Method of combustion with low acoustics

Combustion – Process of combustion or burner operation – Flame shaping – or distributing components in combustion zone

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431114, 431285, 431284, 431350, 60750, F02C 100

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active

058656090

ABSTRACT:
A method of reducing pressure fluctuations in the combustor of a gas turbine engine resulting from the combustion of fuel and air therein comprises combusting a fuel/air mixture in a combustor downstream of the exit plane of a fuel nozzle assembly such that such recirculation zones generated by the fuel nozzle assembly are in spaced relation to the exit plane and the combustion products are isolated from the fuel and air in the mixing zone at all operating conditions of the engine.

REFERENCES:
patent: 2889871 (1959-06-01), Voheis
patent: 2982347 (1961-05-01), Kidwell et al.
patent: 2986206 (1961-05-01), Boelsma
patent: 5307634 (1994-05-01), Hu

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