Cambered vane for use in turbochargers

Rotary kinetic fluid motors or pumps – Selectively adjustable vane or working fluid control means – Upstream of runner

Reexamination Certificate

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Details

C415S164000

Reexamination Certificate

active

07001143

ABSTRACT:
Improved cambered vanes comprise an inner airfoil surface oriented adjacent a turbine wheel, and an outer airfoil surface oriented opposite the inner airfoil surface. The inner and outer airfoil surfaces define a vane airfoil thickness. A cambered vane leading edge or nose is positioned along a first inner and outer airfoil surface junction, and a vane trailing edge positioned along a second inner and outer surface junction. The vane airfoil surfaces, in conjunction with the vane leading edge, are specifically configured to provide a vane camberline, measured between the airfoil surfaces and extending along a length of the vane, having a gradually curved section and a substantially flat section.

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Fukaya and Watanabe: “Compressible Turbulent Flow Analysis On Variable Nozzle Vane and Spacer in Turbocharger Turbine;” SAE International; Mar. 2000; pp. 1-7; Volume-issue No. 2000-02-0526; SAE Technical Paper Series, Warrendale, PA.

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