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A flow control assembly for controlling cooling flow of a turbine engine is provided. The flow control assembly includes a first flow control device having a first sidewall and a second sidewall. The first sidewall is coupled to a compressor vane and is configured to define a first flow path from a

A flow control assembly for controlling cooling flow of a turbine engine is provided. The flow control assembly includes a first flow control device having a first sidewall and a second sidewall. The first sidewall is coupled to a compressor vane and is configured to define a first flow path from a compressor to a turbine vane. The second sidewall is coupled to a compressor vane and is configured to define a second flow path from the compressor to a turbine blade. A second flow control device is coupled to the compressor and includes an orifice device coupled to the compressor vane and a meter device coupled to the orifice, wherein the orifice is configured to direct a cooling flow to the meter device. A controller is configured to control the meter device to facilitate regulating the cooling flow into at least one of the first flow path and the second flow path.

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1. A flow control assembly for controlling a cooling flow of a turbine engine having a compressor and a turbine, the compressor having an exit guide vane and the turbine having a turbine vane and a turbine blade, said flow control assembly comprising: a first flow control device comprising a first s

1. A flow control assembly for controlling a cooling flow of a turbine engine having a compressor and a turbine, the compressor having an exit guide vane and the turbine having a turbine vane and a turbine blade, said flow control assembly comprising: a first flow control device comprising a first sidewall and a second sidewall, said first sidewall coupled to the exit guide vane and the turbine vane and configured to define a first flow path from the compressor to the turbine vane, said second sidewall coupled to the exit guide vane and to the turbine blade and configured to define a second flow path from the compressor to the turbine blade;a second flow control device coupled to the exit guide vane and in flow communication with said first flow control device, said second flow control device comprising an orifice device coupled to the exit guide vane and a meter device coupled to said orifice device, said orifice device configured to direct the cooling flow to said meter device; anda controller coupled to said second flow control device and configured to control said meter device to facilitate regulating the cooling flow into at least one of said first flow path and said second flow path. 2. The flow control assembly of claim 1, wherein said first sidewall is configured to isolate said first flow path from said second flow path. 3. The flow control assembly of claim 1, wherein said orifice device is coupled to a suction side of the exit guide vane. 4. The flow control assembly of claim 1, wherein said orifice device is coupled to a mid-span portion of the exit guide vane. 5. The flow control assembly of claim 1, wherein said orifice device is coupled to an inlet end of the exit guide vane. 6. The flow control assembly of claim 1, wherein said orifice device comprises at least one of a port, a nozzle and a snorkel. 7. The flow control assembly of claim 1, wherein said meter device comprises a pneumatic valve comprising: a bias member; andan orifice plate coupled to said bias member. 8. The flow control assembly of claim 1, wherein said controller is configured to control said meter device to meter the cooling flow into said first flow path. 9. The flow control assembly of claim 1, wherein said controller is configured to control said meter device to meter the cooling flow into said second flow path. 10. The flow control assembly of claim 1, wherein said controller is configured to control said meter device to meter the cooling flow into said first flow path and said second flow path. 11. A turbine engine comprising: a compressor comprising an exit guide vane, said exit guide vane comprising an inlet end, an outlet end and a mid-span portion located therebetween;a turbine coupled to said compressor and comprising a turbine vane and a turbine blade; anda flow control assembly coupled to said compressor and said turbine, said control assembly comprising:a first flow control device comprising a first sidewall and a second sidewall, said first sidewall coupled to said outlet end and said turbine vane and configured to define a first flow path from said outlet end to said turbine vane, said second sidewall coupled to said exit guide vane and said turbine blade and configured to define a second low path from about said mid-span portion to said turbine blade; anda second flow control device coupled to said exit guide vane and in flow communication with said first flow control device, said second flow control device comprising an orifice device and a meter device, said orifice device coupled to said mid-span portion and configured to direct a cooling flow to said meter device and said meter device configured to meter said cooling flow into at least one of said first flow path and said second flow path. 12. The turbine engine of claim 11, further comprising a combustor and said first sidewall is positioned between said combustor and said compressor. 13. The turbine engine of claim 11, wherein said first sidewall is configured to isolate said first flow path from said second flow path. 14. The turbine engine of claim 11, wherein said second sidewall is coupled to said exit guide vane between said inlet end and said mid-span portion. 15. The turbine engine of claim 11, wherein said exit guide vane comprises a first end wall and a second end wall and said mid-span portion is located therebetween. 16. A method of assembling a flow control assembly to a turbine engine comprising a compressor and a turbine, said method comprising: coupling a first control device to an exit guide vane of the compressor and the turbine;coupling a first sidewall of the first flow control device to an outlet end of exit guide vane and to a turbine vane of the turbine;coupling a second sidewall of the first flow control device to about a mid-span portion of the exit guide vane and to a turbine blade of the turbine;coupling a second flow control device comprising an orifice device to the exit guide vane and in flow communication with the first flow control device; andcoupling a controller to the second flow control device to control a cooling flow into the flow control assembly. 17. The method of claim 16, wherein coupling the second flow control device comprises coupling the orifice device to a mid-span portion of the exit guide vane. 18. The method of claim 16, wherein coupling the second flow control device further comprises coupling a meter device to a mid-span portion of the exit guide vane and in flow communication to the first flow control device. 19. The method of claim 16, wherein coupling the second flow control device further comprises coupling a meter device in flow communication to the first sidewall. 20. The method of claim 16, wherein coupling the second flow control device further comprises coupling a meter device in flow communication to the second sidewall.