Turbine module for gas turbine engine with rotor that...

Details Turbine module for gas turbine engine with rotor that... Turbine module for gas turbine engine with rotor that...

F - Mech Eng,Light,Heat,Weapons

01

D

F01D 5/06 (2006.01) F01D 5/34 (2006.01)

Patent

CA 2520069

L'invention porte sur un module de turbine pour un moteur à turbine à gaz avec un rotor (109) de turbine constitué de quatre disques au moins supportant des aubes à leur périphérie, deux desdits disques formant un corps monobloc. Le module est caractérisé par le fait que ledit corps monobloc (109') comprend deux viroles latérales inter disques (109BA, 109CD), les dites viroles étant boulonnées sur les disques (109A3, 109D3) des deux rotors adjacents au corps monobloc. L'invention s'applique en particulier aux modules de turbine comprenant de 4 à 6 étages de turbine.

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