Low NOx combustion

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

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Details

60739, 60 39826, F02C 708

Patent

active

052633250

ABSTRACT:
A burner for a gas turbine combustor has a perforated plate facing the combustor and a plurality of gaseous fuel premixing tubes conveying a lean premixed fuel through the plate. A gas pilot extending through the plate projects jets of fuel parallel to the plate between the tube locations nearest the pilot. Ignition stability at turndown is maintained.

REFERENCES:
patent: 2850875 (1958-09-01), Gahwyler
patent: 2935128 (1960-05-01), Ferguson
patent: 3685950 (1972-08-01), Nomaguchi et al.
patent: 4100733 (1978-07-01), Striebel et al.
patent: 4618323 (1986-10-01), Mansour
patent: 4967561 (1990-11-01), Bruhwiler et al.
patent: 5094610 (1992-03-01), Mandai et al.
patent: 5121608 (1992-06-01), Willis et al.
John B. McVey & Jan B. Kennedy, "Lean Stability Augmentation for Premixing, Prevaporizing Combustors", Journal of Energy, vol. 4, Jul. 1980, pp. 7, 8, 11.

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