Turbomachine comprising thermal deformation means

F - Mech Eng,Light,Heat,Weapons – 01 – D

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170/70

F01D 9/00 (2006.01) F01D 11/24 (2006.01) F01D 25/12 (2006.01)

Patent

CA 2027283

Cooling and heating mechanisms are associated with a restricted peripheral zone in a turbomachine stator in such way that a peripherally irregular distribution of temperatures results in a deformation of the stator which mirrors the rotor deformations during various phases of the use of the turbomachine. The longitudinal axes (R,5) of the stator and rotor are thus coincident.

Des moyens de refroidissement ou réchauffement sont associés à une zone périphérique limitée de stator de turbomachine de manière qu'une répartition périphériquement non uniforme des températures entraîne une déformation du stator qui reproduise les déformations du rotor à diverses phases d'utilisation de la turbomachine. Les axes longitudinaux (R,5) des stator et rotor sont ainsi confondus.

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