Gas turbine engine component

A gas turbine engine component such as a high pressure turbine nozzle guide vane (NGV) or blade includes an external wall which is exposed to hot gas flowing through the engine. The component includes an air inlet arrangement 42 and effusion (film) cooling holes 46 formed in the external wall. Air i...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ANTHONY JOHN RAWLINSON, PETER IRELAND, IAN TIBBOTT
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04 LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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