AIRFOIL SECTION FOR TURBINE BUCKET AND TURBINE INCORPORATING THE SAME
PROBLEM TO BE SOLVED: To provide an airfoil section for a turbine bucket and a turbine with the same incorporated therein. SOLUTION: Third stage turbine buckets (24) have airfoil section 34 profiles substantially in accordance with Cartesian coordinate values of X, Y and Z' set forth in Table I...
Gespeichert in:
Hauptverfasser: | , , , , |
---|---|
Format: | Patent |
Sprache: | eng |
Schlagworte: | |
Online-Zugang: | Volltext bestellen |
Tags: |
Tag hinzufügen
Keine Tags, Fügen Sie den ersten Tag hinzu!
|
Zusammenfassung: | PROBLEM TO BE SOLVED: To provide an airfoil section for a turbine bucket and a turbine with the same incorporated therein. SOLUTION: Third stage turbine buckets (24) have airfoil section 34 profiles substantially in accordance with Cartesian coordinate values of X, Y and Z' set forth in Table I wherein X and Y values are in inches and the Z' values are non-dimensional values from 0 to 1 convertible to Z distances in inches by multiplying the Z' values by the height of the airfoil section in inches. The X and Y values are distances which, when connected by smooth continuing arcs, define airfoil section profile cross sections at each distance Z. The profile cross sections at each distance Z are joined smoothly to one another to form a complete airfoil section. The X, Y and Z distances may be scalable as a function of the same constant or number to provide a scaled up or scaled down airfoil section cross section for the bucket. The nominal airfoil section given by the X, Y and Z distances lies within an envelope of ±0.060 inches in directions vertical to the surface of the airfoil section. COPYRIGHT: (C)2009,JPO&INPIT |
---|