Ring combustion chamber with ring burner for gas turbines

Power plants – Combustion products used as motive fluid – Combustion products generator

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60743, 60747, F02G 300, F02G 100

Patent

active

044558406

ABSTRACT:
A ring burner of a ring combustion chamber is divided into a large number of honeycomb-like parallel axis canals for the combustion air, by radial and circumferential plate canals or by radial plate canals, longitudinal tubing, radial tubing and annular tubing into which combustion gas is introduced from nozzles in the surrounding walls. At the burner outlet there are flame retention nozzles provided above the frontal surface area of the plate canals or tubes. Fuel nozzles are provided in front of the burner inlet for operation as a dual burner with gaseous and liquid fuels.

REFERENCES:
patent: 2701444 (1955-02-01), Day
patent: 2712221 (1955-07-01), Pouchot
patent: 3046731 (1962-07-01), Cambel et al.
patent: 4158949 (1979-06-01), Reider

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

Ring combustion chamber with ring burner for gas turbines does not yet have a rating. At this time, there are no reviews or comments for this patent.

If you have personal experience with Ring combustion chamber with ring burner for gas turbines, we encourage you to share that experience with our LandOfFree.com community. Your opinion is very important and Ring combustion chamber with ring burner for gas turbines will most certainly appreciate the feedback.

Rate now

     

Profile ID: LFUS-PAI-O-2226353

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