Compressor turbine blade airfoil profile

Details Compressor turbine blade airfoil profile Compressor turbine blade airfoil profile

2011-01-04

2011-01-04

Look, Edward (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

Specific blade structure

Radial flow devices

C416SDIG004, C416S243000

Reexamination Certificate

active

07862304

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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