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An axial flow or centrifugal flow compressor having arrays of blades (16) extending across a working medium flowpath (18) includes a casing treatment for enhancing the compressor's fluid dynamic stability. In one variant of the invention the casing treatment comprises one or more circumferentially e

An axial flow or centrifugal flow compressor having arrays of blades (16) extending across a working medium flowpath (18) includes a casing treatment for enhancing the compressor's fluid dynamic stability. In one variant of the invention the casing treatment comprises one or more circumferentially extending grooves (40) that each receive indigenous fluid from the compressor flowpath at a fluid extraction site (56) and discharge indigenous fluid into the flowpath at a fluid injection site (58), circumferentially offset from the extraction site, where the migrated fluid is better able to advance against an adverse pressure gradient in the flowpath. Each groove is oriented so that the discharged fluid enters the flowpath with a streamwise directional component that promotes efficient and reliable integration of the introduced fluid into the flowpath fluid stream (20). In a second variant of the invention, the casing treatment comprises a circumferentially extending compartment (62), typically comprising a voluminous pressure compensation chamber (64) and a single passage (66) circumferentially coextensive with the chamber, for establishing fluid communication between the chamber and the flowpath. The voluminous character of the compartment attenuates the inordinate circumferential pressure difference across the tips of excessively loaded compressor blades (16), making the compressor less susceptible to tip vortex induced instabilities. One embodiment of the pressure compensating variant includes a passage (66) oriented similarly to the groove (40) of the grooved variant of the casing treatment so that fluid flowing from the passage enters the flowpath with a streamwise directional component.

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[ We claim:] [1.]1. A fluid compressor, comprising:a blade array rotatable about a rotational axis, each blade of the array having a root, a tip, a leading edge, a trailing edge and a projected tip chord, each blade spanning a fluid flowpath that channels a stream of fluid through the compressor;a c

[ We claim:] [1.]1. A fluid compressor, comprising:a blade array rotatable about a rotational axis, each blade of the array having a root, a tip, a leading edge, a trailing edge and a projected tip chord, each blade spanning a fluid flowpath that channels a stream of fluid through the compressor;a casing having a flowpath surface circumscribing and spanwisely spaced from the blade tips, the casing having a circumferentially extending groove in fluid communication with the flowpath for receiving fluid from the flowpath at a fluid extraction site and for discharging fluid into the flowpath at a fluid injection site circumferentially offset from the extraction site;the groove being defined at least in part by an upstream wall and a downstream wall, both walls extending to and adjoining the flowpath surface at respective upstream and downstream lips, the lips forming a mouth of the groove, the upstream wall being oriented at an acute angle relative to the adjoining flowpath surface, and the downstream wall being oriented at an obtuse angle relative to the adjoining flowpath surface so that the discharged fluid enters the flowpath with a streamwise directional component. [15.]15. A method of augmenting fluid flow stability of a compressor, the compressor having a blade array rotatable about an axis, each blade of the array extending across a flowpath that channels a stream of fluid through the compressor, each blade also having a blade tip, the compressor also having a casing with a flowpath surface spaced apart from and circumscribing the blade tips, the fluid stream having a circumferentially nonuniform, streamwisely adverse pressure gradient, the method comprising:diverting indigenous fluid from the flowpath at an extraction site circumferentially aligned with a relatively high flowpath fluid pressure ;directing the indigeneous fluid circumferentially to an injection site circumferentially aligned with a relatively low flowpath fluid pressure ; anddischarging the indigenous fluid into the flowpath at the injection site so that the discharged fluid enters the flowpath with a streamwise directional component.16. A method of augmenting fluid flow stability of a compressor, the compressor having a blade array rotatable about an axis, each blade of the array extending across a flowpath that channels a stream of fluid through the compressor, each blade also having a blade tip a pressure surface and a suction surface, the compressor also having a casing with a flowpath surface spaced apart from and circumscribing the blade tips, the fluid stream having a circumferentially nonuniform, streamwisely adverse pressure gradient, the method comprising:diverting indigenous fluid from the flowpath at an extraction site circumferentially aligned with a relatively high circumferential pressure difference across a blade tip;directing the indigeneous fluid circumferentially to an injection site circumferentially aligned with a flowpath fluid pressure lower than the flowpath fluid pressure adjacent the pressure surface of the blade at the extraction site; anddischarging the indigenous fluid into the flowpath at the injection site so that the discharged fluid enters the flowpath with a streamwise directional component.17. A fluid compressor, comprising:a blade array rotatable about a rotational axis, each blade of the array having a root, a tip, a leading edge a trailing edge, a suction surface extending from the leading edge to the trailing edge, a pressure surface spaced from the suction surface and also extending from the leading edge to the trailing edge and a projected chord, each blade spanning a fluid flowpath that channels a stream of fluid through the compressor; anda casing having a flowpath surface circumscribing and spanwisely spaced from the blade tips, the casing including a compartment with a passage that extends to the flowpath at a location axially proximate the blade tips, the compartment comprising a circumferentially extending chamber and a single passage circumferentially coextensive with the chamber, the passage having a slot connecting the passage to the chamber and a mouth connecting the passage to the flowpath, the passage being defined at least in part by an upstream wall and a downstream wall each having a surface roughness of at least about 75 AA microinches, both walls extending to and adjoining the flowpath surface at respective upstream and downstream lips bordering the passage mouth, the compartment having a volume sufficiently large to attenuate circumferential pressure differences across the blade tip and to keep fluid pressure within the compartment approximately circumferentially uniform during normal operation of the compressor thereby attenuating circumferential variation in flowpath pressure and resisting vorticity induced fluid dynamic instabilities.18. The fluid compressor of claim 17 wherein the surface roughness is between about 300 AA microinches and about 400 AA microinches.