Boundary layer prefilmer airblast nozzle

Details Boundary layer prefilmer airblast nozzle Boundary layer prefilmer airblast nozzle

1980-08-22

1982-12-28

Love, John J.

Fluid sprinkling, spraying, and diffusing

Combining of separately supplied fluids

Including whirler device to induce fluid rotation

60743, B05B 710

Patent

active

043657532

ABSTRACT:
A gas turbine fuel injection nozzle is disclosed in which the secondary fuel is spread into a very thin film entirely within a region of low air momentum. The fuel is therefore not affected by turbulence, and this results in an evenly circumferentially distributed fuel film at the discharge orifice of the nozzle resulting in an even and extremely fine spray of fuel to enhance proper engine performance.

REFERENCES:
patent: 3013732 (1961-12-01), Webster et al.
patent: 3424100 (1969-01-01), Schoenecker et al.
patent: 3912164 (1975-10-01), Lefebure et al.

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