TURBOMACHINERY
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United States of America
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Issued Date -
Feb 27, 2020
app pub date -
Feb 22, 2019
filing date -
Feb 22, 2019
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Abstract
A turbomachine (105) configured to compress supercritical carbon dioxide is shown. The turbomachine comprises, in fluid flow series, an inlet (201), an inducerless radial impeller (202) having a plurality of blades, a fully vaneless diffuser (203), and a volute (204) comprising a tongue and having a flow area at the tongue equal to that of the diffuser.
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