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US5217669A Expired / Lapsed US ⏱️ 0.0 years remaining

Method for forming complex composite articles

Assignee: RTX Corp
•
Filing: 1991-09-11
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Granted: 1993-06-08
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Expires: 2011-09-11
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Abstract

Abstract A method of making a flexible composite tool particularly adapted for composite molding and the composite tool made by this method. The method includes dissolving a B-staged fluoroelastomer in a suitable solvent such as methyl ethyl ketone or toluene to form a fluoroelastomer solution. A fabric is then coated with the fluoroelastomer solution. The solvent is evaporated and the impregnated fabric is sandwiched between unreinforced sheets to form a reinforced tooling material. The reinforced tooling material is laid up with alternating layers of unreinforced fluoroelastomer and then cured to form a composite tool which is stable through multiple thermal cycles. In addition, an elastomer tool can be provided with detail cavities shaped to accept separately formed detail structures, with each cavity including extra reinforcement in order to locate the details to close tolerances without extensive hand positioning or use of adhesives. The tool is useful in molding composites and is reusable. The life of the tool is further prolonged by a described method of repairing damaged portions of the tool.

Inventors

  • 👤 Alex C. Dublinski
  • 👤 David A. Evans
  • 👤 Joseph Goldberg
  • 👤 Geoffrey C. R. Davis
  • 👤 Jr. William Sharp
  • 👤 Michael A. Kornitzky

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 14:54
CPC Classifications
C; C08; C08J; C08J5/00; C08J5/04; C08J5/06; B; B29; B29C; B29C33/00; B29C33/30; B29C33/307; B29C33/38; B29C33/3842; B29C33/3857; B29C43/00; B29C43/32; B29C43/36; B29C43/3642; B29C70/00; B29C70/04; B29C70/06; B29C70/08; B29C70/086; B29C70/28; B29C70/40; B29C70/42; B29C70/44; B29C70/54; B29C2033/385; B29C2043/3644; B29C2791/00; B29C2791/001; B29C33/40; B29K; B29K2105/00; B29K2105/24; B29K2105/243; B29K2277/00; B29K2827/00; B29K2827/12; B29K2827/18; C08J2327/00; C08J2327/02; C08J2327/12

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 201 words
A method for molding a complex composite article and accurately locating a separately formed detailed structure on the article for co-curing therewith, the method comprising: providing a semi-rigid tool half having an elastomer layer having sufficient flexibility and stretch to provide uniform compaction of a plurality of laminate plys, the tool half formed to a shape essentially matching the shape of the article, the elastomer layer having one or more cavities shaped to accept a detail structure therein, and means for preventing movement or shifting of a detail structure located in the cavity during processing, said means including at least one additional layer of a reinforced elastomer disposed over the portion of the elastomer layer forming the cavity, the additional reinforcement provided by the reinforced elastomer layer increasing the rigidity of the elastomer layer about the detail cavity, without eliminating the elasticity of the elastomer layer, providing a rigid tool half shaped to mate with the semi-rigid tool half; placing the plurality of laminate plys on the rigid tool half; inserting detail structures into the one or more cavities in the elastomer layer; mating the two tool halves; and, processing to form a composite article having accurately located integral detail structures.
Claim 2
Independent Claim 201 words
A method for molding a complex composite article and accurately locating a separately formed detailed structure on the article for co-curing therewith, the method comprising: providing a semi-rigid tool half having an elastomer layer having sufficient flexibility and stretch to provide uniform compaction of a plurality of laminate plys, the tool half formed to a shape essentially matching the shape of the article, the elastomer layer having one or more cavities shaped to accept a detail structure therein, and means for preventing movement or shifting of a detail structure located in the cavity during processing, said means including at least one additional layer of a reinforced elastomer disposed over the portion of the elastomer layer forming the cavity, the additional reinforcement provided by the reinforced elastomer layer increasing the rigidity of the elastomer layer about the detail cavity, without eliminating the elasticity of the elastomer layer, providing a rigid tool half shaped to mate with the semi-rigid tool half; placing the plurality of laminate plys on the rigid tool half; inserting detail structures into the one or more cavities in the elastomer layer; mating the two tool halves; and, processing to form a composite article having accurately located integral detail structures.
Claim 3
Dependent Claim 15 words
The method of claim 1 wherein the elastomer layer comprises a fluoroelastomer impregnated polyaramid fabric.
Claim 4
Dependent Claim 25 words
The method of claim 1 wherein the elastomer layer is a series of plies, comprising an impregnated polyaramid fabric ply sandwiched between un-reinforced fluoroelastomer plies.

References Cited (Backward Citations)

US3295818A Cited
US4025686A Cited
US4882118A Cited
US4721593A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1996-06-07 1996-12-07 1997-06-08 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 2000-06-07 2000-12-07 2001-06-08 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2004-06-07 2004-12-07 2005-06-08 $7700.00 Window Closed / Lapsed

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