Method and apparatus for cooling combustor liner and...

Power plants – Combustion products used as motive fluid – Combustion products generator

Reexamination Certificate

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C060S754000, C060S760000

Reexamination Certificate

active

07010921

ABSTRACT:
A method and apparatus for cooling a combustor liner and transitions piece of a gas turbine include a combustor liner with a plurality of circular ring turbulators arranged in an array axially along a length defining a length of the combustor liner and located on an outer surface thereof; a first flow sleeve surrounding the combustor liner with a first flow annulus therebetween including a plurality of axial channels (C) extending over a portion of an aft end portion of the liner parallel to each other, the cross-sectional area of each channel either constant or varying along the length of the channel, the first flow sleeve having a plurality of rows of cooling holes formed about a circumference of the first flow sleeve for directing cooling air from the compressor discharge into the first flow annulus; a transition piece connected to the combustor liner and adapted to carry hot combustion gases to a stage of the turbine; a second flow sleeve surrounding the transition piece a second plurality of rows of cooling apertures for directing cooling air into a second flow annulus between the second flow sleeve and the transition piece; wherein the first plurality of cooling holes and second plurality of cooling apertures are each configured with an effective area to distribute less than 50% of compressor discharge air to the first flow sleeve and mix with cooling air from the second flow annulus.

REFERENCES:
patent: 3349558 (1967-10-01), Smith
patent: 4191011 (1980-03-01), Sweeney et al.
patent: 4195475 (1980-04-01), Verdouw
patent: 4232527 (1980-11-01), Reider
patent: 4236378 (1980-12-01), Vogt
patent: 4653279 (1987-03-01), Reynolds
patent: 4719748 (1988-01-01), Davis et al.
patent: 4864827 (1989-09-01), Richardson et al.
patent: 4903477 (1990-02-01), Butt
patent: 4916905 (1990-04-01), Havercroft et al.
patent: 5094069 (1992-03-01), Boffo
patent: 5181377 (1993-01-01), Napoli et al.
patent: 5329773 (1994-07-01), Myers et al.
patent: 5461866 (1995-10-01), Sullivan et al.
patent: 5758504 (1998-06-01), Abreu et al.
patent: 5802841 (1998-09-01), Maeda
patent: 5974805 (1999-11-01), Allen
patent: 6098397 (2000-08-01), Glezer et al.
patent: 6134877 (2000-10-01), Alkabie
patent: 6170266 (2001-01-01), Pidcock et al.
patent: 6408628 (2002-06-01), Pidcock et al.
patent: 6484505 (2002-11-01), Brown et al.
patent: 6494044 (2002-12-01), Bland
patent: 6530225 (2003-03-01), Hadder
patent: 6681578 (2004-01-01), Bunker
patent: 6718774 (2004-04-01), Razzell
patent: 6772595 (2004-08-01), Martling et al.
patent: 2004/0079082 (2004-04-01), Bunker

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