First and second stage turbine airfoil shapes

The first stage nozzles and buckets have nominal airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and R set forth in Tables I and II, respectively, and second stage nozzles and buckets have nominal airfoil profiles substantially in accordance with Cartesian coord...

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Bibliographische Detailangaben
Hauptverfasser: SULLIVAN, MICHAEL ADELBERT, LADOON, DALE W, FREDMONSKI, ADAM, CANDELA, FERRUCCIO
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung:The first stage nozzles and buckets have nominal airfoil profiles substantially in accordance with Cartesian coordinate values of X, Y and R set forth in Tables I and II, respectively, and second stage nozzles and buckets have nominal airfoil profiles substantially in accordance with Cartesian coordinate values set forth in Tables III and IV, respectively. The X, Y and R values are in millimeters. R represents distances along a radius from an axis of rotation of the turbine. For each airfoil, X and Y are distances which, when connected by smooth continuous arcs, define airfoil profile sections in planes normal to the radius at each distance R. The profile sections at the R distances for each airfoil are joined smoothly with one another to form the airfoil shape. The airfoil shapes given by the X, Y and R distances lie within envelopes of ± 4.064 millimeters in a direction normal to any airfoil surface location therealong.