Gas turbine engine including a turbine braking device

Power plants – Combustion products used as motive fluid – With safety device

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415 9, 415123, F02C 700

Patent

active

050294393

ABSTRACT:
A gas turbine engine is provided with a braking device for stopping the compressor drive turbine if a common shaft interconnecting the turbine and compressor rotors breaks, the braking device including a conical ring carried by the turbine rotor at its downstream end and a structural member of a generally conical shape carried by the upstream end of the turbine exhaust casing such that the ring will frictionally interlock with the structural member if the shaft breaks.

REFERENCES:
patent: 3903690 (1975-09-01), Jones
patent: 3989407 (1976-11-01), Cunningham
patent: 4279575 (1981-07-01), Avery
patent: 4639188 (1987-01-01), Swadley
patent: 4639399 (1987-01-01), Aprigliano

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