Augmentor pilot nozzle

Details Augmentor pilot nozzle Augmentor pilot nozzle

2005-12-06

2005-12-06

Kim, Ted (Department: 3746)

Power plants

Reaction motor

Having afterburner

C060S765000, C060S749000

Reexamination Certificate

active

06971239

ABSTRACT:
A gas turbine engine augmentor nozzle has an inlet for connection to an augmentor fuel conduit and an outlet for expelling a spray of fuel. A passageway between the inlet and outlet is at least partially bounded by outlet end surface portions diverging from each other. The nozzle may be used as a replacement for a non-divergent nozzle and may reorient a fuel jet centerline toward radial.

REFERENCES:
patent: 2799991 (1957-07-01), Conrad
patent: 2866313 (1958-12-01), Holl
patent: 3455108 (1969-07-01), Clare et al.
patent: 3605407 (1971-09-01), Bryce
patent: 3913319 (1975-10-01), Hall
patent: 4887425 (1989-12-01), Vdoviak
patent: 5385015 (1995-01-01), Clements et al.
patent: 5685140 (1997-11-01), Clements et al.

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