Unitized manufacturing of a gas turbine engine

A unitized build assembly for a gas turbine engine includes an exhaust duct, a hot section with a locking structure and including a combustor and turbine section. The hot section at least partially circumferentially surrounds the exhaust duct. The build assembly includes a compressor section with an...

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Bibliographische Detailangaben
Hauptverfasser: Morganson, David W, Boyer, Jesse R, Binek, Lawrence A
Format: Patent
Sprache:eng
Schlagworte:
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