US4065340A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Composite lamination method
Assignee: National Aeronautics and Space Administration
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Filing: 1977-04-28
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Granted: 1977-12-27
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Expires: 1997-04-28
Abstract
Abstract A process for preparing relatively thick composite laminate structures wherein thin layers of prepreg tapes are assembled, these thin layers are cut into strips that are partially cured, stacked into the desired thickness with uncured prepreg disposed between each layer of strips and the thus formed laminate finally cured and thereafter machined to the desired final dimensions.
Inventors
- 👤 George E. Dickerson
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-23 20:44
CPC Classifications
B; B29; B29C; B29C70/00; B29C70/04; B29C70/28; B29C70/54; B29C70/549; B32; B32B; B32B5/00; B32B5/22; B32B5/24; B32B5/26; B29C35/00; B29C35/02; B29C70/30; B29C70/34; B29C70/342; B29C70/40; B29C70/42; B29C70/44; B29C70/545; B32B37/00; B32B37/10; B32B37/1018; B32B38/00; B32B38/0004; B29C43/00; B29C43/32; B29C43/36; B29C43/3642; B29C2043/3644; B29C2791/00; B29C2791/001; B29C2793/00; B29C2793/009; B29C43/02; B29C43/10; B29C43/12; B29K; B29K2063/00; B29K2105/00; B29K2105/24; B29K2105/243; B29K2307/00; B32B2038/0052; B32B2038/0076; B32B2260/00; B32B2260/02; B32B2260/021; B32B2260/04; B32B2260/046; B32B2305/00; B32B2305/07; B32B2305/076; B32B2309/00; B32B2309/02; B32B2309/12; Y; Y10; Y10T; Y10T156/00; Y10T156/10; Y10T156/1052; Y10T156/1062; Y10T156/1075; Y10T156/1089; Y10T156/1092; Y10T156/1093; Y10T428/00; Y10T428/249921; Y10T428/249924; Y10T428/24994; Y10T428/249941
Claims Analysis
Total Claims: 15
Claim 1
Independent Claim
193 words
A process of preparing structural components of composite laminates comprising: providing prepreg resin impregnated fiber tape material having the fibers therein running the length of the tape, cutting the prepreg tape into a plurality of desired lengths, stacking the plurality of lengths of tape in layers to a predetermined thickness while maintaining the same fiber orientation for each layer, partially curing the stacked tape assembly into a unitary mass under vacuum for approximately ten minutes and at an elevated temperature of at least 350° F., cooling the partial cured mass and cutting it into a plurality of strips along the parallel orientation of the fibers, stacking this plurality of strips vertically in layers atop each other with two strips of uncured prepreg tape disposed between each of the plurality of laminate strips, curing the stacked layer strips into a unitary structure under vacuum, pressure and an elevated temperature of at least 350° F. for least thirty minutes, cooling the cured structure to a minimum of 150° F. while maintaining the pressure and vacuum, and after allowing to cool to room temperature, machining the unitary structure formed into the final desired size and shape.
Claim 2
Dependent Claim
193 words
A process of preparing structural components of composite laminates comprising: providing prepreg resin impregnated fiber tape material having the fibers therein running the length of the tape, cutting the prepreg tape into a plurality of desired lengths, stacking the plurality of lengths of tape in layers to a predetermined thickness while maintaining the same fiber orientation for each layer, partially curing the stacked tape assembly into a unitary mass under vacuum for approximately ten minutes and at an elevated temperature of at least 350° F., cooling the partial cured mass and cutting it into a plurality of strips along the parallel orientation of the fibers, stacking this plurality of strips vertically in layers atop each other with two strips of uncured prepreg tape disposed between each of the plurality of laminate strips, curing the stacked layer strips into a unitary structure under vacuum, pressure and an elevated temperature of at least 350° F. for least thirty minutes, cooling the cured structure to a minimum of 150° F. while maintaining the pressure and vacuum, and after allowing to cool to room temperature, machining the unitary structure formed into the final desired size and shape.
Claim 3
Dependent Claim
49 words
The method of claim 1 wherein the step of partially curing the stacked tape assembly into a unitary mass includes, placing the stacked assembly between separator cloths and fiberglass bleeder cloths, bagging the resulting stack assembly in a vacuum bag, and placing the bagged assembly in a pressure vessel.
