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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Bibliographische Detailangaben
Hauptverfasser: CHAN SZE BUN B, GREENE JOHN E, ARNESS BRIAN P
Format: Patent
Sprache:eng
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