Systems and methods for cooling gas turbine engine...

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

Reexamination Certificate

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C060S760000, C060S754000

Reexamination Certificate

active

07954326

ABSTRACT:
A gas turbine engine assembly includes a combustor configured to combust an air-fuel mixture to produce combustion gases in a first direction; a transition liner coupled to the combustor and adapted to receive the combustion gases from the combustor and to redirect the combustion gases in a second direction; and a turbine coupled to the transition liner and adapted to receive the combustion gases from the transition liner. The transition liner has a plurality of effusion holes that include a first group that extend at least partially in a tangential direction.

REFERENCES:
patent: 3844116 (1974-10-01), Matto
patent: 3869864 (1975-03-01), Bunn
patent: 5237813 (1993-08-01), Harris et al.
patent: 5323602 (1994-06-01), Defever
patent: 5918467 (1999-07-01), Kwan
patent: 6155056 (2000-12-01), Sampath et al.
patent: 6408629 (2002-06-01), Harris et al.
patent: 6655149 (2003-12-01), Farmer et al.
patent: 6810672 (2004-11-01), Coutandin
patent: 6925810 (2005-08-01), Swaffar
patent: 6955053 (2005-10-01), Chen et al.
patent: 7146816 (2006-12-01), Anderson et al.
patent: 7155913 (2007-01-01), Beule et al.
patent: 7260936 (2007-08-01), Patel et al.
patent: 7269958 (2007-09-01), Stastny et al.
patent: 7302801 (2007-12-01), Chen
patent: 7350358 (2008-04-01), Patel et al.
patent: 7624577 (2009-12-01), Patel et al.
patent: 7628020 (2009-12-01), Alkabie et al.
patent: 2006/0037323 (2006-02-01), Reynolds et al.
patent: 2006/0042257 (2006-03-01), Stastny
patent: 2006/0272335 (2006-12-01), Schumacher et al.
patent: 2007/0130953 (2007-06-01), Burd et al.
patent: 2007/0169484 (2007-07-01), Schumacher et al.
patent: 2010/0050650 (2010-03-01), Patel et al.

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