Gas Turbine Engine Stator Vane Assembly

A method of assembling gas turbine engine front architecture (36) includes positioning inner and outer fairings (40,42) relative to one another. Multiple vanes (44) are arranged circumferentially between the inner and outer fairings (40,42). A liquid sealant (74,80) is applied around a perimeter (72...

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Bibliographische Detailangaben
Hauptverfasser:	FEIGLESON, STEVEN J, TREMBLAY, DENNIS R, EDWARDS, WILLIAM R
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A method of assembling gas turbine engine front architecture (36) includes positioning inner and outer fairings (40,42) relative to one another. Multiple vanes (44) are arranged circumferentially between the inner and outer fairings (40,42). A liquid sealant (74,80) is applied around a perimeter (72,78) of the vanes (44) to seal between the vanes (44) and at least one of the fairings (40,42).