Turbine blade airfoil profile

A turbine blade for a gas turbine engine has an airfoil including leading and trailing edges joined by spaced-apart pressure and suction sides to provide an external airfoil surface extending from a platform in a spanwise direction to a tip. The external airfoil surface is formed in substantial conf...

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Bibliographische Detailangaben
Hauptverfasser: Twahir, Abdulhalim, Lecuyer, Daniel, Moradi, Niloofar, Tsifourdaris, Panagiota, Menard, Jocelyn
Format: Patent
Sprache:eng
Schlagworte:
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