Gas turbine with running gap control

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – Vane or deflector

Reexamination Certificate

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Details

C415S209300

Reexamination Certificate

active

10933257

ABSTRACT:
A gas turbine with several shroud segments (1) which enclose rotor blades (3) of a turbine wheel (5) as a seal, with the shroud segments (1) having at least a front and a rear attachment at the radially outward area of stator vane segments (7, 12), and with each of the stator vane segments (7, 12) being located at their radially inner area on a control ring (9, 10), wherein the stator vane segments (7, 12) are located on the control ring (9, 10) in a radially adjustable manner.

REFERENCES:
patent: 4688378 (1987-08-01), Harris
patent: 5141394 (1992-08-01), Donlan
patent: 5149250 (1992-09-01), Plemmons et al.
patent: 5224822 (1993-07-01), Lenahan et al.
patent: 5372476 (1994-12-01), Hemmelgarn et al.
patent: 5921749 (1999-07-01), McLaurin et al.
patent: 6095750 (2000-08-01), Ross et al.
patent: 3038603 (1980-10-01), None
patent: 2061396 (1981-05-01), None

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