Gas turbine having a ceramic rotor

Claim 1

In a gas turbine power plant comprising a compressor, a first turbine rotor mounted upon the shaft as, and imparting rotary movement to said compressor, at least one further turbine rotor mounted upon a shaft separate from that of said first turbine rotor and compressor combination, and at least one combustion chamber having fuel supply means, receiving air from the compressor and supplying combustion gas to said first and at least one further turbine rotor, the improvement comprising said shaft mounting said first turbine rotor and said compressor, being hollow, said first turbine rotor being manufactured of ceramic material and being provided with an integral stub shaft introduced into the void at the end of said hollow shaft, means including a resilient clamping member and a tightening rod connected integrally therewith at one end to said clamping member for retaining said stub shaft to said hollow shaft, said clamping member having a corrugated sleeve portion enclosing said stub shaft, means for preventing relative rotation during torque transfer including said stub shaft, said corrugated sleeve and said void at the end of said hollow shaft all having mating, but successively bigger polygonal cross sections.