Combustion chamber for gas turbine engine

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

Reexamination Certificate

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Reexamination Certificate

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07076956

ABSTRACT:
A combustion chamber suitable for a gas turbine engine is provided with at least one Helmholtz resonator having a resonator cavity and a damping tube in flow communication with the chamber interior. The damping tube is provided with at least one cooling hole extending through its wall for improved damping and cooling.

REFERENCES:
patent: 2807931 (1957-10-01), Bodine, Jr.
patent: 3982392 (1976-09-01), Crow
patent: 4216651 (1980-08-01), Ormerod
patent: 4786188 (1988-11-01), Myhre et al.
patent: 5285630 (1994-02-01), Ansart et al.
patent: 5373695 (1994-12-01), Aigner et al.
patent: 5431008 (1995-07-01), Ross et al.
patent: 5685157 (1997-11-01), Pandalai et al.
patent: 6354733 (2002-03-01), Glasheen et al.
patent: 6370879 (2002-04-01), Stalder et al.
patent: 6530221 (2003-03-01), Sattinger et al.
patent: 2288660 (1995-10-01), None

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