Tube-type vortex reducer with retaining ring

Rotary kinetic fluid motors or pumps – With passage in blade – vane – shaft or rotary distributor...

Reexamination Certificate

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C416S24400R

Reexamination Certificate

active

07086830

ABSTRACT:
A tube-type vortex reducer conducts cooling air in a compressor (1) of a gas turbine. Radial secondary air tubes (2) are arranged in a disk interspace (5) and attached to a compressor disk (3) with their radial outward end sections. The end sections of the secondary air tubes (2) are attached to a separate carrier ring (6), which is connected to a compressor disk (3).

REFERENCES:
patent: 2772069 (1956-11-01), Hockert et al.
patent: 2917276 (1959-12-01), Klompas et al.
patent: 4034558 (1977-07-01), Korta et al.
patent: 4576547 (1986-03-01), Weiner et al.
patent: 5482431 (1996-01-01), Taylor
patent: 6397604 (2002-06-01), Eldrid et al.
patent: 6648592 (2003-11-01), Escure et al.
patent: 2002/0182059 (2002-12-01), Escure et al.
patent: 2003/0101730 (2003-06-01), Hein et al.
patent: 4216031 (1993-10-01), None
patent: 10159670 (2003-06-01), None
German Search Report dated Mar. 12, 2003.

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