Patent US4963301A successfully refreshed from Google Patents.
US4963301A
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Method for fabrication of refractory composite tubing
Assignee: Kaiser Aerotech Inc
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Filing: 1988-06-28
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Granted: 1990-10-16
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Expires: 2008-06-28
Abstract
Abstract Reinforced composite tubes are formed by rolling a flat reinforcement fabric onto a cylindrical or conical mandrel under tension. By pre-impregnating the fabric with a suitable matrix precursor or by serving the individual threads of the fabric with a thermoplastic, the fabric may be compressed by applying heat and pressure during the rolling process. After rolling, the resulting prepreg is cured in a suitable vacuum bag, also under heat and pressure. The cured prepreg may then be converted by pyrolysis and densified by repeated impregnation and converting steps. The resulting composite tubes are substantially free from mechanical defects which would reduce their strength.
Inventors
- 👤 H. O. Davis
- 👤 James M. Barrier
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-07 17:55
CPC Classifications
C; C04; C04B; C04B35/00; C04B35/71; C04B35/78; C04B35/80; C04B35/01; C04B35/10; C04B35/111; C04B35/117; C04B35/515; C04B35/56; C04B35/565; C04B35/571; C04B35/82; C04B35/83; C04B2235/00; C04B2235/02; C04B2235/30; C04B2235/48; C04B2235/50; C04B2235/52; C04B2235/5208; C04B2235/5216; C04B2235/524; C04B2235/5248; C04B2235/5264; C04B2235/60; C04B2235/602; C04B2235/6028; C04B2235/616; C04B2235/70; C04B2235/94; C04B2235/96; C04B2235/9607
Claims Analysis
Total Claims: 16
Claim 1
Independent Claim
159 words
A method for forming reinforced refractory composite tubes, said method comprising: (a) rolling a continuous reinforcement fabric onto a mandrel under tension while simultaneously applying heat and pressure, said fabric being pre-impregnated with a refractory matrix precursor or served with a thermoplastic so that successive plies of the fabric are compressed without the introduction of mechanical defects; (b) curing the refractory matrix precursor or thermoplastic serving on the rolled reinforcement fabric under a vacuum at an elevated temperature; (c) converting the cured refractory matrix precursor or thermoplastic on the rolled reinforcement fabric to the corresponding refractory matrix by pyrolysis while the rolled reinforcement fabric is present on a mandrel having a coefficient of thermal expansion from 1.1 to 10 times greater than that of the refractory matrix; (d) impregnating the rolled reinforcement fabric with additional matrix precursor; (e) converting the additional matrix precursor to matrix; and (f) repeating steps (d) and (e) until a desired matrix density is achieved.
Claim 2
Independent Claim
159 words
A method for forming reinforced refractory composite tubes, said method comprising: (a) rolling a continuous reinforcement fabric onto a mandrel under tension while simultaneously applying heat and pressure, said fabric being pre-impregnated with a refractory matrix precursor or served with a thermoplastic so that successive plies of the fabric are compressed without the introduction of mechanical defects; (b) curing the refractory matrix precursor or thermoplastic serving on the rolled reinforcement fabric under a vacuum at an elevated temperature; (c) converting the cured refractory matrix precursor or thermoplastic on the rolled reinforcement fabric to the corresponding refractory matrix by pyrolysis while the rolled reinforcement fabric is present on a mandrel having a coefficient of thermal expansion from 1.1 to 10 times greater than that of the refractory matrix; (d) impregnating the rolled reinforcement fabric with additional matrix precursor; (e) converting the additional matrix precursor to matrix; and (f) repeating steps (d) and (e) until a desired matrix density is achieved.
Claim 3
Dependent Claim
53 words
A method as in claim 1, wherein step (b) is performed while the rolled reinforcement fabric is present on a first mandrel and step (c) is performed while the rolled reinforcement fabric is present on a second mandrel, wherein the first mandrel has a higher coefficient of thermal expansion than the second mandrel.
Claim 4
Dependent Claim
35 words
A method as in claim 1, further comprising tapering one end of the rolled reinforcement fabric prior to step (d), whereby the tapered end can serve as an attachment point on the reinforced composite tube.
Claim 5
Dependent Claim
21 words
A method as in claim 3, wherein the one end is tapered by forming over a tapered end of the mandrel.
Claim 6
Independent Claim
16 words
A method as in claim- 3, further comprising trimming the tapered end to a desired profile.
Claim 7
Dependent Claim
26 words
A method as in claim 1, wherein the reinforcement fabric is composed of a material selected from the group consisting of graphite, ceramic, glass, and aramid.
Claim 8
Dependent Claim
31 words
A method as in claim 1, wherein fabric is impregnated with an organic matrix precursor material selected from the group consisting of liquid organic precursors, polycarbosilanes, and liquid aluminum oxide precursors.
Claim 9
Dependent Claim
23 words
A method as in claim 1, wherein the rolling is performed using opposed rollers and bars which are under a preselected compressive force.
Claim 10
Dependent Claim
35 words
A method as in claim 8 wherein the mandrel is cylindrical and supported on a pair of bars rollers with at least one opposed roller overhead, wherein at least one of the bars is heated.
Claim 11
Dependent Claim
25 words
A method as in claim 1, wherein the rolling step increases the density of the reinforcement fabric by a factor of at least about 1.4.
Claim 12
Dependent Claim
17 words
A method as in claim 1, wherein the rolled fabric has from about 2 to 50 plies.
Claim 13
Independent Claim
41 words
A method as in claim- 1. wherein the matrix precursor is cured by placing the rolled fabric on the mandrel into a fitted vacuum bag, applying an elevated pressure to the exterior of the vacuum bag, and externally heating the bars.
Claim 14
Dependent Claim
42 words
A method as in claim 1, wherein the matrix precursor is cured by placing the rolled fabric into a fitted vacuum bag, applying an elevated pressure to the exterior of the vacuum bag, and internally heating the mandrel supporting the rolled fabric.
Claim 15
Dependent Claim
26 words
A method as in claim 1, wherein individual fibers of the reinforcement fabric are served with thermoplastic filaments and cured as set forth in step (b).
Claim 16
Dependent Claim
24 words
A method as in claim 1, wherein step (b) and step (c) are performed with the rolled reinforcement fabric present on the same mandrel.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1993-10-15 | 1994-04-16 | 1994-10-16 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1997-10-15 | 1998-04-16 | 1998-10-16 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2001-10-15 | 2002-04-16 | 2002-10-16 | $7700.00 | Window Closed / Lapsed |