Gas turbine combustor, gas turbine, and jet engine

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

Reexamination Certificate

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C181S213000

Reexamination Certificate

active

06973790

ABSTRACT:
For the purpose of reduced NOx gas emission, a gas turbine engine comprises a cylinder having a combustion region inside of the cylinder; a resonator having a cavity and provided around the surface of the cylinder and sound absorption holes formed on the cylinder and having opening ends on the cylinder.

REFERENCES:
patent: 4036324 (1977-07-01), Washbourne
patent: 4135603 (1979-01-01), Dean, III et al.
patent: 6530221 (2003-03-01), Sattinger et al.
patent: 6640544 (2003-11-01), Suenaga et al.
patent: 0 576 717 (1994-01-01), None
patent: 0 892 216 (1999-01-01), None
patent: 0 985 882 (2000-03-01), None
patent: 0 990 851 (2000-04-01), None
patent: 6-147485 (1994-05-01), None
patent: 6-173711 (1994-06-01), None
patent: 7-280270 (1995-10-01), None
patent: 11-141878 (1999-05-01), None
patent: 2000-265856 (2000-09-01), None
McGraw-Hill Encyclopedia of Science & Technology, 7thEdition, 1992, p. 616.

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