초록 ▼

Method and apparatus for assembling steam turbines are provided. The method of assembling a steam turbine includes providing an annular outer member, providing an annular inner member, coupling a plurality of airfoils to the inner member with a plurality of generally radial fastener assemblies such

Method and apparatus for assembling steam turbines are provided. The method of assembling a steam turbine includes providing an annular outer member, providing an annular inner member, coupling a plurality of airfoils to the inner member with a plurality of generally radial fastener assemblies such that the plurality of airfoils extend substantially radially outward from the inner member, and coupling each of the plurality of airfoils to the outer member.

대표청구항 ▼

What is claimed is: 1. A method for assembling a steam turbine, said method comprising: providing an annular outer member; providing an annular inner member; rotatably coupling a plurality of airfoils to the inner member with a first plurality of fasteners that are each inserted into one of a plura

What is claimed is: 1. A method for assembling a steam turbine, said method comprising: providing an annular outer member; providing an annular inner member; rotatably coupling a plurality of airfoils to the inner member with a first plurality of fasteners that are each inserted into one of a plurality of circumferentially-spaced bores extending substantially radially through the inner member and oriented towards the outer member such that the plurality of airfoils extend substantially radially outward from the inner member adjusting the plurality of airfoils into a final airfoil position; limiting rotational movement of the plurality of airfoils; coupling each of the plurality of airfoils to the inner member with a second plurality of fasteners; and welding each of the plurality of airfoils to the outer member. 2. A method in accordance with claim 1 wherein coupling a plurality of airfoils to the inner member with a first plurality of fasteners further comprises inserting at least one alignment pin generally radially into each of the plurality of airfoils to facilitate aligning each of the plurality of airfoils with respect to the inner member. 3. A method in accordance with claim 1 wherein coupling a plurality of airfoils to the inner member with a second plurality of fasteners further comprises coupling each of the plurality of airfoils to the inner member with at least one bolt. 4. A method in accordance with claim 1 further comprising forming the plurality of circumferentially-spaced bores within the inner member such that each of the bores is sized to receive a portion of the first plurality of fasteners therethrough to facilitate securing each of the plurality of airfoils to the inner member 5. A diaphragm for a steam turbine, said diaphragm comprises: a radially outer member configured to extend substantially circumferentially within said steam turbine; a radially inner member configured to extend substantially circumferentially within said steam turbine, said inner member comprising a plurality of circumferentially-spaced bores extending substantially radially through said inner member towards said outer member, some of said plurality of bores each comprise a countersunk portion; and at least one airfoil extending substantially radially between said outer and inner members, said at least one airfoil rotatably coupled to said radially inner member with a first plurality of fasteners, said first plurality of fasteners facilitate orienting said at least one airfoil relative to said inner member, said at least one airfoil coupled to said radially inner member with a second plurality of fasteners, said at least one airfoil welded to said radially outer member. 6. A diaphragm in accordance with claim 5 wherein said first plurality of fasteners comprises at least one alignment pin and said second plurality of fasteners comprises at least one bolt. 7. A diaphragm in accordance with claim 5 wherein one of said radially inner member and said radially outer member comprises a plurality of openings extending therethrough, said plurality of openings facilitate aligning said at least one airfoil with respect to said diaphragm. 8. A diaphragm in accordance with claim 5 wherein said first and second plurality of fasteners facilitate reducing weld distortion within said diaphragm. 9. A diaphragm in accordance with claim 5 wherein said first and second plurality of fasteners facilitate reducing assembly time of said diaphragm. 10. A diaphragm in accordance with claim 5 wherein said first and second plurality of fasteners facilitate improving turbine performance. 11. A steam turbine comprising at least one diaphragm comprising a radially outer member, a radially inner member comprising a plurality of circumferentially-spaced bores extending substantially radially therethrough and towards said outer member, and a plurality of airfoils extending therebetween and spaced circumferentially from each other, said radially outer and inner members configured to extend circumferentially within said turbine, said plurality of airfoils rotatably coupled to said radially inner member with a first plurality of fasteners that orient at least one airfoil relative to said inner member, said plurality of airfoils coupled to said radially inner member with a second plurality of fasteners, said plurality of airfoils welded to said radially outer member. 12. A steam turbine in accordance with claim 11 wherein said radially inner member and said radially outer member comprise a plurality of circumferentially-spaced openings extending therethrough, said openings facilitate aligning each of said plurality of airfoils with respect to said diaphragm. 13. A steam turbine in accordance with claim 11 wherein said plurality of circumferentially spaced bores are sized to receive at least a portion of said second plurality of fasteners therethrough for securing each of said plurality of airfoils within said diaphragm. 14. A steam turbine in accordance with claim 11 wherein said first plurality of fasteners comprise an alignment pin, said second plurality of fasteners comprises a bolt, said alignment pin facilitates aligning each of said plurality of airfoils within said diaphragm, said bolt facilitates securing each of said plurality of airfoils within said diaphragm. 15. A steam turbine in accordance with claim 11 wherein said first and second plurality of fasteners facilitate improving an operating efficiency of said steam turbine. 16. A steam turbine in accordance with claim 11 wherein said first and second plurality of fasteners facilitate reducing weld distortion of said diaphragm. 17. A steam turbine in accordance with claim 11 wherein said first and second plurality of fasteners facilitate reducing assembly time of said diaphragm.