Vane ring thermal strain relief cuts

Vane ring thermal strain relief cuts

A product for a turbocharger assembly is disclosed. A turbine wheel assembly may be adapted to rotate when exposed to a flow of gas. A vane ring may be disposed in the turbine wheel assembly. A plurality of vanes may be mounted to the vane ring. The flow of gas may meet the plurality of vanes at an...

Ausführliche Beschreibung

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Bibliographische Detailangaben
1. Verfasser: KENNEDY DONALD MICHAEL
Format: Patent
Sprache:eng
Schlagworte:
BLASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
STEAM ENGINES
WEAPONS
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Beschreibung
Zusammenfassung:A product for a turbocharger assembly is disclosed. A turbine wheel assembly may be adapted to rotate when exposed to a flow of gas. A vane ring may be disposed in the turbine wheel assembly. A plurality of vanes may be mounted to the vane ring. The flow of gas may meet the plurality of vanes at an angle of incidence. The plurality of vanes may be adjustable to selectively change the angle of incidence. The vane ring may have at least one slot adapted to direct a thermal deformation of the vane ring in a selected direction when exposed to the flow of gas.