US4664731A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Pultrusion of glass and glass-ceramic matrix composites
Assignee: NAVY United States, THE, Secretary of, Department of
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Filing: 1985-01-07
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Granted: 1987-05-12
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Expires: 2005-01-07
Abstract
Abstract A method of making fiber reinforced glass composite articles utilizes preregnated preforms which are bound with a temporary plastic binder. The binder is removed in a gradient oven and the frit or preform is drawn through a pultrusion die assembly heated to the degree necessary to render the frit workable. Deformation in the heated die assembly is maintained during cooling, resulting in a formed glass composite article.
Inventors
- 👤 George K. Layden
- 👤 Karl M. Prewo
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-30 16:17
CPC Classifications
C; C03; C03C; C03C14/00; C03C14/002; C03B; C03B17/00; C03B17/04; C03C2214/00; C03C2214/02; C03C2214/20; C03C2214/30
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
125 words
A method for making fiber reinforced glass composite articles comprising: passing glass impregnated fiber preforms containing a temporary thermoplastic resin binder through a bakeout gradient oven for burnout of the binder; and passing the preform through a pultrusion die assembly to effect consolidation by matrix flow and diffusion bonding, thus yielding formed structural members; wherein passing the preform through the pultrusion die assembly comprises drawing said preform through a heated pultrusion die; heating said assembly and preform to between about 1000 degrees C. and about 1300 degrees C.; providing intermediate deformation of said preform at a temperature of about 1300 degrees C.; and providing final deformation and bonding of said preforms as the temperature decreases between about 1300 degrees C. and about 600 degrees C.
Claim 2
Independent Claim
125 words
A method for making fiber reinforced glass composite articles comprising: passing glass impregnated fiber preforms containing a temporary thermoplastic resin binder through a bakeout gradient oven for burnout of the binder; and passing the preform through a pultrusion die assembly to effect consolidation by matrix flow and diffusion bonding, thus yielding formed structural members; wherein passing the preform through the pultrusion die assembly comprises drawing said preform through a heated pultrusion die; heating said assembly and preform to between about 1000 degrees C. and about 1300 degrees C.; providing intermediate deformation of said preform at a temperature of about 1300 degrees C.; and providing final deformation and bonding of said preforms as the temperature decreases between about 1300 degrees C. and about 600 degrees C.
Claim 3
Independent Claim
105 words
A method of making fiber reinforced glass composite articles comprising the steps of: passing continuous strip glass impregnated fiber preforms containing a temporary thermoplastic resin binder through a bakeout gradient oven for burnout of the binder; and passing the preform through a pultrusion die assembly to effect consolidation by matrix flow and diffusion bonding, thus yielding formed structural members; wherein said preforms are woven about a sting longitudinally disposed through said gradient oven and pultrusion die assembly, said sting cooperating with said die assembly to deform said preform; and wherein said preform is removed from said sting such that said formed structural members are hollow.
Claim 4
Independent Claim
105 words
A method of making fiber reinforced glass composite articles comprising the steps of: passing continuous strip glass impregnated fiber preforms containing a temporary thermoplastic resin binder through a bakeout gradient oven for burnout of the binder; and passing the preform through a pultrusion die assembly to effect consolidation by matrix flow and diffusion bonding, thus yielding formed structural members; wherein said preforms are woven about a sting longitudinally disposed through said gradient oven and pultrusion die assembly, said sting cooperating with said die assembly to deform said preform; and wherein said preform is removed from said sting such that said formed structural members are hollow.
Claim 5
Independent Claim
152 words
A method of making fiber reinforced glass composite articles comprising: passing glass impregnated fiber preforms containing a temporary thermoplastic resin binder through a bakeout gradient oven for burnout of the binder; and passing the preform through a pultrusion die assembly to effect consolidation by matrix flow and diffusion bonding, thus yielding formed structural members; wherein the said step of passing the preform through a pultrusion die assembly comprises the further steps of mechanically drawing said preform through an oven wherein the preform is heated to a temperature below the working point of the glass but yet high enough to be effective for burnout of the said thermoplastic resin binder; thereafter drawing said preform into the said pultrusion die; continuously heating the preform beyond the working point thereof without deformation; causing an initial deformation by heating the preform to a temperature beyond the working point; and cooling the preform below the working point.
Claim 6
Independent Claim
152 words
A method of making fiber reinforced glass composite articles comprising: passing glass impregnated fiber preforms containing a temporary thermoplastic resin binder through a bakeout gradient oven for burnout of the binder; and passing the preform through a pultrusion die assembly to effect consolidation by matrix flow and diffusion bonding, thus yielding formed structural members; wherein the said step of passing the preform through a pultrusion die assembly comprises the further steps of mechanically drawing said preform through an oven wherein the preform is heated to a temperature below the working point of the glass but yet high enough to be effective for burnout of the said thermoplastic resin binder; thereafter drawing said preform into the said pultrusion die; continuously heating the preform beyond the working point thereof without deformation; causing an initial deformation by heating the preform to a temperature beyond the working point; and cooling the preform below the working point.
References Cited (Backward Citations)
US3607608A
Cited
US3575789A
Cited
US3695960A
Cited
US4207371A
Cited
US4151031A
Cited
US4344556A
Cited
US4268562A
Cited
US4357286A
Cited
US4412854A
Cited
US4464192A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1990-05-11 | 1990-11-10 | 1991-05-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1994-05-11 | 1994-11-10 | 1995-05-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1998-05-11 | 1998-11-10 | 1999-05-12 | $7700.00 | Window Closed / Lapsed |