A rotor assembly for a gas turbine engine, the rotor assembly has a disc supporting a plurality of radially extending blades. The blades define passages therebetween and each passage has an annulus filler assembly. The annulus filler assembly includes at l...

An annulus filler is provided for mounting to a rotor disc of a gas turbine engine and for bridging the gap between two adjacent blades attached to the rotor disc. The annulus filler has a body portion which defines an airflow surface for air being drawn t...

A gas turbine engine fan section (24) is disclosed that includes a hub (28). Circumferentially spaced fan blades (30) are supported on the hub (28). A spacer (40) is arranged between adjacent fan blades (30) and is operatively supported by the hub (28). Th...

A rotor assembly, particularly for a gas turbine, comprising: a plurality of rotor discs interconnected by an axially extending rim, the outside of the rim having a circumferential array of dovetail slots and the underside of the rim having a circumferenti...