RETAINING ASSEMBLY AND RETAINING SEAL ASSEMBLY FOR RETAINING TURBINE NOZZLE ASSEMBLY
PROBLEM TO BE SOLVED: To provide a method for assembling a turbine nozzle assembly 12 to a combustor of a gas turbine engine 10. SOLUTION: This method includes a stage of coupling a radial outer retaining ring 102 to a rear end part 108 of the combustor. A plurality of turbine nozzles are prepared....
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