Annulus filler for gas turbine engine rotor disc

An annulus filler (interblade platform) for bridging the gap between two adjacent blades, eg fan blades, attached to the rotor disc 51 of a gas turbine engine has a body portion 52, eg of composite material, with a lid portion 53 defining an airflow surface for air being drawn through the engine. A...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	KRISTOFER JOHN BOTTOME
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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