Fluid reaction surfaces (i.e. – impellers) – Rotor having flow confining or deflecting web – shroud or... – Axially extending shroud ring or casing
Reexamination Certificate
2006-08-22
2006-08-22
Look, Edward K. (Department: 3745)
Fluid reaction surfaces (i.e., impellers)
Rotor having flow confining or deflecting web, shroud or...
Axially extending shroud ring or casing
C415S173600
Reexamination Certificate
active
07094032
ABSTRACT:
A shroud for use with a turbine blade is disclosed wherein the shroud provides at least one knife edge with at least one tooth for cutting a groove in a compliant rub strip that minimizes wear on the knife edge. The tooth is positioned along the knife edge inward of the ends of the knife edge and a distance from an airfoil stackline such that the moment created by the tooth mass and its effect on shroud bending stress is significantly reduced, thereby resulting in increased turbine blade durability.
REFERENCES:
patent: 5083903 (1992-01-01), Erdmann
patent: 6491498 (2002-12-01), Seleski et al.
patent: 6805530 (2004-10-01), Urban
patent: 6857853 (2005-02-01), Tomberg et al.
patent: 6890150 (2005-05-01), Tomberg
patent: 6913445 (2005-07-01), Beddard et al.
patent: 2005/0175453 (2005-08-01), Dube et al.
Edgar Richard A.
Look Edward K.
LandOfFree
Turbine blade shroud cutter tip does not yet have a rating. At this time, there are no reviews or comments for this patent.
If you have personal experience with Turbine blade shroud cutter tip, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Turbine blade shroud cutter tip will most certainly appreciate the feedback.
Profile ID: LFUS-PAI-O-3715866