Gas turbine with extraction-air conditioner
The present disclosure is directed to a gas turbine including a primary compressor, a combustion section disposed downstream from the primary compressor and a turbine disposed downstream from the combustion section. A pipe assembly defines an extraction-air circuit between an extraction port of the primary compressor and an inlet port of the turbine. The gas turbine further includes an extraction-air conditioning system. The extraction-air conditioning system includes a secondary compressor having an inlet and an outlet. Both the inlet and the outlet are fluidly coupled to the extraction-air circuit at respective locations defined along the pipe assembly between the extraction port of the primary compressor and the inlet port of the turbine.
1. A gas turbine, comprising:
a primary compressor, a combustion section disposed downstream from the primary compressor and a turbine disposed downstream from the combustion section, the turbine comprising an inner turbine casing enclosed within an outer turbine shell, wherein the inner turbine casing includes various cooling passages;
a pipe assembly defining an extraction-air circuit between an extraction port of the primary compressor and an inlet port of the turbine disposed on the outer turbine shell, wherein extraction-air flows through the extraction-air circuit from the primary compressor to the inlet port of the turbine and through the various cooling passages of the inner turbine casing;
an extraction-air conditioning system, the extraction-air conditioning system including a secondary compressor having an inlet and an outlet, wherein both the inlet and the outlet are fluidly coupled to the extraction-air circuit at respective locations defined between the extraction port of the primary compressor and the inlet port of the turbine; and,
a combustor module disposed on the extraction air circuit, the combustor module having a first inlet fluidly coupled to the extraction-air circuit, a second inlet immediately downstream the outlet of the secondary compressor and an outlet fluidly coupled to the extraction-air circuit downstream from the first inlet and upstream from the inlet port of the turbine, wherein all the extraction-air exiting the primary compressor flows through the combustor module.
2. The gas turbine as in claim 1 , wherein the combustor module includes a burner disposed downstream from the first inlet and the second inlet and upstream from the outlet of the combustor module.
3. The gas turbine as in claim 2 , wherein the burner is enveloped within the extraction-air flowing from the extraction port of the primary compressor and through the combustor module, wherein the extraction-air flows around the burner.
4. The gas turbine as in claim 2 , wherein a portion of the burner converges radially inwardly along an axial centerline of the burner proximate to an outlet end of the burner.
5. The gas turbine as in claim 1 , wherein the extraction-air conditioning system further comprises a mixing chamber disposed downstream from the extraction port of the primary compressor and upstream from the inlet port of the turbine.
6. the gas turbine as in claim 1 , wherein a first rotor shaft couples the primary compressor to the turbine.
7. The gas turbine as in claim 6 , further comprising a drive motor coupled to a second rotor shaft of the secondary compressor.
8. A gas turbine, comprising:
a primary compressor, a combustion section disposed downstream from the primary compressor and a turbine disposed downstream from the combustion section, the turbine comprising an inner turbine casing enclosed within an outer turbine shell, wherein the inner turbine casing includes various cooling passages;
a pipe assembly defining an extraction-air circuit between an extraction port of the primary compressor and an inlet port of the turbine, wherein the inlet port of the turbine is disposed on the outer turbine shell, and wherein extraction-air flows through the extraction-air circuit from the primary compressor to the inlet port of the turbine and through the various cooling passages of the inner turbine casing;
an extraction-air conditioning system, the extraction-air conditioning system including a combustor module disposed on the extraction-air circuit and having an inlet in direct fluid communication with the extraction port of the primary compressor and an outlet fluidly coupled to the inlet port of the turbine, wherein all the extraction-air exiting the primary compressor flows through the combustor module.
9. The gas turbine as in claim 8 , further comprising a mixing chamber disposed downstream from the outlet of the combustion module and upstream from the inlet port of the turbine.
10. The gas turbine as in claim 8 , wherein the combustor module includes a burner disposed downstream from the inlet and upstream from the outlet of the combustor module.
11. The gas turbine as in claim 10 , wherein the burner is enveloped within the extraction-air flowing from the extraction port of the primary compressor and through the combustor module, wherein the extraction-air flows around and cools the burner.
12. A gas turbine, comprising:
a primary compressor, a combustion section disposed downstream from the primary compressor and a turbine disposed downstream from the combustion section, the turbine comprising an inner turbine casing enclosed within an outer turbine shell, wherein the inner turbine casing includes various cooling passages;
a pipe assembly defining an extraction-air circuit between an extraction port of the primary compressor and an inlet port of the turbine, wherein the inlet port of the turbine is disposed on the outer turbine shell, and wherein extraction-air flows through the extraction-air circuit from the primary compressor to the inlet port of the turbine and through the various cooling passages of the inner turbine casing;
an extraction-air conditioning system, the extraction-air conditioning system including a secondary compressor having an inlet and an outlet, wherein both the inlet and the outlet are fluidly coupled to the extraction-air circuit at respective locations defined between the extraction port of the primary compressor and the inlet port of the turbine; and,
a combustor module disposed on the extraction-air circuit and having a first inlet fluidly coupled to the extraction-air circuit, a second inlet immediately downstream the outlet of the secondary compressor and an outlet fluidly coupled to the extraction-air circuit downstream from the first inlet and upstream from the inlet port of the turbine, wherein the combustor module includes a burner positioned within a combustor housing, the burner disposed downstream from the first inlet and the second inlet and upstream from the outlet of the combustor module, the combustor housing partially defining the extraction air circuit.
13. The gas turbine as in claim 12 , wherein the burner is enveloped within a flow of the extraction-air flowing from the extraction port of the primary compressor and through the combustor housing, wherein the extraction-air flows around the burner.
14. The gas turbine as in claim 13 , wherein a portion of the burner converges radially inwardly along an axial centerline of the burner proximate to an outlet end of the burner.