Gas turbine

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – With runner shaft of specific shape or material

Reexamination Certificate

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C415S221000, C415S914000

Reexamination Certificate

active

06877953

ABSTRACT:
A gas turbine with a compressor area has a rotor shaft2to carry rotor blades1and a casing4to carry stator vanes3,with the related rotor blades1and stator vanes3forming an axial clearance space5between one another, wherein, in the area of the axial clearance space5,at least one wall of the rotor shaft2and/or of the casing4is provided with an arrangement of fins6which are inclined against the axial direction.

REFERENCES:
patent: 4086022 (1978-04-01), Freeman et al.
patent: 4645417 (1987-02-01), Wisler
patent: 5137419 (1992-08-01), Waterman
patent: 5762470 (1998-06-01), Gelmedov et al.

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