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A packing segment for an annular seal ring assembly for use in a hot gas path of a turbomachine, includes a sealing face mounting a plurality of axially spaced sealing teeth; a necked-in center portion radially outward of the sealing face; and a mounting portion radially outward of the center portio

A packing segment for an annular seal ring assembly for use in a hot gas path of a turbomachine, includes a sealing face mounting a plurality of axially spaced sealing teeth; a necked-in center portion radially outward of the sealing face; and a mounting portion radially outward of the center portion. At least one steam feed hole extends angularly from a radially outermost face of the segment to a location along a side of the center portion such that, in use, at least a portion of the feed hole is exposed to hot gas in the hot gas path for flow through the feed hole to a cavity behind the segment.

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1. A packing segment for an annular seal ring assembly for use in a hot gas path of a turbomachine, the packing segment comprising a radially inner sealing portion including a sealing face mounting a plurality of axially spaced sealing teeth; a necked-in center portion radially outward of said seali

1. A packing segment for an annular seal ring assembly for use in a hot gas path of a turbomachine, the packing segment comprising a radially inner sealing portion including a sealing face mounting a plurality of axially spaced sealing teeth; a necked-in center portion radially outward of said sealing face; and a mounting portion radially outward of said center portion, said mounting portion having a radially outermost face; and at least one steam feed hole extending angularly between a first location on said radially outermost face and a second location along a side of said necked-in center portion such that, in use, at least a portion of said feed hole is exposed to gas in the gas path for flow through said feed hole to a cavity area behind said segment. 2. The packing ring segment of claim 1 wherein said steam feed hole extends at an acute angle relative to a radial center line through the segment. 3. The packing ring segment of claim 1 wherein said steam feed hole has a diameter determined by steam volume. 4. The packing ring segment of claim 1 wherein said mounting portion includes a pair of laterally extending flanges adapted to seat radially behind a pair of dovetail hooks in a nozzle diaphragm. 5. An annular seal ring assembly for a turbine nozzle diaphragm comprising a plurality of part annular packing segments adapted to seat in a dovetail groove in the diaphragm, with a cavity radially between a back face of the segment and the diaphragm, each segment comprising a sealing face mounting a plurality of axially spaced sealing teeth; a center portion radially outward of said sealing face; and a mounting portion radially outward of said center portion, said mounting portion including a pair of laterally extending flanges adapted to seat radially behind a pair of dovetail hooks in the nozzle diaphragm; and having a radially outermost face; and at least one steam feed hole extending angularly between a first location on said radially outermost face and a second location along a side of said center portion such that, in use, at least a portion of said feed hole is exposed to gas in a hot gas path for flow through said feed hole to a cavity behind said packing segment to thereby displace said packing segment in a radially inward direction. 6. The packing ring segment of claim 5 wherein said steam feed hole extends at an acute angle relative to a radial center line through the segment. 7. The packing ring segment of claim 5 wherein said steam feed hole has a diameter determined by steam volume.