Thermally compliant turbine shroud mounting

Rotary kinetic fluid motors or pumps – Including thermal expansion joint – Resilient

Reexamination Certificate

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

C415S173100

Reexamination Certificate

active

07448846

ABSTRACT:
A shroud segment is adapted to surround a row of rotating turbine blades in a gas turbine engine. The shroud segment includes: an arcuate, axially extending first mounting flange having a first radius of curvature, and an arcuate, axially extending first overhang having a second radius of curvature. The overhang is disposed parallel to and radially inboard of the first mounting flange so that a first groove is defined between the first mounting flange and the first overhang. The first and second radii of curvature are substantially different from each other. The shroud segment may attached to a supporting structure or shroud hanger to form a shroud assembly.

REFERENCES:
patent: 3860358 (1975-01-01), Cavicchi et al.
patent: 6354795 (2002-03-01), White et al.
patent: 6361273 (2002-03-01), Eng 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

Thermally compliant turbine shroud mounting does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Thermally compliant turbine shroud mounting, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Thermally compliant turbine shroud mounting will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-4022559

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