Turbine module for a gas turbine engine

Rotary kinetic fluid motors or pumps – Bearing – seal – or liner between runner portion and static part – Labyrinth seal

Reexamination Certificate

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Details

C415S009000

Reexamination Certificate

active

07364402

ABSTRACT:
A turbine module for a gas turbine engine includes at least one turbine disk and a disk-shaped component mounted on the turbine disk upstream relative to the gas flow. The module can be assembled to the compressor of the engine, wherein the component is preassembled to the turbine disk, before the module is assembled to the compressor, by bolting to an attachment flange fixedly attached to the turbine disk.

REFERENCES:
patent: 5816776 (1998-10-01), Chambon et al.
patent: 6893222 (2005-05-01), Allam
patent: 7210909 (2007-05-01), Escure et al.
patent: 0 541 250 (1993-05-01), None
patent: 0 718 469 (1996-06-01), None
patent: 2 857 419 (2005-01-01), None

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