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US4121002A Expired / Lapsed US ⏱️ 0.0 years remaining

Fabrication of antenna windows

Assignee: United States Department of the Air Force
•
Filing: 1977-07-06
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Granted: 1978-10-17
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Expires: 1997-07-06
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Abstract

Abstract An integral antenna window is fabricated in a fiber-reinforced, resin matrix composite by the controlled localized removal of resin to provide a window area after which the area containing reinforcing fibers is impregnated with a second resin.

Inventors

  • 👤 R. Bruce Baldwin

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 20:15
CPC Classifications
H; H01; H01Q; H01Q1/00; H01Q1/42; Y; Y10; Y10T; Y10T428/00; Y10T428/13; Y10T428/131; Y10T428/1314; Y10T428/1352; Y10T428/1372; Y10T428/24; Y10T428/24273

Claims Analysis

Total Claims: 8
Claim 1
Independent Claim 86 words
In a fiber-reinforced, resin matrix composite an antenna window comprising an opening in the composite having edges defining a predetermined shape, the opening being free of the resin matrix and containing the reinforcing fibers originally present in the composite prior to removal of resin to form the opening; and an electromagnetic-transparent resin filling the opening and being bonded to its edges and to the reinforcing fibers therein so that the resin is an integral part of the composite, lacking in joints and containing continuous reinforcing fibers.
Claim 2
Dependent Claim 86 words
In a fiber-reinforced, resin matrix composite an antenna window comprising an opening in the composite having edges defining a predetermined shape, the opening being free of the resin matrix and containing the reinforcing fibers originally present in the composite prior to removal of resin to form the opening; and an electromagnetic-transparent resin filling the opening and being bonded to its edges and to the reinforcing fibers therein so that the resin is an integral part of the composite, lacking in joints and containing continuous reinforcing fibers.
Claim 3
Dependent Claim 24 words
The antenna window according to claim 1 in which the resin matrix is a phenolic resin matrix and the electromagnetic-transparent resin is a polyformaldehyde.
Claim 4
Independent Claim 77 words
A method for fabricating an antenna window in a fiber-reinforced, resin matrix composite which comprises heating a defined area of the composite corresponding to a predetermined window area so as to remove resin therefrom while leaving intact the reinforcing fibers of the composite; and impregnating the area free from the resin matrix with an electromagnetic-transparent resin, thereby forming an antenna window which is an integral part of the composite, lacking in joints and containing continuous reinforcing fibers.
Claim 5
Independent Claim 77 words
A method for fabricating an antenna window in a fiber-reinforced, resin matrix composite which comprises heating a defined area of the composite corresponding to a predetermined window area so as to remove resin therefrom while leaving intact the reinforcing fibers of the composite; and impregnating the area free from the resin matrix with an electromagnetic-transparent resin, thereby forming an antenna window which is an integral part of the composite, lacking in joints and containing continuous reinforcing fibers.
Claim 6
Dependent Claim 23 words
The method according to claim 3 in which the resin matrix is a phenolic resin matrix and the electromagnetic-transparent resin is a polyformaldehyde.
Claim 7
Independent Claim 259 words
A method for fabricating an antenna window in a fiber-reinforced, phenolic resin matrix composite having opposed first and second surfaces which comprises the following steps: (a) heating a selected area of predetermined geometry of the first surface of the composite at a temperature sufficient to char the phenolic resin within the area; (b) applying a vacuum to the selected area; (c) continuing to heat the selected area and to apply a vacuum to the selected area until at least one-half of the phenolic resin in the area between the first and second surfaces is degraded and removed as pyrolysis gases; (d) terminating the heating and the application of vacuum; (e) heating an area of the second surface identical in shape to and directly opposite to the selected area of the first surface; (f) applying a vacuum to the area of the second surface; (g) continuing to heat the area of the second surface and to apply a vacuum thereto until all remaining phenolic resin in the area between the first and second surfaces is degraded as indicated by absence of pyrolysis gases; (h) terminating the heating and the application of vacuum; (i) recovering the composite having an opening therein with a shape corresponding to the selected area and containing the reinforcing fibers originally present in the composite prior to removal of resin to form the opening; and (j) impregnating the opening with a polyformaldehyde so as to form an antenna window which is an integral part of the composite and is lacking in joints and contains continuous reinforcing fibers.
Claim 8
Independent Claim 259 words
A method for fabricating an antenna window in a fiber-reinforced, phenolic resin matrix composite having opposed first and second surfaces which comprises the following steps: (a) heating a selected area of predetermined geometry of the first surface of the composite at a temperature sufficient to char the phenolic resin within the area; (b) applying a vacuum to the selected area; (c) continuing to heat the selected area and to apply a vacuum to the selected area until at least one-half of the phenolic resin in the area between the first and second surfaces is degraded and removed as pyrolysis gases; (d) terminating the heating and the application of vacuum; (e) heating an area of the second surface identical in shape to and directly opposite to the selected area of the first surface; (f) applying a vacuum to the area of the second surface; (g) continuing to heat the area of the second surface and to apply a vacuum thereto until all remaining phenolic resin in the area between the first and second surfaces is degraded as indicated by absence of pyrolysis gases; (h) terminating the heating and the application of vacuum; (i) recovering the composite having an opening therein with a shape corresponding to the selected area and containing the reinforcing fibers originally present in the composite prior to removal of resin to form the opening; and (j) impregnating the opening with a polyformaldehyde so as to form an antenna window which is an integral part of the composite and is lacking in joints and contains continuous reinforcing fibers.

References Cited (Backward Citations)

US2474201A Cited
US3190338A Cited
US3509571A Cited
US3618112A Cited
US3668028A Cited
US3766562A Cited
US3874958A Cited
US4006480A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-10-16 1982-04-17 1982-10-17 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-10-16 1986-04-17 1986-10-17 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-10-16 1990-04-17 1990-10-17 $7700.00 Window Closed / Lapsed

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