Methods and apparatus for assembling gas turbine engines

A method enables a variable vane assembly for a gas turbine engine including a casing and an inner shroud to be assembled. The method comprises providing at least one variable vane including a radially inner spindle that has a substantially circular cross-sectional shape, and coupling the variable v...

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Bibliographische Detailangaben
Hauptverfasser: HEADLEY MITCHELL J, PELLETIER SCOTT H, BARBE ROGER O, ROSENOW DAVID N
Format: Patent
Sprache:eng
Schlagworte:
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