US4182495A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Graphite or carbon fiber composite structure, low temperature cure
Assignee: United States Department of the Navy
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Filing: 1978-12-04
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Granted: 1980-01-08
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Expires: 1998-12-04
Abstract
Abstract Accordingly the present invention provides a method of construction using araphite or carbon fiber composite structure with a low temperature cure epoxy resin system to have a material system of minimum weight, high strength and high stiffness which eliminates a secondary bonding operation to effect load transfer between structural components and to have service life compatible to its use environment. A graphite or carbon fiber, preimpregnated with a low temperature (195° F.) curing epoxy resin prepared in the form of unidirectional tape, is laid up or wrapped over a contour form and then cured to provide stiffness and strength equal to or exceeding those of a selected metal such as aluminum or steel.
Inventors
- 👤 Donald E. Borgmeier
- 👤 Edward W. Higgs
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 06:43
CPC Classifications
F; F02; F02K; F02K9/00; F02K9/97; Y; Y10; Y10S; Y10S239/00; Y10S239/19; Y10S428/00; Y10S428/902; Y10T; Y10T156/00; Y10T156/10; Y10T156/1089; Y10T156/1092; Y10T428/00; Y10T428/24; Y10T428/24132; Y10T428/30; Y10T428/31504; Y10T428/31511
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
68 words
A rocket nozzle exit cone subassembly comprising: (a) an adaptor of annular configuration; (b) an exit cone bonded to the inner surface of said adaptor; and (c) a net of preimpregnated carbon fiber tape, said tape having a low temperature cure epoxy resin system, wrapped about said exit cone and said adaptor so that when cured said net is firmly bonded to said exit cone and said adaptor.
Claim 2
Dependent Claim
68 words
A rocket nozzle exit cone subassembly comprising: (a) an adaptor of annular configuration; (b) an exit cone bonded to the inner surface of said adaptor; and (c) a net of preimpregnated carbon fiber tape, said tape having a low temperature cure epoxy resin system, wrapped about said exit cone and said adaptor so that when cured said net is firmly bonded to said exit cone and said adaptor.
Claim 3
Dependent Claim
62 words
A rocket nozzle exit cone subassembly as recited in claim 1 wherein said preimpregnated carbon fiber tape comprises unidirectional, continuous filaments of a material selected from the group consisting of high modulus graphite and high strength carbon reinforcing said low temperature cure epoxy resin system, the resin content of said preimpregnated carbon fiber tape being from 34 to 45 percent by weight.
Claim 4
Dependent Claim
67 words
A construction method comprising the steps of: (a) applying a low temperature cure epoxy resin to the surface of a material combination; (b) laying up a plurality of strips of a preimpregnated carbon fiber tape, said tape having a low temperature cure epoxy resin system, to form a predetermined net about said material combination; and (c) curing said material combination with said net at a low temperature.
Claim 5
Dependent Claim
67 words
A construction method comprising the steps of: (a) applying a low temperature cure epoxy resin to the surface of a material combination; (b) laying up a plurality of strips of a preimpregnated carbon fiber tape, said tape having a low temperature cure epoxy resin system, to form a predetermined net about said material combination; and (c) curing said material combination with said net at a low temperature.
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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) | 1983-01-07 | 1983-07-09 | 1984-01-08 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-01-07 | 1987-07-09 | 1988-01-08 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-01-07 | 1991-07-09 | 1992-01-08 | $7700.00 | Window Closed / Lapsed |