Curvature steam turbine vane airfoil

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Radial flow devices

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416DIG2, 415191, H01D 514

Patent

active

052922308

ABSTRACT:
A high performance steam turbine vane having a novel airfoil shape. The pressure surface of the airfoil has a substantially straight region proximate the trailing edge that provides the airfoil with adequate thickness to prevent distortion during forging. The novel shape on the suction surface is such that a first region of the suction surface downstream of the gauging point is essentially straight. Traveling in the upstream direction, the first region is followed by a second region that has a large amount of curvature. The second region is followed by a third region that has a lower curvature than the second region. The third region is followed by a fourth region of constantly increasing curvature that increases to a curvature greater than the curvature of the second region. The fourth region is followed by a fifth region, ending at the leading edge, of essentially constant large curvature that includes the maximum curvature throughout the suction surface.

REFERENCES:
patent: 3475108 (1969-10-01), Zickuhr
patent: 4080102 (1978-03-01), Schwab
patent: 4695228 (1987-09-01), Purcaru
patent: 4900230 (1990-02-01), Patel
patent: 4919593 (1990-04-01), Brown
patent: 4968216 (1990-11-01), Anderson et al.
patent: 5035578 (1991-07-01), Tran

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