Appeal No. 2001-2193 Page 5
Application No. 09/152,515
A liquid fuel pressure atomizing nozzle for gas-
turbine burners, comprising a nozzle body having at least
two separate feed passages for one liquid to be atomized,
the first feed passage being at least partly enclosed by
the second feed passage and also being connected
downstream to an outer space via a discharge orifice, and
the second feed passage likewise being connected to the
outer space, wherein the second feed passage has at least
two discharge orifices to the outer space wherein an axis
of each of said at least two discharge orifices are
oriented outwardly from a central axis of said first feed
passage.
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