Gas turbine vane with integral cooling system

Fluid reaction surfaces (i.e. – impellers) – With heating – cooling or thermal insulation means – Changing state mass within or fluid flow through working...

Reexamination Certificate

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C415S115000

Reexamination Certificate

active

10884441

ABSTRACT:
A turbine vane usable in a turbine engine and having at least one cooling system. The cooling system includes three diffusors in an outer wall of the vane for reducing the velocity of the cooling fluids exiting the turbine vane. One of the diffusors is formed from one or more cavities in an outer wall of the turbine vane for heat dissipation. The cavities may be supplied with cooling fluids from an internal cooling cavity through one or more interior metering orifices. The cooling fluids may exit the cooling cavity through one or more exterior metering orifices, which are second diffusors, and diffusion slots, which are third diffusors, that reduce the velocity of the cooling fluids and enable formation of a film cooling layer on the outer surface of the turbine vane.

REFERENCES:
patent: 4551064 (1985-11-01), Pask
patent: 4573865 (1986-03-01), Hsia et al.
patent: 4601638 (1986-07-01), Hill et al.
patent: 4664597 (1987-05-01), Auxier et al.
patent: 4726735 (1988-02-01), Field et al.
patent: 5169287 (1992-12-01), Proctor et al.
patent: 5368441 (1994-11-01), Sylvestro et al.
patent: 5405242 (1995-04-01), Auxier et al.
patent: 5584651 (1996-12-01), Pietraszkiewicz et al.
patent: 5772397 (1998-06-01), Morris et al.
patent: 6004095 (1999-12-01), Waitz et al.
patent: 6153889 (2000-11-01), Jones
patent: 6234754 (2001-05-01), Zelesky et al.
patent: 6402470 (2002-06-01), Kvasnak et al.
patent: 6616405 (2003-09-01), Torii et al.
patent: 6616406 (2003-09-01), Liang

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