The role of transverse air jets in the formation of gas turbine emissions

Shouse, Dale T.; Frayne, Charles W.; Stutrud, J.; Gogineni, Sivaram; Sturgess, G. J.

doi:10.2514/6.1996-705

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“…[Or [N] g mole 1 cm 3 sec. compared to the prompt NO expression of De Soete (De Soete, 1975 equivalence ratios to avoid reaction at stoichiometric interfaces which generate large quantities of NO (Shouse et at, 1996) , and to minimize the post-flame residence time (commensurate with accomplishing CO burn-up) (Sturgess et at, 1996) . Most low-NOx designs involve staging of some form, and the bulk equivalence ratios may be either fuel-lean (with a pilot for stability), or, rich-then-lean.…”

Section: Equivalence -Ratiomentioning

confidence: 99%

Combustor Design Trends for Aircraft Gas Turbine Engines

Sturgess

1996

ASME 1996 Turbo Asia Conference

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Advanced performance trends are surveyed for possible future gas turbine engines to power several classes of military and commercial aircraft. The resulting combustor trends are enumerated. Examples of enabling technology are given. Combustion considerations are discussed, and many commonalities between applications are discovered; fuel/air mixing and combustion dynamics emerge as topics of considerable importance.

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Section: Equivalence -Ratiomentioning

confidence: 99%