Zero running clearance centrifugal compressor
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United States of America Patent
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Nov 2, 2010
Issued Date -
N/A
app pub date -
Dec 6, 2006
filing date -
Dec 6, 2006
priority date (Note) -
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Abstract
A turbine engine includes an engine housing enclosing: a centrifugal compressor having a rotor; at least one centrifugal compressor bore mounted to the rotor; at least one blade mounted to each of the at least one centrifugal bore and disposed proximate to at least one static wall; a turbine disposed in connection with the centrifugal compressor; a thrust bearing disposed in connection with the rotor; and means for moving said rotor with reference to the at least one static wall attached to the thrust bearing.
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