Turbomachine having swirl-inhibiting seal
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United States of America Patent
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Jul 19, 2016
Grant Date -
Jul 24, 2014
app pub date -
Jan 21, 2013
filing date -
Jan 21, 2013
priority date (Note) -
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status (Latency Note)
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Abstract
Various embodiments include a turbomachine including a swirl-inhibiting seal. In various particular embodiments, a turbomachine includes: a rotor section having sets of axially disposed blades; a diaphragm section at least partially surrounding the rotor section, the diaphragm section including a set of nozzles positioned between adjacent sets of axially disposed blades, wherein the set of nozzles includes at least one nozzle having: a base section coupled to the diaphragm section; a blade coupled to the base section; and a radial tip section coupled to a radial end of the blade, the radial tip section including an axially extending flange having a slot extending therethrough for controlling fluid flow within the turbomachine.
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