US4990391A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Reticulated core to perforate sheet bonding and galvanic barrier
Assignee: Rohr Inc
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Filing: 1989-02-03
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Granted: 1991-02-05
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Expires: 2009-02-03
Abstract
Abstract The invention is directed a laminate structure using a reticulated adhesive material positioned between the honeycomb core and a perforate sheet and a precured reticulated adhesive between the perforated sheet and an outer layer of wire screen or other porous fibrous materials with similar pore openings therethrough through which the cells of the honeycomb core can communicate the atmosphere adjacent to the opposite side of the outer layer of porous material and a method of manufacturing same. During the manufacturing process of honeycomb noise attenuation structures which includes an imperforate sheet, an open cell honeycomb core, a perforated sheet and a layer of porous material stacked in that order a thin sheet of a reticulative adhesive material is positioned between the honeycomb core and perforated sheet and between the perforated sheet and the outer porous layer. During reticulation the reticulative material by its physical makeup shrinks to the edges of the perforations of the perforated sheet thereby leaving the perforations of both sheets of material open to the cells providing a bonding agent between the honeycomb core and perforated sheet and a similar precured layer providing galvanic isolation between the porous sheet and the perforated sheet.
Inventors
- 👤 Ross E. Veta
- 👤 Ernest C. Millard
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 04:20
CPC Classifications
B; B32; B32B; B32B3/00; B32B3/10; B32B3/12; B32B15/00; B32B15/04; B32B15/08; B32B15/092; B32B27/00; B32B27/38; B32B3/26; B32B3/266; E; E04; E04C; E04C2/00; E04C2/30; E04C2/34; E04C2/36; E04C2/365; G; G10; G10K; G10K11/00; G10K11/16; G10K11/172; B32B2305/00; B32B2305/02; B32B2305/024; B32B2305/026; B32B2311/00; B32B2311/24; B32B2311/30; B32B2363/00; B32B2605/00; B32B2605/18; Y; Y10; Y10T; Y10T428/00; Y10T428/24; Y10T428/24149; Y10T428/24273; Y10T428/24322; Y10T428/24331
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
227 words
A method for producing acoustical honeycomb sandwich laminate panel for use as supporting structure for an aircraft for sound suppression wherein said acoustic honeycomb sandwich laminate panel is exposed to the element and engine sounds comprising the steps of: providing a honeycomb core having a plurality of open cells defined by edgewise directed walls positioned transverse to the surface of said panel; providing a thin sheet of perforated facing material for bonding to one the faying edge surface of said honeycomb core; providing a thin layer of porous material for bonding to the other surface of said thin sheet of perforated material; positioning said thin sheet of perforated material between said honeycomb core and said thin layer of porous material; bonding together said honeycomb, perforated facing material, thin layer of porous material comprising the steps of, positioning a thin sheet of a reticulative adhesive material between said honeycomb core and said perforated sheet, heating said thin sheet of reticulative adhesive to a molten state, passing air through said cells, perforated sheet and pores of said thin layer of porous material thereby causing the reticulative material to be attracted to the solid areas of said perforated sheet clearing the perforations of said reticulative material; providing a thin sheet of imperforate material; and bonding said thin sheet of imperforate material to the other faying edge of said honeycomb material.
Claim 2
Independent Claim
227 words
A method for producing acoustical honeycomb sandwich laminate panel for use as supporting structure for an aircraft for sound suppression wherein said acoustic honeycomb sandwich laminate panel is exposed to the element and engine sounds comprising the steps of: providing a honeycomb core having a plurality of open cells defined by edgewise directed walls positioned transverse to the surface of said panel; providing a thin sheet of perforated facing material for bonding to one the faying edge surface of said honeycomb core; providing a thin layer of porous material for bonding to the other surface of said thin sheet of perforated material; positioning said thin sheet of perforated material between said honeycomb core and said thin layer of porous material; bonding together said honeycomb, perforated facing material, thin layer of porous material comprising the steps of, positioning a thin sheet of a reticulative adhesive material between said honeycomb core and said perforated sheet, heating said thin sheet of reticulative adhesive to a molten state, passing air through said cells, perforated sheet and pores of said thin layer of porous material thereby causing the reticulative material to be attracted to the solid areas of said perforated sheet clearing the perforations of said reticulative material; providing a thin sheet of imperforate material; and bonding said thin sheet of imperforate material to the other faying edge of said honeycomb material.
Claim 3
Dependent Claim
43 words
The method as defined in claim 1 additionally comprising the step of positioning a thin sheet of said reticulative material between said thin sheet of perforated material and said thin layer of porous material prior to the step of heating the reticulative material.
Claim 4
Dependent Claim
25 words
The method as defined in claim 1 wherein said layer of thin reticulative material has a thickness in the range of 0.05 to 0.07 inches.
Claim 5
Dependent Claim
25 words
The method as defined in claim 2 wherein said layer of thin reticulative material has a thickness in the range of 0.05 to 0.07 inches.
Claim 6
Dependent Claim
14 words
The invention as defined in claim 1 wherein said reticulative material is epoxy based.
Claim 7
Dependent Claim
14 words
The invention as defined in claim 2 wherein said reticulative material is epoxy based.
Claim 8
Dependent Claim
27 words
The method as defined in claim 1 including the step of precuring said thin sheet of reticulative material prior to the step of heating said reticulative material.
Claim 9
Dependent Claim
27 words
The method as defined in claim 2 including the step of precuring said thin sheets of reticulative material prior to the step of heating said reticulative material.
Claim 10
Dependent Claim
10 words
A laminated structure resulting from the method of claim 1.
Claim 11
Dependent Claim
10 words
A laminated structure resulting from the method of claim 2.
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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) | 1994-02-04 | 1994-08-06 | 1995-02-05 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-02-04 | 1998-08-06 | 1999-02-05 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-02-04 | 2002-08-06 | 2003-02-05 | $7700.00 | Window Closed / Lapsed |