Compressor turbine blade airfoil profile

Details Compressor turbine blade airfoil profile Compressor turbine blade airfoil profile

2008-07-14

2011-10-18

Estrada, Michelle (Department: 2829)

Fluid reaction surfaces (i.e., impellers)

Specific blade structure

Concave surface

C416SDIG004

Reexamination Certificate

active

08038411

ABSTRACT:
A 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 1. 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 arc joined smoothly to one another to form a complete airfoil shape.

REFERENCES:
patent: 6398489 (2002-06-01), Burdgick et al.
patent: 6832897 (2004-12-01), Urban
patent: 6854961 (2005-02-01), Zhang et al.
patent: 6910868 (2005-06-01), Hyde et al.
patent: 7513749 (2009-04-01), Duong et al.
patent: 2003/0017052 (2003-01-01), Frost et al.
patent: 2003/0021680 (2003-01-01), Bielek et al.
patent: 2005/0079061 (2005-04-01), Beddard
patent: 2008/0240924 (2008-10-01), Kizuka et al.
patent: 2008/0273984 (2008-11-01), Liang et al.
U.S. Appl. No. 11/366,018, filed Mar. 2, 2006, Girgis et al.
U.S. Appl. No. 11/366,025, filed Mar. 2, 2006, Girgis et al.
U.S. Appl. No. 11/366,020, filed Mar. 2, 2006, Girgis et al.
U.S. Appl. No. 11/366,015, filed Mar. 2, 2006, Girgis et al.
U.S. Appl. No. 11/366,026, filed Mar. 2, 2006, Girgis et al.
U.S. Appl. No. 11/514,987, filed Sep. 5, 2006, Marini et al.
U.S. Appl. No. 11/514,983, filed Sep. 5, 2006, Ravanis et al.
U.S. Appl. No. 11/514,990, filed Sep. 5, 2006, Tsifourdaris et al.
U.S. Appl. No. 11/514,989, filed Sep. 5, 2006, Girgis et al.
U.S. Appl. No. 11/514,972, filed Sep. 5, 2006, Mah et al.
U.S. Appl. No. 11/470,416, filed Sep. 6, 2006, Trindade et al.
U.S. Appl. No. 11/516,598, filed Sep. 7, 2006, Papple et al.
U.S. Appl. No. 11/516,601, filed Sep. 7, 2006, Sleiman et al.
U.S. Appl. No. 11/516,599, filed Sep. 7, 2006, Sreekanth et al.
U.S. Appl. No. 11/563,839, filed Nov. 28, 2006, Marini et al.
U.S. Appl. No. 11/563,808, filed Nov. 28, 2006, Ravanis et al.
U.S. Appl. No. 11/563,801, filed Nov. 28, 2006, Kidikian et al.
U.S. Appl. No. 11/563,797, filed Nov. 28, 2006, Kidikian et al.
U.S. Appl. No. 11/563,783, filed Nov. 28, 2006, Kidikian et al.
U.S. Appl. No. 11/562,604, filed Nov. 22, 2006, Mohan et al.
U.S. Appl. No. 11/562,556, filed Nov. 22, 2006, Mohan et al.
U.S. Appl. No. 11/562,577, filed Nov. 22, 2006, Findlay et al.
U.S. Appl. No. 11/562,502, filed Nov. 22, 2006, Tsifourdaris et al.
U.S. Appl. No. 11/562,516, filed Nov. 22, 2006, Mohan et al.

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