Compressor turbine vane airfoil profile

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Radial flow devices

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C416S243000, C416SDIG004

Reexamination Certificate

active

07862303

ABSTRACT:
A single stage high pressure turbine vane 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.

REFERENCES:
patent: 6398489 (2002-06-01), Burdgick et al.
patent: 6769879 (2004-08-01), Cleveland et al.
patent: 6779980 (2004-08-01), Brittingham 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: 7559746 (2009-07-01), Tsifourdaris et al.
patent: 2005/0079061 (2005-04-01), Beddard
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.

LandOfFree

Say what you really think

Search LandOfFree.com for the USA inventors and patents. Rate them and share your experience with other people.

Rating

Compressor turbine vane airfoil profile does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Compressor turbine vane airfoil profile, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Compressor turbine vane airfoil profile will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2671962

  Search
All data on this website is collected from public sources. Our data reflects the most accurate information available at the time of publication.