Modular fuel nozzle air swirler

Fluid sprinkling – spraying – and diffusing – Combining of separately supplied fluids – Including whirler device to induce fluid rotation

Reexamination Certificate

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Details

C239S403000, C239S405000, C239S423000, C239S424000

Reexamination Certificate

active

07658339

ABSTRACT:
A modular fuel nozzle air swirler for a gas turbine engine has a body defining a fuel passage extending between an inlet end and a discharge end of the body. An annular cap is removably secured to the discharge end of the body via cooperating interlocking members.

REFERENCES:
patent: 3790086 (1974-02-01), Masai
patent: 5722032 (1998-02-01), Gay
patent: 6119459 (2000-09-01), Gomez et al.
patent: 6289677 (2001-09-01), Prociw et al.
patent: 6560964 (2003-05-01), Steinhorsson et al.
patent: 6863228 (2005-03-01), Mao et al.
patent: 7117678 (2006-10-01), Sampath et al.
patent: 7237730 (2007-07-01), Prociw et al.

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