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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
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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)

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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) 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

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