Cooled turbine vane platform

Details Cooled turbine vane platform Cooled turbine vane platform

2006-02-28

2006-02-28

Look, Edward K. (Department: 3745)

Rotary kinetic fluid motors or pumps

With passage in blade, vane, shaft or rotary distributor...

C416S09600A, C416S09700R

Reexamination Certificate

active

07004720

ABSTRACT:
A vane assembly for a gas turbine engine comprises a plurality of airfoils extending between platforms and a plurality of effusion holes which are defined in at least one of the inner and outer platforms in a region intermediate adjacent airfoils. The effusion holes provide fluid flow communication between a cooling air source and the gas path.

REFERENCES:
patent: 3610769 (1971-10-01), Schwedland et al.
patent: 4798514 (1989-01-01), Pask
patent: 4946346 (1990-08-01), Ito
patent: 5169287 (1992-12-01), Proctor et al.
patent: 5407319 (1995-04-01), Harrogate et al.
patent: 5417545 (1995-05-01), Harrogate
patent: 5470198 (1995-11-01), Harrogate et al.
patent: 6082961 (2000-07-01), Anderson et al.
patent: 6508620 (2003-01-01), Sreekanth et al.
patent: 6565317 (2003-05-01), Beeck et al.
patent: 2003/0002975 (2003-01-01), Dudebout et al.
patent: 1 221 536 (2002-07-01), None

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