Airfoil with large fillet and micro-circuit cooling

Details Airfoil with large fillet and micro-circuit cooling Airfoil with large fillet and micro-circuit cooling

2007-05-15

2007-05-15

Nguyen, Ninh H. (Department: 3745)

Fluid reaction surfaces (i.e., impellers)

With heating, cooling or thermal insulation means

Changing state mass within or fluid flow through working...

C416S19300A

Reexamination Certificate

active

10967558

ABSTRACT:
A gas turbine engine blade has a relatively large fillet to improve the characteristics of the air flow thereover. The fillet has a thin wall which partially defines a fillet cavity therebehind, and cooling air is provided to the fillet cavity and is then routed to the outer surface by way film cooling holes. Various design features are provided to enhance the effectiveness of the cooling air being provided to both the fillet cavity and other cavities within the blade.

REFERENCES:
patent: 4515526 (1985-05-01), Levengood
patent: 5382133 (1995-01-01), Moore et al.
patent: 5975851 (1999-11-01), Liang
patent: 6290463 (2001-09-01), Fargher et al.
patent: 6406260 (2002-06-01), Trindade et al.
patent: 7063506 (2006-06-01), Davison et al.
patent: 2003/0108423 (2003-06-01), Morgan et al.
patent: 2005/0265840 (2005-12-01), Levine et al.
patent: 1 013 877 (2000-06-01), None
patent: 1 128 024 (2001-08-01), None
patent: 1 262 631 (2002-12-01), None
patent: 872705 (1961-07-01), None

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