US4294329A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Double layer attenuation panel with two layers of linear type material
Assignee: Rohr Inc
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Filing: 1979-12-17
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Granted: 1981-10-13
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Expires: 1999-12-17
Abstract
Abstract A double degree acoustic attenuation sandwich panel having a plurality of stacked components adhered together to form a unitary sandwich structure. The structure comprising an impervious facing of thin sheet material, a first honeycomb core with end wise directed cells, a first perforate facing of thin sheet material, a first thin layer of porous fibrous material, a second perforated facing of thin sheet material, a second honeycomb core with end wise directed cells, a third perforate facing of thin sheet material, the second perforated facing sheet having substantially larger perforations than the first and third sheets, and a second layer of porous fibrous material. The resulting sandwich panel has a pre-determined flow through resistance between the outer surface of the first and second layers of porous fibrous material and the cells of the first and second honeycomb cores. The cells of the first and second honeycomb cores may be of equal or different volume and may be constructed of similar or dis-similar materials.
Inventors
- 👤 Philip M. Rose
- 👤 Frank J. Riel
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 06:39
CPC Classifications
E; E04; E04C; E04C2/00; E04C2/30; E04C2/34; E04C2/36; E04C2/365; B; B32; B32B; B32B3/00; B32B3/10; B32B3/12; G; G10; G10K; G10K11/00; G10K11/16; G10K11/172; Y; Y10; Y10T; Y10T428/00; Y10T428/24; Y10T428/24149; Y10T428/24165; Y10T428/24273; Y10T428/24322; Y10T428/24331
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
246 words
A double layer acoustical honeycomb sandwich panel having structural strength for use in the severe environment in and around high velocity fluid flow paths associated with aircraft gas turbine engines comprising: first and second honeycomb cores having a multiplicity of endwise directed cells with walls of thin sheet material disposed transversely to the panel; an impervious facing of thin sheet material; first, second and third facings of perforated thin sheet material; and first and second thin sheets of porous fibrous material; said impervious facing of this sheet material is adhesively bonded to one end wise cell face of said first honeycomb core; said first perforated facing of thin sheet material is adhesively bonded to said first honeycomb core on the surface opposite said impervious facing of this sheet material; said first thin sheet of porous fibrous material is adhesively bonded to the other surface of said first perforated facing of thin sheet material; said third facing of perforated thin sheet material is adhesively bonded between one end wise cell surface of said second honeycomb core and to the other surface of said first thin sheet of porous fibrous material; said second perforated facing of thin sheet material is adhesively bonded to the opposite surface of said second honeycomb core; said second thin sheet of porous fibrous material is adhesively bonded to the opposite surface of said second perforated facing of this sheet material whereby a smooth outer surface is presented to a high velocity fluid flow.
Claim 2
Dependent Claim
246 words
A double layer acoustical honeycomb sandwich panel having structural strength for use in the severe environment in and around high velocity fluid flow paths associated with aircraft gas turbine engines comprising: first and second honeycomb cores having a multiplicity of endwise directed cells with walls of thin sheet material disposed transversely to the panel; an impervious facing of thin sheet material; first, second and third facings of perforated thin sheet material; and first and second thin sheets of porous fibrous material; said impervious facing of this sheet material is adhesively bonded to one end wise cell face of said first honeycomb core; said first perforated facing of thin sheet material is adhesively bonded to said first honeycomb core on the surface opposite said impervious facing of this sheet material; said first thin sheet of porous fibrous material is adhesively bonded to the other surface of said first perforated facing of thin sheet material; said third facing of perforated thin sheet material is adhesively bonded between one end wise cell surface of said second honeycomb core and to the other surface of said first thin sheet of porous fibrous material; said second perforated facing of thin sheet material is adhesively bonded to the opposite surface of said second honeycomb core; said second thin sheet of porous fibrous material is adhesively bonded to the opposite surface of said second perforated facing of this sheet material whereby a smooth outer surface is presented to a high velocity fluid flow.
Claim 3
Dependent Claim
31 words
The invention as defined in claim 1, wherein said honeycomb cores and perforated facing of thin sheet material are aluminum and said thin sheets of porous fibrous material are stainless steel.
Claim 4
Dependent Claim
34 words
The invention as defined in claim 1, wherein the adhesive material for bonding together said perforated facings of thin sheet material and porous fibrous material is of sufficient thickness to form an insulation therebetween.
Claim 5
Dependent Claim
43 words
The invention as defined in claim 1, wherein nonmetallic material is positioned between said first and second perforated facings of thin sheet material and porous fibrous material in selected areas where sizing and drill through holes are required for enhancing the insulation therebetween.
Claim 6
Dependent Claim
16 words
The invention as defined in claim 1, wherein said honeycomb cores are constructed of dissimilar materials.
Claim 7
Dependent Claim
19 words
The invention as defined in claim 1, wherein the cells of said first and honeycomb cores have different volumes.
Claim 8
Dependent Claim
35 words
The invention as defined in claim 1, wherein said sandwich panel has a predetermined flow through resistance between the outer free surface of said second thin sheet material and said first and second honeycomb cores.
Claim 9
Dependent Claim
44 words
The invention as defined in claim 1, wherein said first and second perforated facings of thin sheet material have perforations of substantially equal cross section, said third perforated facing sheet has perforations of greater cross section than said first and second perforated facing sheet.
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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) | 1984-10-12 | 1985-04-13 | 1985-10-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-10-12 | 1989-04-13 | 1989-10-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-10-12 | 1993-04-13 | 1993-10-13 | $7700.00 | Window Closed / Lapsed |