A gas turbine engine transition duct 34 is used to convey exhaust gas and bypass air away from the engine, towards an exhaust nozzle (not shown). The duct 34 defines the outer extremity of the path for gas and/or air through the duct. The duct comprises a plurality of flat panel members 36 which together define the outer extremity of the path.
Improvements in or relating to gas turbine engine transition ducts
Verbesserungen an oder in Zusammenhang mit Gasturbinenüberleitkanälen
Améliorations de ou relatives à des conduits de transition sur un moteur à turbine à gaz
2017-11-15
Patent
Elektronische Ressource
Englisch
Flow-Control-Enabled Aggressive Turbine Transition Ducts and Engine System Analysis
British Library Conference Proceedings | 2006
|Flow-Control-Enabled Aggressive Turbine Transition Ducts and Engine System Analysis
Online Contents | 2007
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