Gas turbine engine exhaust mixer

An exhaust mixer for a gas turbine engine includes an annular wall having upstream end adapted to be fastened to an engine case and a downstream end forming a plurality of inner and outer mixer lobes. A support member interconnects at least a number of the inner lobes, and includes a circumferential...

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Bibliographische Detailangaben
Hauptverfasser: Bouchard, Richard, Grivas, Nicolas, Durocher, Eric, Leclair, Denis, Lefebvre, Guy
Format: Patent
Sprache:eng
Schlagworte:
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