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COMBUSTOR LINER AND METHOD OF OPERATING SAME
A gas turbine combustor liner (20) delimits a combustion chamber (24) and has at least one monolithic ceramic block (30) having a first face (42) exposed to the combustion chamber (24) and a second face opposite the first face (42), and a 3D fabric of ceramic fibers (28) partially embedded inside the monolithic ceramic block (30), and partially extending outside the second face of the monolithic ceramic block (30), away from the combustion chamber (24).
COMBUSTOR LINER AND METHOD OF OPERATING SAME
A gas turbine combustor liner (20) delimits a combustion chamber (24) and has at least one monolithic ceramic block (30) having a first face (42) exposed to the combustion chamber (24) and a second face opposite the first face (42), and a 3D fabric of ceramic fibers (28) partially embedded inside the monolithic ceramic block (30), and partially extending outside the second face of the monolithic ceramic block (30), away from the combustion chamber (24).
COMBUSTOR LINER AND METHOD OF OPERATING SAME
BRENNKAMMERAUSKLEIDUNG UND VERFAHREN ZU DEREN BETRIEB
CHEMISE DE CHAMBRE DE COMBUSTION ET SON PROCÉDÉ DE FONCTIONNEMENT
LEBEL LARRY (Autor:in)
20.12.2023
Patent
Elektronische Ressource
Englisch
Heat Transfer Study on Liner Wall of Heat Recirculating Combustor
Springer Verlag | 2019
|Heat Transfer Study on Liner Wall of Heat Recirculating Combustor
Online Contents | 2019
|