Reduction of play in a gas turbine

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

Patent

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Details

F01D 11/16 (2006.01) F01D 5/20 (2006.01) F01D 7/02 (2006.01)

Patent

CA 2463182

A gas turbine, in particular a high pressure turbine for an airplane engine, the turbine comprising moving blades with tips that are fitted with radially slidable stubs for being pressed in operation by centrifugal forces against the inside surface of the casing of the turbine in order to eliminate radial clearance between said surface and the tips of the blades.

Turbine à gaz, en particulier turbine haute pression pour moteur d'aéronef, comprenant des aubes mobiles dont les sommets sont équipés de talons radialement coulissants destinés à être appliqués en fonctionnement par des forces centrifuges sur la surface intérieure du carter de la turbine pour supprimer les jeux radiaux entre cette surface et les sommets des aubes.

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