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Home Navigation and GPS Closed-cavity-noise-suppressor

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 Closed cavity noise suppressor

Details
Inventors: Motsinger, Russell E.; Vdoviak, John W.;
Assignee: General Electric Company (Cincinnati, OH)
Primary Examiner: Fuller; Benjamin R.
Assistant Examiner:
Attorney, Agent or Firm: Squillaro; Jerome C.

An annular acoustic liner for gas turbine engine ducts comprising Helmholtz resonator chambers wherein the resonator's turnable neck length and chamber depth lie on a surface which is concentric to the liner centerline. In another embodiment of the invention the liner is generally rectangular and the resonator's turnable neck length and chamber depth lie on a surface which is parallel to the duct flow. A more particular embodiment of the invention the duct is an afterburner duct which may have a rectangular or circular cross section.

DETAILED DESCRIPTION Accordingly one form of the present invention provides A Helmholtz resonator-type chamber for attenuating noise in a duct containing a gas flow comprising a chamber and a neck wherein the tunable neck length and chamber resonating depth run in a plane parallel to the gas flow.
In one particular embodiment of the present invention the tunable neck length and chamber resonating depth run in a plane parallel to or concentric to and in the same direction as the gas flow.
In another particular embodiment of the present invention the tunable neck length and chamber resonating depth run in a plane parallel to or concentric to and in a direction perpendicular to the gas flow.
A more particular form of the present invention provides an acoustic liner for a gas turbine engine annular duct comprising a plurality of Helmholtz resonator-type chambers having neck lengths and chamber resonating depths running circumferentially with respect to the duct.
One embodiment of the present invention provides an acoustic liner for a gas turbine engine duct comprising a plurality of Helmholtz resonator type chambers having neck lengths and chamber resonating depths running circumferentially with respect to the duct and wherein the neck occupies a portion of said chamber nearest the gas flow.
Another embodiment of the present invention provides an acoustic liner for a gas turbine engine duct comprising a plurality of Helmholtz resonator type chambers having neck lengths and chamber resonating depths running axially with respect to the duct and wherein the neck occupies a portion of said chamber nearest the gas flow.
Yet Another embodiment of the present invention provides an acoustic liner for a gas turbine engine duct comprising a plurality of Helmholtz resonator type chambers having neck lengths and chamber resonating depths running parallel with respect to the duct and wherein the neck occupies a portion of said chamber nearest the gas flow.
Another more particular embodiment of the invention provides an acoustic liner for a gas turbine engine duct comprises a bifurcated compartment containing two resonating chambers and necks



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