Turbine ring for a gas turbine engine

Rotary kinetic fluid motors or pumps – With diversely oriented inlet or additional inlet for...

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415171, F04D 2958

Patent

active

046799818

ABSTRACT:
A turbine ring has an annular metallic carrier which is mounted within the inside of the turbine casing and within the carrier there is provided a ceramic abradable ring. A cooling air circuit is provided to regulate the temperature of only the annular carrier such that the latter always exerts a centripetal compression force on the ring under all operational conditions of the gas turbine to clamp the abradable ring.

REFERENCES:
patent: 3583824 (1971-06-01), Smuland
patent: 4087199 (1978-05-01), Hemsworth
patent: 4329113 (1982-05-01), Ayache et al.
patent: 4379677 (1983-04-01), Hallinger et al.
patent: 4497610 (1985-02-01), Richardson et al.
patent: 4551064 (1985-11-01), Pask

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