Method and apparatus for assembling turbine nozzle assembly
A turbine nozzle assembly and a method for assembling the turbine nozzle assembly with respect to a combustor of a gas turbine engine are provided. The method includes coupling a radial outer retaining ring to an aft end of the combustor. A plurality of turbine nozzles are provided. Each turbine noz...
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Format: | Patent |
Sprache: | eng |
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