초록 ▼

A loading spring segment for radially loading a turbine bucket within a turbine rotor groove includes a substantially circular metal sheet with a gap between opposed edges of the sheet, the sheet defining an arcuate segment in an arcuate length direction of the spring segment; and a plurality of rad

A loading spring segment for radially loading a turbine bucket within a turbine rotor groove includes a substantially circular metal sheet with a gap between opposed edges of the sheet, the sheet defining an arcuate segment in an arcuate length direction of the spring segment; and a plurality of radial slots in the sheet, spaced along the arcuate length direction to thereby create a plurality of individual springs within the arcuate segment.

대표청구항 ▼

1. A loading spring segment for radially loading turbine buckets within a turbine rotor groove, the loading spring segment comprising a substantially circular metal sheet with a gap between opposed edges of the sheet, said sheet defining an arcuate segment in an arcuate length direction of the sprin

1. A loading spring segment for radially loading turbine buckets within a turbine rotor groove, the loading spring segment comprising a substantially circular metal sheet with a gap between opposed edges of the sheet, said sheet defining an arcuate segment in an arcuate length direction of the spring segment; and a plurality of radial slots in said sheet, spaced along said arcuate length direction to thereby create a plurality of individual springs within said arcuate segment adapted to provide localized compression to the turbine buckets. 2. The loading spring segment of claim 1 wherein said sheet comprises stainless steel. 3. The loading spring segment of claim 1 wherein said arcuate segment extends along a plurality of buckets in said arcuate length direction. 4. The loading spring segment of claim 1 wherein said plurality of radial slots each extend more than 180° about the sheet. 5. A turbine rotor and bucket assembly comprising a rotor formed with a bucket retaining groove about a periphery thereof; a plurality of buckets, each having a mounting portion including a radially inner face received within said bucket retaining groove; an annular spring groove located in a base portion of said bucket retaining groove, and at least one radial loading spring segment seated in said annular spring groove, radially interposed between said base portion of said bucket retaining groove and the radially inner face of at least one of said plurality of buckets; said radial loading spring segment comprising a metal sheet of substantially circular cross-section, with a gap between opposed edges thereof, and at least one radial slot in said circular sheet to thereby form at least two discrete springs within said radial loading spring segment. 6. The assembly of claim 5 wherein said sheet comprises stainless steel. 7. The assembly of claim 5 wherein said radial loading spring segment extends along a plurality of buckets in said arcuate length direction. 8. The loading spring segment of claim 5 wherein said at least one radial slot extends more than 180° about the sheet. 9. The assembly of claim 5 wherein said mounting portion comprises a male dovetail and said bucket retaining groove comprises a complementary female dovetail. 10. The assembly of claim 5 wherein said gap is located substantially 90° from a location where said radial loading spring segment engages said radially inner face portion. 11. A method of assembling a turbine bucket to a rotor wherein the turbine bucket is formed with a male dovetail and said rotor is formed with a peripheral female dovetail groove, wherein the female dovetail groove has a base portion formed with an annular spring retaining groove, the method comprising:a) locating a radial loading spring segment of predetermined arcuate length in said spring retaining groove;b) twisting the bucket to enable the male dovetail to pass into the female dovetail groove;c) applying a radial force to the bucket to thereby compress the radial loading spring segment; andd) twisting the turbine bucket to a desired orientation where the male dovetail is fully seated within the female dovetail groove. 12. The method of claim 11 wherein the radial loading spring segment comprises a substantially circular metal sheet with a gap between opposed edges of the sheet, said sheet defining an arcuate segment in an arcuate length direction of the spring segment; and a plurality of radial slots in said sheet, spaced along said arcuate length direction to thereby create a plurality of individual springs within said arcuate segment. 13. The method of claim 11 wherein said sheet comprises stainless steel. 14. The method of claim 11 wherein said arcuate segment extends along a plurality of buckets in said arcuate length direction. 15. The method of claim 11 wherein said plurality of radial slots each extend more than 180° about the sheet. 16. The method of claim 11 wherein, during step a), said gap is located substantially 90° from a location where said spring segment engages said radially inner face portion.