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A support arrangement for a turbine diaphragm segment in a split turbine casing includes a semi-annular diaphragm segment having a horizontal joint surface; a support bar joined to the diaphragm segment adjacent the horizontal joint surface, the support bar formed with a first flange extending outwa

A support arrangement for a turbine diaphragm segment in a split turbine casing includes a semi-annular diaphragm segment having a horizontal joint surface; a support bar joined to the diaphragm segment adjacent the horizontal joint surface, the support bar formed with a first flange extending outwardly over a portion of the casing, the portion including a horizontal surface; and a shim on the horizontal surface and engaged by the first flange.

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What is claimed is: 1. A support arrangement for a turbine diaphragm segment in a split turbine casing comprising: a semi-annular diaphragm segment having a horizontal joint surface; a support bar joined to said diaphragm segment adjacent said horizontal joint surface, said support bar formed with

What is claimed is: 1. A support arrangement for a turbine diaphragm segment in a split turbine casing comprising: a semi-annular diaphragm segment having a horizontal joint surface; a support bar joined to said diaphragm segment adjacent said horizontal joint surface, said support bar formed with a center body portion and a first flange extending perpendicular to said center body portion and radially outwardly over a portion of the casing, said portion including a horizontal surface; and a shim on said horizontal surface and engaged by a lower surface of said first flange, an upper surface of said first flange being substantially flush with said horizontal joint surface. 2. The support arrangement of claim 1 wherein said support bar is formed with a second flange extending perpendicular to said center body portion and radially inwardly and seated in a slot formed in said diaphragm segment. 3. The support arrangement of claim 2 wherein one or more bolts extend through said second flange and into said diaphragm segment. 4. The support arrangement of claim 2 wherein said horizontal surface is formed with a shallow pocket with said shim seated in said pocket. 5. The support arrangement of claim 1 wherein said portion of said casing comprises a cut-out area, said horizontal surface forming a base of said cutout area. 6. The support arrangement of claim 1 wherein said shim comprises a shim pack with plural stacked shim elements. 7. A support arrangement for a turbine diaphragm segment in a split turbine casing comprising: a semi-annular diaphragm segment having a horizontal joint surface; a support bar joined to said diaphragm segment adjacent said horizontal joint surface, said support bar formed with a first flange extending outwardly over a portion of the casing, said portion including a horizontal surface; and a shim on said horizontal surface and engaged by said first flange wherein said horizontal surface is formed with a shallow pocket with said shim seated in said pocket. 8. The support arrangement of claim 7 wherein said pocket surrounds said shim on at least three sides thereof. 9. The support arrangement of claim 8 wherein said pocket surrounds said shim on four sides thereof. 10. A support arrangement for a turbine diaphragm segment in a split turbine casing comprising: a semi-annular diaphragm segment having a horizontal joint surface; a support bar joined to said diaphragm segment adjacent said horizontal joint surface, said support bar formed with a vertically-oriented center body portion, with a first flange extending perpendicular to said center body portion and radially outwardly over a cut-out area of the casing such that an upper surface of said first flange is substantially flush with said horizontal joint surface, said cut-out area defined by a vertical wall and a horizontal surface, said support bar formed with a second flange extending perpendicular to said center body portion and radially inwardly and seated in a slot formed in said diaphragm segment; and at least one shim seated on said horizontal surface, and engaged by said first flange. 11. The support arrangement of claim 10 wherein one or more bolts extend through said second flange and into said diaphragm segment. 12. The support arrangement of claim 10 wherein said at least one shim comprises a shim pack with plural stacked discrete shim elements. 13. The support arrangement of claim 10 wherein said horizontal surface is formed with a shallow pocket with said shim seated in said pocket. 14. A support arrangement for a lower turbine diaphragm segment in a lower turbine casing comprising: a semi-annular diaphragm segment having a pair of horizontal joint surfaces, spaced circumferentially 180�� from each other; a support bar joined to said diaphragm segment adjacent each of said horizontal joint surfaces, each support bar formed with a first flange extending outwardly over a portion of the casing, said portion including a horizontal surface; a shim located on said horizontal surface and engaged by said first flange, wherein said horizontal surface is formed with a shallow pocket with said shim seated in said pocket; further comprising an upper turbine casing that at least partially overlies each said support bar; and wherein a shim is interposed between and engaged with said upper casing and each said support bar. 15. The support arrangement of claim 14 wherein said pocket surrounds said shim on at least three sides thereof. 16. The support arrangement of claim 15 wherein said pocket surrounds said shim on four sides thereof. 17. The support arrangement of claim 14 and further comprising an upper turbine casing that at least partially overlies each said support bar. 18. The support arrangement of claim 14 wherein a shim is interposed between and engaged with said upper casing and each said support bar.