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Figure 3.2: The meridional plane view of a typical centrifugal compressor. This exaggerated view is probably not to scale for any real compressor design. Flow enters at the impeller inlet, sometimes called the inducer. The term inducer identifies the portion of the rotor whose blade passage is at the inlet, before radius has begun to increase. The impeller turns along the axis, and flow exits the impeller into a vaneless space. Sometimes the vaneless space is formed with two parallel plates and sometimes the plates diverge. In the Real Gas Radial Compressor (RGRC) code, the vaneless space is always of constant depth in the axial direction. Beyond the vaneless space is typically a vaned diffuser, which serves to slow down the flow and raise the static pressure of the fluid. It is a circular plate of metal that has vanes inside it which direct the flow, such that the flow area of the passage increases as radius increases. Figure 3.3 shows a view of a straight-vaned diffuser looking along the axis of rotation. In RGRC the vanes can be curved by the user up to 25o. This just means that the angle of the vane with respect to the radial direction will be 25o greater at the diffuser outlet than it is at the diffuser inlet. The area ratio of a diffuser refers to the ratio of the outlet flow area to the throat flow area. 47PDF Image | Supercritical Carbon Dioxide Cycle Analysis
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