Shroud honeycomb cutter

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Between blade edge and static part

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C415S173600, C416S189000, C416S191000, C416S192000

Reexamination Certificate

active

07094023

ABSTRACT:
A turbine blade for use in a gas turbine engine is provided. The turbine blade includes an airfoil portion having a tip end, a shroud attached to the tip end, which shroud has an outer surface, and a knife edge attached to an outer surface of the shroud. The knife edge has a pair of cutter blades protruding outwardly from the knife edge.

REFERENCES:
patent: 6491498 (2002-12-01), Seleski et al.
patent: 6805530 (2004-10-01), Urban
patent: 6913445 (2005-07-01), Beddard et al.
patent: 08-303204 (1996-11-01), None

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

Shroud honeycomb cutter does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Shroud honeycomb cutter, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Shroud honeycomb cutter will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-3687216

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