Turbine blade with spar and shell

Fluid reaction surfaces (i.e. – impellers) – Specific blade structure – Formed with main spar

Reexamination Certificate

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Details

C416S24100B

Reexamination Certificate

active

07993104

ABSTRACT:
A turbine blade assembly with a spar and shell construction. The shell is held in place between a tip edge of the spar and an airfoil shaped groove on the platform surface. A segmented seal assembly is held within the groove between the shell bottom surface. The segmented seal has a top face slanted inward toward the spar to engage with a similar slanted surface formed on the bottom face of the shell. The seal segments fit within the groove to engage both side walls to form a tight seal interface between the shell bottom surface and the outer wall of the groove. The seal segments are forced upward against the slanted underside of the shell due to centrifugal forces from rotation. A cooling air passage to supply pressurized cooling air to the groove and the underside surface of the seal segments also can be used to force the seal segments up against the slanted underside of the shell. Forcing the seal segments up against the slanted shell underside also forces the seal segments outward from the spar to enhance the sealing interface with the wall groove to further enhance the sealing affect.

REFERENCES:
patent: 4473336 (1984-09-01), Coney et al.
patent: 4519745 (1985-05-01), Rosman et al.
patent: 4790721 (1988-12-01), Morris et al.
patent: 7080971 (2006-07-01), Wilson et al.
patent: 35 12 008 (1986-10-01), None

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