TURBINE BLADES
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United States of America Patent
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Issued Date -
Apr 16, 2015
app pub date -
Jun 5, 2014
filing date -
Oct 11, 2013
priority date (Note) -
Published
status (Latency Note)
Importance
Abstract
A turbomachine apparatus for driving a compressor is disclosed. The turbomachine apparatus contains at least one rotor stage and at least one retaining element. The at least one rotor stage contains a plurality of blades and is configured to rotate about an axis. The at least one retaining element is configured to retain the at least one rotor stage with the blades thereof at least partly or wholly in radial compression during rotation thereof.
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