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One-part UV and abrasion resistant pigmented surfacing film composition for prepregs

A technology of veneer and composition, applied in the field of paint and traditional veneer substitute, alicyclic epoxy resin system, can solve the problem of no overhang function in the contour area, increase the weight of aerospace vehicles, etc., and achieve the elimination of harmful waste , reduce weight, reduce labor and cost effects

Active Publication Date: 2012-09-05
CYTEC TECH CORP
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

These PTFE-based membranes offer UV stability and ease of use with adhesive backings, but have no overhang in contoured areas
[0011] Also, the paint adds extra weight to the space vehicle

Method used

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  • One-part UV and abrasion resistant pigmented surfacing film composition for prepregs
  • One-part UV and abrasion resistant pigmented surfacing film composition for prepregs
  • One-part UV and abrasion resistant pigmented surfacing film composition for prepregs

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0062] Take 100 parts of Epalloy5000 cycloaliphatic epoxy resin, add 30 parts of bisphenol A and 10 parts of NIPOL1472 resin, and prepare a solution with a concentration of 20% (the solvent is methyl ethyl ketone (MEK)). The mixture was heated to 130°F while stirring, then 0.1 part of triphenylphosphine catalyst was added and the mixture was heated to 300°F. The temperature was maintained at 300°F for 1 hour, then the mixture was cooled to below 200°F, and MEK was added to reduce the solids content to 80%. The cycloaliphatic resin prereactant is used as a base for the surfacing film composition.

Embodiment 2

[0064] By weight, get 100 parts of cycloaliphatic resin pre-reactants in embodiment 1, add 20 parts of novolac epoxy resin DEN439 (Dow Chemical provides), hollow microspheres G-200 ceramic microspheres (3M provides, Minneapolis Lithium) 90 parts, amorphous silicon 8 parts, in order to control the viscosity of the above mixture, add the necessary solvent (MEK) to a solid content of about 80%. After mixing the above ingredients, add a curing agent (such as 8 parts of dicyandiamide and 2 parts of Omicure52 (provided by CVC Chemical)).

[0065] The above mixture was degassed to 80% solids by weight and then coated into a film with a film weight of 0.035 psf. The film was then dried to less than 1% by weight volatiles and the polyester random mat carrier was pressed into the film under low pressure so that the mat just adhered to the film.

Embodiment 3

[0067] Follow the same steps as in Example 2, except that 140 parts of alumina is used as filler instead of hollow microspheres.

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PUM

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Abstract

The present invention is a one-part ultraviolet light and abrasion resistant pigmented surfacing film composition adapted for co-curing with an amine cured composite prepreg material using a chain extended base cycloaliphatic epoxy resin. The chain extended cycloaliphatic epoxy resin is formed through the pre-reaction of a base cycloaliphatic epoxy resin with a chain extension agent such as bisphenol and a high molecular weight elastomer in the presence of triphenyl phosphine to chain link the base cycloaliphatic epoxy resin to form a film formable cycloaliphatic resin prereact capable of lowtemperature curing when added to a latent amine based epoxy curing agent; an amine catalyst; at least one filler; at least one pigment; and a flow control agent to form surfacing film composition. The surfacing film composition adapted for co-curing with an amine curable composite from about 180 DEG F to about 350 DEG F.

Description

technical field [0001] The invention relates to a face mask composition, the composite structure of which has UV resistance and abrasion resistance. In a preferred embodiment, the present invention is directed to a paint and conventional surfacing film replacement comprising a compound capable of co-curing with most amine-curable epoxy resins and bismaleimide-based composite prepreg systems. Cycloaliphatic epoxy resin system. The surfacing film compositions of the present invention utilize pre-reacted basic cycloaliphatic epoxy resins in combination with amine curing agents and catalysts, hardening fillers, pigments, and fluid control agents. Background technique [0002] Fiber-reinforced, polymer-matrix-laminated composite structures are widely used in many applications. For example, more and more composite structures are being used in high-performance aerospace applications. [0003] Most composite parts in the aerospace industry use epoxy-based prepregs because of thei...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): C08G59/18C08J5/24
CPCC08J2363/02C08G59/182C08J5/24C08J5/246C08J5/249C08J5/247C08J5/242C08L63/00C08J5/18
Inventor 达利普·库马尔·科利
Owner CYTEC TECH CORP