← Back to Patent Explorer
US4449607A Expired / Lapsed US ⏱️ 0.0 years remaining

Soundproofing for a gas pipe, in particular for the fan jet of a turbojet, and equipment for its fabrication

Assignee: Safran Aircraft Engines SAS
•
Filing: 1982-01-26
•
Granted: 1984-05-22
•
Expires: 2002-01-26
📄 Original PDF 🌐 Google Patents 🔄 Sync Now

Abstract

Abstract Soundproof lining for a gas pipe, in particular for a turbojet fan jet, of the type including a multiplicity of thin, perforated panels juxtaposed by tiling, as well as an intermediate layer between the wall of the pipe and each of said panels to delimit with said perforated panel a multiplicity of resonant acoustical cavities in which the acoustical vents consist of the ports in the perforated panel. According to the invention, in order to make the tubular vents, each perforated panel has a short, tubular sleeve at right angles to each port and located on its face opposite the wall of the pipe.

Inventors

  • 👤 Alexandre Forestier
  • 👤 Alain A. Pluquet
  • 👤 Roger A. Rosa
  • 👤 Mansour Tabet
  • 👤 Pierre M. Teysseyre

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-06 09:38
CPC Classifications
G; G10; G10K; G10K11/00; G10K11/16; G10K11/172; F; F02; F02K; F02K1/00; F02K1/78; F02K1/82; F02K1/827; F05; F05D; F05D2250/00; F05D2250/10; F05D2250/19; F05D2250/191; Y; Y10; Y10T; Y10T428/00; Y10T428/24; Y10T428/24149

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 127 words
A soundproof lining for the wall of a gas jet, said lining comprising: a plurality of thin panels having overlapping ends and extending parallel to said wall; means for fixing said panels directly to said wall and at a distance from said wall whereby said wall and panels define a space therebetween; an intermediate ductile panel in said space, said ductile panel and said thin panels together defining a multiplicity of resonant acoustical cavities, wherein said intermediate panel comprises a thin polymer resin sheet having portions contacting said wall, said sheet including first ribs, the distal ends of said first ribs contacting said thin sheet to define said acoustical cavities; and a plurality of acoustical vents for said cavities, said vents comprising perforations in said thin panels.
Claim 2
Dependent Claim 127 words
A soundproof lining for the wall of a gas jet, said lining comprising: a plurality of thin panels having overlapping ends and extending parallel to said wall; means for fixing said panels directly to said wall and at a distance from said wall whereby said wall and panels define a space therebetween; an intermediate ductile panel in said space, said ductile panel and said thin panels together defining a multiplicity of resonant acoustical cavities, wherein said intermediate panel comprises a thin polymer resin sheet having portions contacting said wall, said sheet including first ribs, the distal ends of said first ribs contacting said thin sheet to define said acoustical cavities; and a plurality of acoustical vents for said cavities, said vents comprising perforations in said thin panels.
Claim 3
Dependent Claim 68 words
The lining of claim 1 wherein each of said thin panels comprises a thin sheet of molded polymer resin reinforced with mineral or organic fibers, said thin panels including a tubular sleeve surrounding each of said vents and extending from the face of said thin panels which faces said wall, said sleeves being formed integrally with said panels, the reinforcing fibers of said panels extending into said sleeves.
Claim 4
Dependent Claim 15 words
The lining of claim 2 wherein said reinforcing fibers comprise stacked layers of fiber felt.
Claim 5
Dependent Claim 38 words
The lining of claims 2 or 3 wherein said means for fixing comprise: braces extending between said thin panels and said wall; and anchoring bolts passing through said braces and fixed to said thin panels and said wall.
Claim 6
Dependent Claim 55 words
The lining of claim 4 including first washers fixed to said thin panels and extending from the face of said thin panels opposite said wall to the face of said thin panels facing said wall, said washers defining countersinks, wherein said anchoring bolts comprise countersunk bolts, the heads of which are positionable in said countersinks
Claim 7
Dependent Claim 41 words
The lining of claim 5 wherein said thin panels and said braces are polymerized, said polymerization of said thin panels and said braces being performed simultaneously and in situ, said lining including second washers positioned between said braces and said wall.
Claim 8
Dependent Claim 15 words
The lining of claim 1 wherein said distal ends of said first ribs include flanges.
Claim 9
Dependent Claim 20 words
The lining of claims 1 or 7 wherein said portions of said intermediate panel contacting said wall comprise second ribs.

References Cited (Backward Citations)

US2830780A Cited
DE1086033B Cited
US3211253A Cited
GB1166843A Cited
FR2201010A5 Cited
US4237176A Cited
US4170674A Cited
FR2396868A1 Cited
GB2019937A Cited
GB2019983A Cited
US4235303A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1987-05-22 1987-11-21 1988-05-22 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1991-05-22 1991-11-21 1992-05-22 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1995-05-22 1995-11-21 1996-05-22 $7700.00 Window Closed / Lapsed

Assigned Categories & Tags

No categories assigned to this patent yet.

Assign Category Tag