07329093 is referenced by 25 patents and cites 63 patents.

First stage stator vanes for a turbine comprised airfoil profile substantially in accordance with Cartesian coordinate values of X, Y and Z set forth in inches in Table I, which define a plurality of radially spaced profile sections forming the nominal profile. The Z coordinate values for each profile section are radial distances from the turbine axis to a portion of the surface of revolution about the axis containing the profile section. The X and Y values for each profile section are coordinate values which, when connected by smooth continuing arcs define the airfoil profile section along the surface of revolution portion. The radially spaced profile sections are joined smoothly with one another to form the nominal airfoil profile.

Title
Nozzle blade airfoil profile for a turbine
Application Number
11/340577
Publication Number
7329093 (B2)
Application Date
January 27, 2006
Publication Date
February 12, 2008
Inventor
Brian P Arness
Simpsonville
SC, US
Sze Bun Brian Chan
Greer
SC, US
Linda J Farral
Greenville
SC, US
Peter C Selent
Taylors
SC, US
John E Greene
Greenville
SC, US
Thomas W Vandeputte
Simpsonville
SC, US
Agent
Nixon & Vanderhye PC
Assignee
General Electric Company
NY, US
IPC
F01D 9/00
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