US 8,297,931 B2 · Annulus filler

Abstract

An annulus filler (101) is provided for mounting to a rotor disc (102) of a gas turbine engine and for bridging the gap between two adjacent blades attached to the rotor disc (102). The annulus filler (101) has an outer part (106) which defines an airflow surface for air being drawn through the engine, and a separate, support part (105) which is connectable to the outer part (106) and to the rotor disc (102) to support the outer part (106) on the rotor disc (102). The outer (106) and support parts (105) are configured to allow a procedure for mounting the annulus filler (101) to the rotor disc (102). In a first step the support part (105) is connected to the rotor disc (102) without the outer part (106), and in a subsequent second step the outer part (106) is connected to the support part (105).

Claims9

Dependent claims

An annulus filler 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,

wherein the annulus filler having an outer part which defines an airflow surface for air being drawn through the engine and a separate support part which is connectable to the outer part and to the rotor disc to support the outer part on the rotor disc,
wherein the support part spaces the outer part from the rotor disc and has an inter-engaging portion that in use connects to the rotor disc and has a further inter-engaging portion that in use connects to the outer part, and
wherein the inter-engaging portion that connects to the outer part is curved in an arc which matches a chordwise curvature of the adjacent blades.

Dependencies are inferred from the claim text.

Annulus filler

Life of this patent

Annulus filler

Life of this patent

Abstract

Claims9