07306436 is referenced by 35 patents and cites 63 patents.

A single stage high pressure turbine blade includes an airfoil 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.

Title
HP turbine blade airfoil profile
Application Number
11/366015
Publication Number
7306436 (B2)
Application Date
March 2, 2006
Publication Date
December 11, 2007
Inventor
Constantinos Ravanis
Brossard
CA
Sami Girgis
Montréal
CA
Agent
Ogilvy Renault
Assignee
Pratt & Whitney Canada
CA
IPC
F01D 5/14
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