US4433751A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Sound suppressor liner
Assignee: Pratt and Whitney Canada Corp
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Filing: 1981-12-09
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Granted: 1984-02-28
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Expires: 2001-12-09
Abstract
Abstract A sound suppressor liner for aircraft exhaust passages is described which is based on the Helmholtz resonator principle including an inlet passage leading into a closed cavity wherein the inlet passages defined by a pair of curved walls with one wall being concave and the other wall being convex and the space between the walls gradually diminishing from the inlet of the inlet passage to the outlet within the cavity in a sense simulating an acoustic horn in reverse.
Inventors
- 👤 Hilaire Bonneau
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 05:38
CPC Classifications
F; F02; F02K; F02K1/00; F02K1/78; F02K1/82; F02K1/827
Claims Analysis
Total Claims: 7
Claim 1
Independent Claim
162 words
A suppressor liner comprising a first shell and a second shell spaced from the first shell with the second shell being permeable to sound and in contact with a gas path, sheet metal members forming a plurality of attenuator cells, each cell defining a cavity and having inlet passage means therein and constituting a battery of cells between the first shell and the second shell, the adjacent cells in the battery being formed by similarly formed sheet metal members with each member having a first concavely curved section relative to the second shell and forming a wall of the inlet passage of a first cell, a second continuing convexly curved section relative to the gas path and forming a portion of the cavity of a second cell with the first shell, an inwardly looped third section forming the convex wall of the inlet passage of the second cell such that each sheet metal member overlaps an adjacent member to form subsequent cells.
Claim 2
Dependent Claim
162 words
A suppressor liner comprising a first shell and a second shell spaced from the first shell with the second shell being permeable to sound and in contact with a gas path, sheet metal members forming a plurality of attenuator cells, each cell defining a cavity and having inlet passage means therein and constituting a battery of cells between the first shell and the second shell, the adjacent cells in the battery being formed by similarly formed sheet metal members with each member having a first concavely curved section relative to the second shell and forming a wall of the inlet passage of a first cell, a second continuing convexly curved section relative to the gas path and forming a portion of the cavity of a second cell with the first shell, an inwardly looped third section forming the convex wall of the inlet passage of the second cell such that each sheet metal member overlaps an adjacent member to form subsequent cells.
Claim 3
Dependent Claim
146 words
A sound suppressor liner adjacent a gas flow path, the liner including a first closed shell, a plurality of attenuator cells formed adjacent the first shell, each attenuator cell having wall means defining a cavity with the first shell and an inlet passage communicating at an inlet end with said gas flow path and leading into and communicating with said cavity, said wall means defining said inlet passage including at least a pair of curved walls with one wall being concave and the other being convex relative to the concave wall, with the space between the walls gradually diminishing from the inlet of the inlet passage towards the cavity, such that the curved walls simulate an acoustic horn, the volume of the cavity and the dimensions of the inlet passage are chosen as a function of the bandwidth of noise frequencies it is desired to attenuate.
Claim 4
Dependent Claim
146 words
A sound suppressor liner adjacent a gas flow path, the liner including a first closed shell, a plurality of attenuator cells formed adjacent the first shell, each attenuator cell having wall means defining a cavity with the first shell and an inlet passage communicating at an inlet end with said gas flow path and leading into and communicating with said cavity, said wall means defining said inlet passage including at least a pair of curved walls with one wall being concave and the other being convex relative to the concave wall, with the space between the walls gradually diminishing from the inlet of the inlet passage towards the cavity, such that the curved walls simulate an acoustic horn, the volume of the cavity and the dimensions of the inlet passage are chosen as a function of the bandwidth of noise frequencies it is desired to attenuate.
Claim 5
Dependent Claim
43 words
A sound suppressor liner as defined in claim 2, wherein the liner includes a second shell which is permeable to sound and air and is in contact with the gas path and covers the inlets of the inlet passages of the attenuator cells.
Claim 6
Dependent Claim
29 words
A suppressor liner as defined in claim 3, wherein the second shell which is permeable to sound is made of fiber sheet material such as fibrous or porous metal.
Claim 7
Dependent Claim
17 words
A sound suppressor liner as defined in claim 3, wherein the second shell is a perforated sheet.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1987-02-27 | 1987-08-29 | 1988-02-28 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1991-02-27 | 1991-08-29 | 1992-02-28 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1995-02-27 | 1995-08-29 | 1996-02-28 | $7700.00 | Window Closed / Lapsed |