초록 ▼

A method of assembling a turbine comprises coupling at least one bucket to a rotor wheel. The bucket includes an upstream side, a downstream side, an airfoil extending therebetween and a dovetail extending radially inwardly from the airfoil to the rotor wheel. The method further comprises fixedly se

A method of assembling a turbine comprises coupling at least one bucket to a rotor wheel. The bucket includes an upstream side, a downstream side, an airfoil extending therebetween and a dovetail extending radially inwardly from the airfoil to the rotor wheel. The method further comprises fixedly securing the bucket to the rotor wheel with a locking pin that extends from the bucket upstream side through the bucket dovetail to the bucket downstream side.

대표청구항 ▼

1. A method of assembling a turbine, said method comprising:coupling at least one bucket including an upstream side, a downstream side, an airfoil extending therebetween and a dovetail extending radially inwardly from the airfoil to a rotor wheel wherein the bucket dovetail includes substantially pl

1. A method of assembling a turbine, said method comprising:coupling at least one bucket including an upstream side, a downstream side, an airfoil extending therebetween and a dovetail extending radially inwardly from the airfoil to a rotor wheel wherein the bucket dovetail includes substantially planar sidewalls; andfixedly securing the at least one bucket to the rotor wheel with a locking pin that extends from the bucket upstream side through the bucket dovetail to the bucket downstream side. 2. A method in accordance with claim 1 further comprising forming a channel to extend from the upstream side through the bucket dovetail to the downstream side of the bucket. 3. A method in accordance with claim 2 wherein fixedly securing the at least one bucket to the rotor wheel comprises inserting a locking pin through the channel. 4. A method in accordance with claim 3 further comprising forming a plurality of channels that each extend from the bucket upstream side through the bucket dovetail to the bucket downstream. 5. A method in accordance with claim 1 wherein fixedly securing the at least one bucket further comprises fixedly securing the at least one bucket to the rotor wheel using at least one locking pin that has a substantially linear cross-sectional profile. 6. A rotor assembly for a turbine comprising:a plurality of buckets secured to a rotor wheel, each said plurality of bucket comprising an upstream side, a downstream side, an airfoil, and a dovetail including substantially planar sidewalls, each said airfoil extending radially from each said dovetail, said plurality of buckets comprising at least a first bucket, and at least a second bucket; andat least one locking pin for securing at least one bucket to said rotor wheel, such that said locking pin extends from said bucket upstream side through said bucket dovetail to said bucket downstream side. 7. A rotor assembly in accordance with claim 6 wherein said at least one locking pin comprises a substantially linear cross-sectional profile. 8. A rotor assembly in accordance with claim 7 wherein said second bucket is secured to said rotor wheel by said dovetail. 9. A rotor assembly in accordance with claim 6 wherein said rotor wheel comprises a substantially annular retaining ring for securing said second bucket to said rotor wheel. 10. A rotor assembly in accordance with claim 6 wherein each said dovetail comprises a plurality of dovetail tangs. 11. A rotor assembly in accordance with claim 6 wherein said at least one locking pin extends through a portion of said bucket dovetail and through at least a portion of a circumferentially adjacent bucket dovetail. 12. A rotor assembly in accordance with claim 6 wherein at least one bucket further comprises a pressure side locking pin and a suction side locking pin. 13. A turbine comprising:at least one rotor assembly comprising at least one rotor wheel;a plurality of buckets secured to said rotor wheel, each said plurality of bucket comprising an upstream side, a downstream side, an airfoil and a dovetail including substantially planar sidewalls, each said airfoil extending radially from said dovetail, said plurality of buckets comprising at least one first bucket and at least one second bucket; andat least one locking pin for securing said at least one first bucket to said rotor wheel, such that said locking pin extends from said bucket upstream side through said bucket dovetail to said bucket downstream side. 14. A turbine in accordance with claim 13 wherein said at least one second bucket is secured to a hook of said rotor wheel by said bucket dovetail. 15. A turbine in accordance with claim 14 wherein said rotor wheel hook comprises a substantially annular retaining ring. 16. A turbine in accordance with claim 14 wherein said at least one locking pin extends through a portion of said bucket dovetail and through at least a portion of a circumferentially adjacent bucket dovetail. 17. A turbine in accordance with claim 14 wherei n each said bucket dovetail comprises dovetail tangs. 18. A turbine in accordance with claim 14 wherein said at least one locking pin further comprises a pressure side locking pin and a suction side locking pin. 19. A turbine in accordance with claim 13 wherein said at least one locking pin comprises a substantially linear cross-sectional profile.