Gas turbine annular combustor

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

Patent

Rate now

  [ 0.00 ] – not rated yet Voters 0   Comments 0

Details

60738, 60739, 60743, 60755, F02C 722, F02C 304

Patent

active

051136473

ABSTRACT:
The expense of fabricating an annular combustor (10) for a gas turbine is minimized by providing a combustor housing (12) including an axially extending sleeve (14) and an annular liner (18) disposed within the housing (12) and about the sleeve (14). The annular liner (18) has concentric inner and outer axially elongated walls (20, 22) spaced from the sleeve (14) and the housing (12), respectively, and also has a radially extending wall (24) spaced from the housing (12) and interconnecting the inner and outer walls (20, 22) at one end to define a combustion chamber (26). The liner (18) to spaced from the housing (12) the sleeve (14) to define a compressed air flow path (28) extending from a radially outer compressed air inlet (30) to a radially inner compressed air outlet (32) in communication with the combustion chamber (26) axially remote from the radially extending wall (24). The annular combustor (26) is provided with a plurality of fuel injectors (36, 40) for injecting a liquid fuel to be burned into the liner (18) in a generally tangential direction adjacent the radially extending wall (24) to impact liquid fuel directly onto an inner surface (22a) of the outer wall (22) adjacent to the radially extending wall (24). The annular combustor (26) also includes a plurality of open ended elongated tubes (34) in the outer wall (22) intermediate the compressed air inlet (30) and the radially extending wall (24) to direct air for combustion into the combustion chamber (26). With this arrangement, a mixture of fuel and air may be ignited within the combustion chamber (26) and the resulting hot gases of combustion utilized to drive the gas turbine.

REFERENCES:
patent: 3383855 (1968-05-01), Freeman et al.
patent: 3613360 (1971-10-01), Howes
patent: 3671171 (1972-06-01), Doyle
patent: 3869864 (1975-03-01), Bunn
patent: 4018043 (1977-04-01), Clemmens
patent: 4151709 (1979-05-01), Melconian et al.
patent: 4216651 (1980-08-01), Ormerod
patent: 4301657 (1981-11-01), Penny
patent: 4549402 (1985-10-01), Saintsbury et al.
patent: 4794754 (1989-01-01), Shekelton et al.
patent: 4926630 (1990-05-01), Shekleton

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

Rate now

     

Profile ID: LFUS-PAI-O-2411549

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