Recirculation seal for a gas turbine exhaust diffuser

F - Mech Eng,Light,Heat,Weapons – 01 – D

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

F01D 11/00 (2006.01) F01D 25/30 (2006.01) F02C 7/28 (2006.01)

Patent

CA 2060876

56,411 ABSTRACT A seal is provided to prevent the recirculation of hot gas through an annular cavity formed between the outer flow liner of a diffuser and an exhaust cylinder in the exhaust section of a gas turbine. The seal is formed from a high temperature cloth, such as fiber glass, which is sandwiched between two layers of a fine wire mesh. The seal is comprised of a plurality of arcuate segments. Although the cloth has a rectangular shape when in its undeformed state, it takes an arcuate shape as a result of being crimped within inner and outer arcuate channels. The seal is retained by sliding the channels into circumferential grooves in the exhaust cylinder and outer flow liner. An expansion loop is formed in the seal to allow for differential expansion between the exhaust cylinder and the outer liner.

LandOfFree

Say what you really think

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

Rating

Recirculation seal for a gas turbine exhaust diffuser does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Recirculation seal for a gas turbine exhaust diffuser, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Recirculation seal for a gas turbine exhaust diffuser will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFCA-PAI-O-1957094

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