STRUCTURAL SUPPORT BRACKET FOR GAS FLOW PATH

A structural support system is provided in a can annular gas turbine engine having an arrangement including a plurality of integrated exit pieces (IEPs) forming an annular chamber for delivering gases from a plurality of combustors to a first row of turbine blades. A bracket structure is connected b...

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Bibliographische Detailangaben
Hauptverfasser: MAYER, CLINTON, A, CHARRON, RICHARD, C, PANKEY, WILLIAM, W, HETTINGER, BENJAMIN, G
Format: Patent
Sprache:eng ; fre
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