Compressor stator vane
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United States of America Patent
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Jan 26, 2010
Grant Date -
Sep 1, 2005
app pub date -
Apr 18, 2005
filing date -
Feb 22, 2002
priority date (Note) -
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status (Latency Note)
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Abstract
A vane unit system having a plurality of vane units having at least one air foil projecting from a base. The base has a hole which receives a pin which extends between adjacent bases of vane units therein forming a rigid ring of vanes that are less susceptible to vane motion caused by pressure fluctuations within the compressor of a gas turbine. A blade assembly tool having a shape to fit within the slot in a casing that receives the vane units allows for the installation of vane units with interlocking pins without the necessity of having to remove the rotor from the casing.
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