Multistage centrifugal compressor
First Claim
1. A multistage centrifugal compressor comprising a shaft rotatably on an axis, a plurality of centrifugal impeller means fixed on said shaft each having an outlet at a periphery thereof, conduit means for connecting said impeller means to form a fluid compression path for fluid undergoing multi-stage compression by said impeller means from a suction side to a delivery side of the compressor, said conduit means including a plurality of diffuser means arranged radially outwardly from impeller means, each impeller means and associated diffuser means constituting a stage of the centrifugal compressor, said diffuser means including at least two vaned diffusers provided with vanes having leading edges at inlet ends thereof a first one of said at least two vaned diffusers has a ratio of diffuser vane leading edge radius to impeller outlet radius larger than a ratio of diffuser vane leading radius to impeller outlet radius ratio of a second of said at least two vaned diffusers, and wherein the second of said at least two vaned diffusers is closer along said fluid compression path to the delivery side of the compressor than said first one of said at least two vaned diffusers.
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Abstract
A multistage centrifugal compressor has a shaft rotatable on an axis and a plurality of centrifugal impellers fixed on the shaft and having outlets at outer peripheries thereof. Conduits connect the impellers to from a path for fluid undergoing multi-stage compression by the impellers from a suction side to a delivery side. The conduits including a plurality of diffusers arranged radially outwardly from the impellers, each impeller and associated diffuser constituting a stage. At least two of the diffusers are vaned diffusers provided with vanes having leading edges at their inlet ends. To provide high efficiency combined with low risk of rotating stalls, among the vaned diffusers, the ratio of diffuser vane leading edge radius to impeller outlet radius increases along the fluid path from the delivery of the compressor to the suction side.
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Citations
18 Claims
- 1. A multistage centrifugal compressor comprising a shaft rotatably on an axis, a plurality of centrifugal impeller means fixed on said shaft each having an outlet at a periphery thereof, conduit means for connecting said impeller means to form a fluid compression path for fluid undergoing multi-stage compression by said impeller means from a suction side to a delivery side of the compressor, said conduit means including a plurality of diffuser means arranged radially outwardly from impeller means, each impeller means and associated diffuser means constituting a stage of the centrifugal compressor, said diffuser means including at least two vaned diffusers provided with vanes having leading edges at inlet ends thereof a first one of said at least two vaned diffusers has a ratio of diffuser vane leading edge radius to impeller outlet radius larger than a ratio of diffuser vane leading radius to impeller outlet radius ratio of a second of said at least two vaned diffusers, and wherein the second of said at least two vaned diffusers is closer along said fluid compression path to the delivery side of the compressor than said first one of said at least two vaned diffusers.
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12. A multi-stage centrifugal compressor comprising a plurality of centrifugal impeller means fixed on a rotary shaft to provide a plurality of compression stages and a diffuser means at each of said stages with at least two of said diffuser means being vaned diffusers, and wherein at least at one of adjacent pairs of stages having vaned diffusers, a ratio of a vane of the vaned diffusers leading edge radius to an outlet radius of the impeller means is larger at a stage of said adjacent pairs which is closer to the a suction side of the compressor.
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13. A multi-stage centrifugal compressor having a shaft rotatable on an axis, a plurality of centrifugal impeller means fixed on said shaft and having outlets at outer peripheries thereof, conduit means for connecting said impeller means to form a path for fluid undergoing multi-stage compression by said impeller means from a suction side to a delivery side of the compressor, said conduit means including a plurality of diffuser means arranged radially outwardly from the impeller means, each of said impeller means and associated diffuser means constituting a stage of the compressor, said diffuser means including at least two vaned diffusers provided with vanes having leading edges at inlet ends thereof, and wherein each of said vaned diffusers and associated impeller means have the following relationships:
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space="preserve" listing-type="equation">h/R≦
0.04, and
space="preserve" listing-type="equation">r/R≦
1+3.3 h/R,wherein; h=an axial height of the vanes, R=an impeller means outlet radius, and r=a diffuser vane leading edge radius. - View Dependent Claims (14, 15, 16, 17, 18)
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Specification