Gas turbine vane with enhanced cooling

Power plants – Combustion products used as motive fluid – Combustion products generator

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415115, 416 97R, F01D 518

Patent

active

054888255

ABSTRACT:
A gas turbine stationary vane having an airfoil portion and inner and outer shrouds. Five serpentine radially extending cooling air passages are formed in the vane airfoil. The first passage is disposed adjacent the leading edge of the airfoil and the second passage is disposed adjacent the trailing edge. A first portion of the cooling air enters the first passage, from which it flows sequentially to the second, third, fourth and fifth passages. Additional cooling air enters the third passage directly, thereby bypassing the first and second passages and preventing over heating of the cooling air by the time it reaches the fifth passage. A radial tube extends through the second passage and directs cooling air through the airfoil, with essentially no rise in temperature, to an interstage cavity for disc cooling. Fins project into each of the passages and serve to increase the effectiveness and flow rate of the cooling air. The fins in the first and fifth passages are angled so as to direct the cooling air toward the leading and trailing edges, respectively. In addition, the fins in the second through fifth passages are angled to retard flow separation as the cooling air turns 180.degree. from one passage to the next.

REFERENCES:
patent: 3171631 (1965-03-01), Aspinwall
patent: 3628885 (1971-12-01), Sidenstick
patent: 3834831 (1974-09-01), Mitchell
patent: 4073599 (1978-02-01), Allen et al.
patent: 4292008 (1981-09-01), Grosjean
patent: 4416585 (1983-11-01), Abdel-Messeh
patent: 4456428 (1984-06-01), Cuvillier
patent: 4474532 (1984-10-01), Pazder
patent: 4514144 (1985-04-01), Lee
patent: 4604031 (1986-08-01), Moss et al.
patent: 4775296 (1988-10-01), Schwarzmann et al.
patent: 4786233 (1988-11-01), Shizuya et al.
patent: 4930980 (1990-06-01), North et al.
patent: 4940388 (1990-07-01), Lilleker et al.
patent: 4962640 (1990-10-01), Tobery
patent: 4992026 (1991-02-01), Ohtomo et al.
patent: 5052889 (1991-10-01), Abdel-Messeh
patent: 5117626 (1992-06-01), North et al.
patent: 5145315 (1982-09-01), North et al.
patent: 5203873 (1993-04-01), Corsmeier et al.
patent: 5246341 (1993-09-01), Hall et al.
patent: 5320483 (1994-06-01), Cunha et al.
patent: 5387085 (1995-02-01), Thomas, Jr. et al.
patent: 5387086 (1995-02-01), Frey et al.
patent: 5395212 (1995-03-01), Anzai et al.
Lau et al., "Heat Transfer Characteristics of Turbulent Flow in a Square Channel with Angled Discrete Ribs", ASME 90-GT-254, Gas Turbine and Aeroengine Congress and Exposition, American Society of Mechanical Engineers, Jun. 1990.
Han et al., "Effect of Rib-Angle Orientation on Local Mass Transfer Distribution in a Three-Pass Rib-Roughened Channel", 89-GT-98, Gas Turbine and Aeroengine Congress and Exposition, American Society of Mechanical Engineers, Jun. 1989.

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