HP turbine blade airfoil profile
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United States of America Patent
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May 19, 2009
Grant Date -
Mar 6, 2008
app pub date -
Sep 5, 2006
filing date -
Sep 5, 2006
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A single stage high pressure turbine blade includes an airfoil having a profile substantially in accordance with at least an intermediate portion of the Cartesian coordinate values of X, Y and Z set forth in Table 2. The X and Y values are distances, which when smoothly connected by an appropriate continuing curve, define airfoil profile sections at each distance Z. The profile sections at each distance Z are joined smoothly to one another to form a complete airfoil shape.
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