Triple annular combustor for gas turbine engine

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

60747, 60748, F23R 334, F02C 7228

Patent

active

053236041

ABSTRACT:
In accordance with one aspect of the present invention, a combustor is disclosed having three separate domes, each dome having disposed therein a plurality of circumferentially spaced mixers for uniformly mixing air and fuel. The combustor utilizes a high percentage of the total available combustion air at the dome area in order to maintain a lean mixture of air and fuel during all levels of engine output. Besides providing an unobstructed area in the diffuser dump region upstream of the mixers for the combustion air, sealing means is included to prevent cooling air from entering the combustion chamber until downstream of the primary combustion zone. Heat shields having radial centerbodies are also included between each dome to isolate each primary combustion zone.

REFERENCES:
patent: 2996884 (1960-02-01), Johnson et al.
patent: 3032990 (1962-05-01), Rogers
patent: 3236048 (1966-02-01), Spears, Jr.
patent: 3714778 (1973-02-01), Howald
patent: 3720058 (1973-03-01), Collinson et al.
patent: 3724207 (1973-04-01), Johnson
patent: 3910035 (1975-10-01), Juhasz et al.
patent: 3915387 (1975-10-01), Caruel et al.
patent: 3943705 (1976-03-01), DeCorso et al.
patent: 3980233 (1976-09-01), Simmons et al.
patent: 4092826 (1978-06-01), Pask
patent: 4100733 (1978-07-01), Striebel et al.
patent: 4107918 (1978-08-01), Andrew et al.
patent: 4180972 (1980-01-01), Herman et al.
patent: 4194358 (1980-03-01), Stenger
patent: 4302932 (1981-12-01), Kuznetsov et al.
patent: 4356698 (1982-11-01), Chamberlain
patent: 4373342 (1983-02-01), Willis et al.
patent: 4455840 (1984-06-01), Matt et al.
patent: 4805411 (1989-02-01), Hellat et al.
patent: 4967561 (1990-11-01), Bruhwiler et al.
patent: 4991398 (1991-02-01), Clark et al.
patent: 5020329 (1991-06-01), Ekstedt et al.
patent: 5195315 (1993-03-01), Holladay
"Asea Brown Boveri introducing a dual fuel dry low-NOx burner design", by Eric Jeffs; Gas Turbine World, May-Jun. 1989.

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

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

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

Rate now

     

Profile ID: LFUS-PAI-O-2369666

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