Methods and apparatus for assembling turbine engines

A method facilitates the assembly of a gas turbine engine. The method of assembly comprises providing a turbine nozzle including an inner band, an outer band, at least one vane extending between the inner and outer bands, and at least one leading edge fillet extending between the at least one vane a...

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Bibliographic Details
Main Authors Lee, Ching-Pang, Guentert, Joseph M, Lu, Wenfeng, Iles, Mitchell E
Format Patent
LanguageEnglish
Published 12.07.2011
Online AccessGet full text

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