Turbine exhaust strut airfoil profile

F - Mech Eng,Light,Heat,Weapons – 02 – K

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F02K 1/80 (2006.01) F01D 25/30 (2006.01) F02K 1/00 (2006.01)

Patent

CA 2611629

A turbine exhaust thin strut includes an airfoil section 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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