Gas turbine combustor

F - Mech Eng,Light,Heat,Weapons – 23 – R

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

F23R 3/42 (2006.01) F23M 99/00 (2010.01)

Patent

CA 2366704

A gas turbine combustor in which a part or all of the wall of the combustor disposed within an intake chamber is formed as an acoustic energy absorbing member that can absorb the acoustic energy of a combustion variation generated within the combustor. The acoustic energy absorbing member is constructed of a thin corrugated plate in a circumferential direction, a high-temperature-proof perforated material, or a back plate disposed at the outside of a perforated plate in a radial direction with a distance from the perforated plate. It is also possible to provide a covering member at the outside of the acoustic energy absorbing member in a radial direction, for covering the acoustic energy absorbing member with a distance from the acoustic energy absorbing member. It is preferable that the acoustic energy-absorbing member and/or the covering member are reinforced with a frame that extends in a circumferential direction and/or a longitudinal direction.

LandOfFree

Say what you really think

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

Rating

Gas turbine combustor does not yet have a rating. At this time, there are no reviews or comments for this patent.

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

Rate now

     

Profile ID: LFCA-PAI-O-1454840

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