Patent US4231447A successfully refreshed from Google Patents.
US4231447A
Expired / Lapsed
US
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Multi-layer acoustic linings
Assignee: Rolls Royce PLC
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Filing: 1979-03-20
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Granted: 1980-11-04
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Expires: 1999-03-20
Abstract
Abstract A multi-layer acoustic lining is of the type having core compartments rendered effective as Helmholtz resonators by means of resonator necks projecting from the core facing layer into the core compartments. In order to broaden the frequency response, those ends of the resonator necks which project into the core compartments are bevelled so as to give the necks a less well defined length. The acoustic lining is particularly for application to the jet pipe or fan duct of a turbofan aeroengine.
Inventors
- 👤 John F. Chapman
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 08:09
CPC Classifications
G; G10; G10K; G10K11/00; G10K11/16; G10K11/172; F; F01; F01N; F01N1/00; F01N1/02; F02; F02K; F02K1/00; F02K1/78; F02K1/82; F02K1/827; F01N2490/00; F01N2490/15; F01N2490/155
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
137 words
For a fluid-flow duct in a gas turbine engine, a multi-layer acoustic lining comprising an air-impermeable backing layer, a compartmented-airspace core structure, a core facing layer overlying said core structure and incorporating apertures having predetermined cross-sections through which sound energy can enter the core, and tube-like Helmholtz resonator necks having bodies with cross-sections substantially the same as the cross-sections of said apertures which extend from said apertures into said core structure such that an end of each resonator neck is situated within a core compartment and spaced from walls thereof to thereby render core compartments effective as Helmholtz resonators; wherein the improvement is that said end of each resonator neck within said core structure is a biased configuration such that said end lies in a plane extending at an acute angle with the body of said neck.
Claim 2
Dependent Claim
137 words
For a fluid-flow duct in a gas turbine engine, a multi-layer acoustic lining comprising an air-impermeable backing layer, a compartmented-airspace core structure, a core facing layer overlying said core structure and incorporating apertures having predetermined cross-sections through which sound energy can enter the core, and tube-like Helmholtz resonator necks having bodies with cross-sections substantially the same as the cross-sections of said apertures which extend from said apertures into said core structure such that an end of each resonator neck is situated within a core compartment and spaced from walls thereof to thereby render core compartments effective as Helmholtz resonators; wherein the improvement is that said end of each resonator neck within said core structure is a biased configuration such that said end lies in a plane extending at an acute angle with the body of said neck.
Claim 3
Dependent Claim
38 words
A multi-layer acoustic lining as claimed in claim 1 in which the predetermined cross-sections of said apertures in the core facing layer are circular and in which the bodies of said tube-like resonator necks are of circular cross-section.
Claim 4
Dependent Claim
61 words
A multi-layer acoustic lining as claimed in claim 1 in which the core facing layer comprises an air-permeable sheet material, which, apart from the apertures therein, has a resistance to airflow therethrough sufficiently high to render the acoustic lining suitable for absorbing a frequency band appreciably higher than the frequency band absorbed by the lining when acting in the Helmholtz mode.
Claim 5
Dependent Claim
22 words
A multi-layer acoustic lining as claimed in claim 3 in which the air-permeable sheet material is a metal felt or the like.
Claim 6
Dependent Claim
59 words
A multi-layer acoustic lining as claimed in claim 1 in which the core facing layer comprises an air-impermeable sheet material, which, besides having the apertures therein, is also provided with perforations therethrough to render the acoustic lining suitable for absorbing a frequency band appreciably higher than the frequency band absorbed by the lining when acting in the Helmholtz mode.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-11-04 | 1984-05-05 | 1984-11-04 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-11-04 | 1988-05-05 | 1988-11-04 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-11-04 | 1992-05-05 | 1992-11-04 | $7700.00 | Window Closed / Lapsed |