Methods and systems for securing turbine nozzles

1. A nozzle assembly comprising:

at least one stationary nozzle;

an outer ring having a predefined shape, said outer ring comprising at least one groove defined therein, said at least one outer ring groove configured to receive at least a portion of said at least one stationary nozzle therein; and

an attachment member coupled between said at least one stationary nozzle and said outer ring, said attachment member having a first configuration at a first nozzle assembly operating temperature, and having a second configuration at a second nozzle assembly operating temperature, wherein said attachment member in the first configuration creates a gap between said at least one stationary nozzle and said outer ring, and said attachment member in the second configuration is transformed such that said at least one stationary nozzle contacts said outer ring.

2. A nozzle assembly in accordance with claim 1 , wherein said attachment member is fabricated from a brass material.

3. A nozzle assembly in accordance with claim 1 , wherein said attachment member is fabricated from a copper material.

4. A nozzle assembly in accordance with claim 1 , wherein said attachment member is configured to radially bias said at least one stationary nozzle a distance from said outer ring while in the first configuration to define said gap.

5. A nozzle assembly in accordance with claim 1 , wherein said attachment member is transformable from the first configuration to the second configuration in response to the second nozzle assembly operating temperature.

6. A nozzle assembly in accordance with claim 1 , wherein said at least one stationary nozzle comprises an end portion comprising a substantially arcuate groove defined therein, said groove configured to receive said attachment member therein.

7. A nozzle assembly in accordance with claim 1 , wherein said at least one outer ring groove defines a substantially arcuate groove, said arcuate groove configured to receive said attachment member therein.

8. A nozzle assembly in accordance with claim 1 , wherein said attachment member comprises a loading pin extending between said at least one stationary nozzle and said outer ring.

9. A nozzle assembly in accordance with claim 1 , wherein said at least one stationary nozzle comprises an end portion coupled within said at least one outer ring groove, said end portion comprises a dovetailed end portion.

10. A rotary machine comprising:

a rotor; and

at least one nozzle assembly coupled to said rotor, said at least one nozzle assembly comprising:

at least one stationary nozzle extending radially outwardly from said rotor;

an outer ring having a predefined shape and said outer ring substantially circumscribes said rotor, wherein said outer ring comprises at least one groove defined therein, said at least one outer ring groove is configured to receive at least a portion of said at least one stationary nozzle therein; and

an attachment member coupled between said at least one stationary nozzle and said outer ring, said attachment member having a first configuration at a first nozzle assembly operating temperature, and having a second configuration at a second nozzle assembly operating temperature, wherein said attachment member in the first configuration creates a gap between said at least one stationary nozzle and said outer ring, and said attachment member in the second configuration is transformed such that said at least one stationary nozzle contacts said outer ring.

11. A rotary machine in accordance with claim 10 , wherein said attachment member is configured to radially bias said at least one stationary nozzle a distance from said outer ring while in the first configuration to define said gap.

12. A rotary machine in accordance with claim 11 , wherein said attachment member is transformable from the first configuration to the second configuration in response to the second nozzle assembly operating temperature, wherein the second nozzle assembly operating temperature is higher than the first nozzle assembly operating temperature.

13. A rotary machine in accordance with claim 12 , wherein said at least one stationary nozzle comprises an end portion comprising a substantially arcuate groove defined therein, said groove configured to receive said attachment member therein.

14. A rotary machine in accordance with claim 10 , wherein said attachment member is fabricated from one of a brass material and a copper material.

15. A method of assembling a rotary machine, said method comprising:

coupling at least one stationary nozzle to a rotor such that the at least one stationary nozzle extends radially outwardly from the rotor;

coupling an outer ring having a predefined shape to the rotor such that the outer ring substantially circumscribes the rotor, the outer ring includes at least one groove defined therein, the at least one groove configured to receive at least a portion of the at least one stationary nozzle therein; and

coupling an attachment member between the at least one stationary nozzle and the outer ring, the attachment member having a first configuration at a first nozzle assembly operating temperature, and having a second configuration at a second nozzle assembly operating temperature, wherein the attachment member in the first configuration creates a gap between the at least one stationary nozzle and the outer ring, and the attachment member in the second configuration is transformed such that the at least one stationary nozzle contacts the outer ring.

16. A method of assembling a rotary machine in accordance with claim 15 , wherein coupling an attachment member further comprises radially biasing the at least one stationary nozzle a distance from the outer ring while in the first configuration to define the gap.

17. A method of assembling a rotary machine in accordance with claim 16 , wherein coupling an attachment member further comprises coupling the attachment member that is transformable from the first configuration to the second configuration in response to the second nozzle assembly operating temperature, wherein the second nozzle assembly operating temperature is higher than the first nozzle assembly operating temperature.

18. A method of assembling a rotary machine in accordance with claim 17 , wherein coupling an attachment member further comprises coupling an attachment member that includes a loading pin fabricated from one of a brass material and a copper material.

19. The nozzle assembly in accordance with claim 1 , wherein the second nozzle assembly operating temperature is higher than the first nozzle assembly operating temperature.

20. The rotary machine of claim 10 , wherein the second nozzle assembly operating temperature is higher than the first nozzle assembly operating temperature.