Platforms with curved side edges and gas turbine engine systems involving such platforms

Platforms with curved side edges and gas turbine engine systems involving such platforms are provided. In this regard, a representative airfoil assembly for a gas turbine engine includes: a platform having a gas path side, a non-gas path side, a leading edge, a trailing edge, a first side edge exten...

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Bibliographische Detailangaben

Hauptverfasser:	Spangler, Brandon W, Beattie, Jeffrey S, Hjelm, Scott D
Format:	Patent
Sprache:	eng
Online-Zugang:	Volltext bestellen
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