffler acting on pump fluid

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417540, 417542, 137568, F04B 1100

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active

051998564

ABSTRACT:
A compressor or pump is connected to a discharge plenum. The plenum includes a movable wall whose motion varies the volume of the plenum. The wall is connected to passive elements forming a spring-mass-damper system whose characteristics are selected to damp pressure fluctuations in the plenum which would give rise to pumping system instabilities. In another aspect of the invention, a compressor is connected to a discharge plenum which in turn is connected to an exit throttle. The throttle includes a movable portion whose motion varies the throttle area. The movable portion is connected to passive elements forming a spring-mass-damper system selected to damp pressure fluctuations in the plenum. In another embodiment, the plenum communicates with a fixed area throttle and a variable area throttle. The variable area throttle includes a movable portion connected to passive elements selected to damp pressure fluctuations in the plenum. Aerodynamic surge control is effected by coupling a second Helmholtz resonator to the plenum.

REFERENCES:
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patent: 2198021 (1940-04-01), Wood
patent: 2316278 (1943-04-01), Orsmansky, Jr.
patent: 3487855 (1970-01-01), Lautenberger, Jr.
patent: 4177649 (1979-12-01), Venema
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patent: 4449358 (1984-05-01), Mani
patent: 4504188 (1985-03-01), Traver et al.
Bodine, A. G., "Sonic Control of Dynamic Compressor Instability", Symposium on Compressor Stall, Surge and System Response, 21-22 (May 1960).
Epstein, A. H., "Active Suppression of Compressor Instabilities", AIAA 10th Aeroacoustics Conference (Jul. 9-11, 1986).
Epstein, A. H., "Smart engine components: A micro inevery blade?", Aerospace America, 60-64 (Jan. 1986).
Venema, H. J., "Surge Suppression in an Inverter Driver Motor Compressor System", no date (not published).

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