Augmentor pilot nozzle
Number of patents in Portfolio can not be more than 2000
United States of America Patent
Stats
-
Jan 13, 2009
Grant Date -
Sep 27, 2007
app pub date -
Sep 20, 2005
filing date -
May 13, 2003
priority date (Note) -
In Force
status (Latency Note)
Importance
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.
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Cited Art Landscape
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