Gas turbine combustor

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

Reexamination Certificate

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Reexamination Certificate

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07032386

ABSTRACT:
A combustor for a gas turbine has an arrangement to form a layer of cooling-air on an inner surface of a liner of a combustion chamber. This layer of the cooling air extends from a fuel nozzle block of the combustor toward a downstream side with respect to the liner.

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patent: 2860483 (1958-11-01), Fox
patent: 3359724 (1967-12-01), Barnwell et al.
patent: 3854285 (1974-12-01), Stenger et al.
patent: 5239831 (1993-08-01), Kuroda et al.
patent: 5479772 (1996-01-01), Halila
patent: 5836164 (1998-11-01), Tsukahara et al.
patent: 6105372 (2000-08-01), Mandai et al.
patent: 1001224 (2000-05-01), None
patent: 2 134 243 (1984-08-01), None
patent: 8-285284 (1996-11-01), None

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