An annulus filler system bridges the gap between two adjacent blades attached to a rim of the rotor disc of a gas turbine engine. The system includes an annulus filler having a lid which extends between the adjacent blades and defines an airflow surface for air being drawn through the engine. The fi
An annulus filler system bridges the gap between two adjacent blades attached to a rim of the rotor disc of a gas turbine engine. The system includes an annulus filler having a lid which extends between the adjacent blades and defines an airflow surface for air being drawn through the engine. The filler also has a support body extending beneath the lid and terminating in an elongate foot which, in use, extends along a groove provided in the rim of the disc. The groove has a neck which prevents withdrawal of the foot through the neck in a radially outward direction of the disc. The system further includes a sleeve which, after installation of the filler, is slidably locatable into a gap between the foot and sides of the groove.
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1. An annulus filler system for bridging the gap between two adjacent blades attached to a rim of the rotor disc of a gas turbine engine, the system including: an annulus filler having a lid which extends between the adjacent blades and defines an airflow surface for air being drawn through the engi
1. An annulus filler system for bridging the gap between two adjacent blades attached to a rim of the rotor disc of a gas turbine engine, the system including: an annulus filler having a lid which extends between the adjacent blades and defines an airflow surface for air being drawn through the engine, and a support body extending beneath the lid and terminating in an elongate foot which, in use, extends along a groove provided in the rim of the disc, the groove having a neck which prevents withdrawal of the foot through the neck in a radially outward direction of the disc; anda sleeve which, after installation of the filler, is slidably locatable into a gap between the foot and sides of the groove,wherein the sleeve has one or more frangible zones located within the groove and contacting both the neck and the foot of the annulus filler, the frangible zone provides permanent deformation to allow a rocking movement of the filler about the foot in response to lateral movement of the adjacent blades which is at least of a magnitude to cause the adjacent blades to contact each other, the sleeve having a pair of first and second sidewalls, each of the first and second sidewalls extending between a stop and a respective sidewall free edge, at least one of the frangible zones being located along the first sidewall between the stop and the sidewall free edge of the first sidewall. 2. The annulus filler system according to claim 1, wherein: the foot is proportioned to pass through the neck of the groove in a radial direction on installation of the filler;the sleeve is proportioned to prevent withdrawal of the foot through the neck, after installation of the filler, in a radially outward direction of the disc, andthe sleeve is further configured to retain sufficient integrity after said permanent deformation to still prevent withdrawal of the foot through the neck in a radially outward direction of the disc. 3. The annulus filler system according to claim 1, wherein the frangible zone or zones are provided by a foamed material selected from the group comprising: phenolic or ceramic foam, or a plastic embrittled by the selective addition of hardener. 4. The annulus filler system according to claim 3, wherein the frangible zone is provided by a ceramic foam impregnated with a thermoplastic elastomer, a fluorocarbon, or a fluorosilicone. 5. The annulus filler system according to claim 1, wherein the sleeve is at least partially wire-reinforced or fibre-reinforced to maintain the integrity of the sleeve after the deformation. 6. The annulus filler system according to claim 5, wherein the wire or fibre reinforcement join the frangible zone to a spine or non frangible zone. 7. The annulus filler system according to claim 1, wherein a frangible zone is provided by a central section of the sleeve, the end sections being a non frangible zone. 8. The annulus filler system according to claim 1, wherein the sleeve is configured to protrude past the neck of the groove and to flare outwardly away from the support body. 9. The annulus filler system according to claim 8, wherein the sleeve protrudes past the neck of the groove and to flare outwardly away from opposing sides of the support body. 10. The annulus filler system according to claim 1, wherein the support body has a pair of side walls, each side wall joining a respective edge of the lid to the foot to give the support body a V-shaped cross-section. 11. The annulus filler system according to claim 10, wherein the side walls are formed from fibre-reinforced plastic. 12. The annulus filler system according to claim 10, wherein a cavity formed by the lid and the two side walls contains a foam core. 13. A rotor assembly for a gas turbine engine including: a rotor disc,a plurality of blades attached to a rim of the disc of a gas turbine engine, andannulus filler systems according to claim 1 bridging the gaps between adjacent blades;wherein respective grooves are provided in the rim, the feet of the annulus fillers extending along the grooves, and the sleeves being located in the gaps between the feet and the sides of the grooves. 14. The annulus filler system according to claim 1, wherein the stop and the sidewall free edge of the first sidewall have no frangible zones such that, upon the permanent deformation to allow the rocking movement, deformation occurs at the at least one frangible zone but not at the stop or the sidewall free edge of the first sidewall. 15. The annulus filler system according to claim 1, wherein the sidewall free edge is outside the groove.
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이 특허에 인용된 특허 (18)
Anderson Bernard J. (Danvers MA), Anti-fretting blade retention means.
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