US4121002A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Fabrication of antenna windows
Assignee: United States Department of the Air Force
•
Filing: 1977-07-06
•
Granted: 1978-10-17
•
Expires: 1997-07-06
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 |