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New Approach to Radial Compressor Return Channel Design

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Abstract

The design and optimisation of a vaneless diffuser, cross-over and return channel of a multistage radial compressor is presented. Special attention is given to the extension of the vanes upstream of the cross-over.

These unconventional vanes are designed by a new 3D procedure that is based on the equations for irrotational flow and accounts for meridional curvature and difference in contour length at hub and shroud. The flow analysis by means of a 3D Navier Stokes solver indicates a substantial improvement of the performance by eliminating part of the flow separation inside the cross-over.

The geometry is further optimised by means of a 3D inverse design method to obtain a smooth Mach number distribution along the vanes at hub and shroud. It resulted in a performance improvement by suppressing also the separation on the return vanes.

3D Navier Stokes analysis also shows a direct impact of lean on secondary flows and a performance increase by introducing negative lean.

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Abbreviations

b :

vane height

c :

reference length

C p :

pressure recovery coefficient

m :

meridional coordinate

m :

mass flow

P :

pressure

R :

radius

s :

curvilinear coordinate

W :

velocity

z :

number of vanes

β :

blade angle (measured from radial)

δ th :

blade thickness

θ :

angular coordinate

ρ :

density

ω :

total pressure loss coefficient

bl :

blade

fl :

flow

LE:

leading edge

m:

meridional component

TE:

trailing edge

th :

thickness

ps:

pressure side

ss:

suction side

2:

impeller exit — diffuser inlet

3:

return channel exit

is :

isentropic

-:

average value

o :

total conditions

s :

static conditions

References

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© 2004 Springer-Verlag Berlin Heidelberg

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Veress, Á., Van den Braembussche, R. (2004). New Approach to Radial Compressor Return Channel Design. In: Vad, J., Lajos, T., Schilling, R. (eds) Modelling Fluid Flow. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-08797-8_27

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  • DOI: https://doi.org/10.1007/978-3-662-08797-8_27

  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-06034-2

  • Online ISBN: 978-3-662-08797-8

  • eBook Packages: Springer Book Archive

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