Claim 4
Dependent Claim
37 words
The method of claim 2 wherein the bagged stack assembly in the pressure vessel is heated from room temperature to 350° F. in increments of 2°-3° F. per minute after the assembly is placed under full vacuum.
Claim 5
Dependent Claim
27 words
The method of claim 3 wherein a pressure of 85 psi external pressure is applied and maintained to the assembly when the temperature thereof reaches 225° F.
Claim 6
Dependent Claim
28 words
The method of claim 4 wherein the vacuum and external pressure are maintained until the temperature reaches and is maintained at about 350° F. for approximately ten minutes.
Claim 7
Dependent Claim
34 words
The method of claim 5 wherein the vacuum and external pressure are maintained while permitting the assembly to cool to at least 150° F. prior to removal of the assembly from the pressure vessel.
Claim 8
Dependent Claim
34 words
The method of claim 1 wherein the plurality of partially cured strips are stacked so as to maintain the fiber orientation of each layer in the stack parallel to that of the adjacent layer.
Claim 9
Dependent Claim
36 words
The method of claim 1 wherein the plurality of partially cured strips are stacked in layers so as to maintain the fiber orientation of each layer in the stack perpendicular to that of the adjacent layer.
Claim 10
Dependent Claim
46 words
The method of claim 1 wherein the plurality of partially cured strips are stacked in layers so as to maintain the fiber orientation of each layer in the stack at an angular relationship to that of the adjacent layer in the range of 1° to 179°.
Claim 11
Dependent Claim
36 words
The method of claim 1 wherein the fiber orientation of the strips of uncured prepreg tape between each layer in the stack is disposed parallel with the fiber orientation of the adjacent layer of the stack.
Claim 12
Dependent Claim
31 words
A process of preparing structural components of composite laminates and skin covers therefor comprising: providing prepreg resin impregnated fiber tape material having the fibers therein running the length of the tape,
Claim 13
Dependent Claim
31 words
A process of preparing structural components of composite laminates and skin covers therefor comprising: providing prepreg resin impregnated fiber tape material having the fibers therein running the length of the tape,
Claim 14
Dependent Claim
183 words
cutting the prepreg tape into a plurality of desired lengths, stacking the plurality of lengths of tape in layers to a predetermined thickness while maintaining the same fiber orientation for each layer, partially curing the stacked tape assembly into a unitary mass under vacuum and at an elevated temperature of at least 350°, cooling the partially cured mass and machining it into the desired configuration, preparing a partially cured prepreg skin cover for the machined configuration from layers of prepreg tape by the same process, positioning this partially cured skin onto the machined configuration so as to maintain parallel fiber orientation between the configuration and skin and with two strips of uncured prepreg tape disposed between the configuration and skin and having the fibers therein disposed parallel to the fibers in the configuration and skin, curing the stacked configuration and skin into a unitary structure under vacuum, pressure and an elevated temperature of at least 350° F. for at least thirty minutes, and maintaining the pressure while cooling the cured structure to a minimum of 150° F. while maintaining the pressure and vacuum.
Claim 15
Dependent Claim
183 words
cutting the prepreg tape into a plurality of desired lengths, stacking the plurality of lengths of tape in layers to a predetermined thickness while maintaining the same fiber orientation for each layer, partially curing the stacked tape assembly into a unitary mass under vacuum and at an elevated temperature of at least 350°, cooling the partially cured mass and machining it into the desired configuration, preparing a partially cured prepreg skin cover for the machined configuration from layers of prepreg tape by the same process, positioning this partially cured skin onto the machined configuration so as to maintain parallel fiber orientation between the configuration and skin and with two strips of uncured prepreg tape disposed between the configuration and skin and having the fibers therein disposed parallel to the fibers in the configuration and skin, curing the stacked configuration and skin into a unitary structure under vacuum, pressure and an elevated temperature of at least 350° F. for at least thirty minutes, and maintaining the pressure while cooling the cured structure to a minimum of 150° F. while maintaining the pressure and vacuum.
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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) | 1980-12-26 | 1981-06-27 | 1981-12-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-12-26 | 1985-06-27 | 1985-12-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-12-26 | 1989-06-27 | 1989-12-27 | $7700.00 | Window Closed / Lapsed |