Connecting system for a transition duct in a gas turbine

Details Connecting system for a transition duct in a gas turbine Connecting system for a transition duct in a gas turbine

2005-05-17

2005-05-17

Look, Edward K. (Department: 3745)

Rotary kinetic fluid motors or pumps

With passage in blade, vane, shaft or rotary distributor...

C415S214100, C415S097000, C060S039300

Reexamination Certificate

active

06893209

ABSTRACT:
A system for connecting a low-pressure jet to a transition duct in a gas turbine, in which the said low-pressure jets are arranged in sectors of two or three stator blades and are filled on to the ring of the jets. The platforms of the jets are provided with a channel inside which the transition duct is positioned by means of an edge. Furthermore, centering between the transition duct and the ring of the jets is achieved directly using centering means at three or more points.

REFERENCES:
patent: 4191011 (1980-03-01), Sweeney et al.
patent: 4901522 (1990-02-01), Commaret et al.
patent: 6139263 (2000-10-01), Klingels
patent: 369680 (1932-03-01), None
patent: 689270 (1953-03-01), None

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