Pratt-whitney Canada Corp

Silvio De Santis

Remo Marini

Edward Vlasic

Dan Olaru

Sophia Levy

A compressor turbine includes a series of compressor turbine blades each having an airfoil with 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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Boucherville, Canada

Silvio De Santis