Gas seal vanes of variable nozzle turbine

F - Mech Eng,Light,Heat,Weapons – 02 – D

Patent

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123/21

F02D 23/00 (2006.01) F01D 17/16 (2006.01) F02B 37/24 (2006.01)

Patent

CA 1222915

ABSTRACT A turbocharger having a variable nozzle vane assembly to be used in association with an engine. A nozzle ring having a plurality of rotatable vanes mounted thereto defining an annular passageway within the turbine housing through which exhaust gas passes upstream of a turbine. Included is a means for rotating the plurality of vanes and a means for preventing binding of the components during thermal cycling.

476183

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