Gas turbine engine combustor

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

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60757, 60760, F02C 100, F02G 300

Patent

active

046515348

ABSTRACT:
A combustor for a gas turbine engine including a two-stage burner having first and second combustion and exhaust sections and a burner casing coaxially surrounding the burner to define an annular conduit for reverse flow of inlet air. The burner includes a fuel injector at the upstream end thereof, primary inlet ports introducing 18% of inlet air into the first combustion section, first cooling ports introducing 12% of inlet air into the first combustion section for generating a swirling cooling flow which mixes with primary air after cooling the upstream end of the first combustion section, secondary inlet ports introducing 18% of inlet air into second stage combustion section, second cooling ports introducing 8% of inlet air into the second combustion section to generate a swirling flow which mixes with primary air after cooling the upstream end of the second combustion section, and dilution ports introducing 44% of inlet air into the exhaust section to cool the exhaust gas.

REFERENCES:
patent: 2446059 (1948-07-01), Peterson et al.
patent: 2654996 (1953-10-01), Boninsegni
patent: 3283502 (1966-11-01), Lefebvre
patent: 3831854 (1974-08-01), Sato et al.
patent: 3910035 (1975-10-01), Juhasz et al.
patent: 4052844 (1977-10-01), Caruel et al.
patent: 4054028 (1977-10-01), Kawaguchi
patent: 4058977 (1977-11-01), Markowski et al.
patent: 4112676 (1978-09-01), De Corso
patent: 4162611 (1979-07-01), Carvel et al.
patent: 4192139 (1980-03-01), Buchheim
patent: 4215535 (1980-08-01), Lewis
patent: 4339925 (1982-07-01), Eggmann 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

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

Rate now

     

Profile ID: LFUS-PAI-O-1346444

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