# Patent

## Title
Articles and methods for protecting substrates

## Abstract

This application is a division of application Ser. No. 06/790,563, filed Oct. 23, 1985, now U.S. Pat. No. 4,675,350, which is a continuation-in-part of application Ser. No. 670,791, filed Nov. 13, 1984, now abandoned.

## Background
Because they are B-stageable and have very good properties, epoxy resins are widely used in making laminates. Laminates have also been made using polyimide-based laminating resins, which have many high performance characteristics not possessed by epoxy resins. However, polyimide resins require more severe curing conditions than do epoxy resins to achieve the optimum properties.

Another approach to improving laminates has been to modify the epoxy resins with imide functional adjuvants. For example, U.S. Pat. No. 4,244,857 teaches the use of certain bis amino imides as curing agents for polyepoxide resins. Similarly, U.S. Pat. No. 3,978,152 discloses thermosetting compositions which are blends of certain unsaturated bisimides with adducts possessing an amino group formed from an epoxy resin and excess amine. U.S. Pat. No. 3,984,373 describes a thermosetting resin composition based on an epoxy resin incorporated with an N,N'-unsaturated amic acid-imide containing compound. Similarly, U.S. Pat. No. 3,979,393 relates to the use of anhydride containing imidyl and isoimidyl compounds as curing agents for polyepoxide resins. In these examples, the imide containing adjuvants are low molecular weight materials which are primarily utilized as polyepoxide hardeners. Therefore, the quantity of imide containing adjuvant blended with the epoxy resin rarely exceeds that amount which is necessary to cure the epoxy resin.

The reason the imides are added as hardeners is that until now it has not been possible to blend or alloy polyimide resins in any quantity with epoxy resins to produce compatible resin blends suitable for laminating applications. For the most part, fully imidized polymers are insoluble in organic solvents, and, while some partially imidized polymers are soluble in organic solvents, the polyimide component is often not soluble in the epoxy component so that a compatible resin blend cannot be formed. In those cases where a blend of epoxy and polyimide resins can be formed which is compatible, very large amounts of organic solvent are required to achieve a blend solution viscosity which is suitable for the manufacture of prepregs. The necessity of evaporating and recovering these large amounts of solvents renders the process uneconomical.

We have discovered that a particular type of imide oligomer will form a compatible blend with an epoxy resin, and with other types of resins, using a moderate amount of solvent. The imide oligomer of this invention is formed from an imide polymer which contains amic acid groups that can be hydrolyzed so that the products of the hydrolization become compatible with the epoxy or other resin and serve to cure the resinous blend. By incorporating an imide oligomer into the resins, we have been able to achieve laminates having improved properties such as a higher glass transition temperature, better chemical resistance, and increased toughness. Wire enamels having good elongation and heat shock, and fast processing times can also be made from blends containing this imide oligomer. We have also found that a thermoplastic laminate can be made using the imide oligomer by itself.

FIG. 1 is an isometric view in section of a certain presently preferred embodiment of a laminate according to this invention.

FIG. 2 is an isometric view of a filament wound tube, such as a launch tube, according to this invention, partially cut away.

In FIG. 1, a layer 1 of a fibrous material 2 is impregnated with a resinous matrix 3 which has been B-staged to form prepregs 4. A stack of prepregs 5 heated under pressure to cure the resinous matrix to the C-stage forms laminate 6. A copper foil 7 has been bonded to one surface of the laminate.

In FIG. 2, filaments 8, for example, of glass, are wound and imbedded in resinous matrix 9, which has been cured to the C-stage, forming tube 10. Filament wound structures are made by passing roving through a resin bath and over a mandrill, where the resin is cured.

In the first step of preparing a laminate according to the process of this invention, a composition is prepared of a resinous component, (which can be a mixture of resinous components), an imide polymer having amic acid functionality, and a solvent. The resinous component, also called a "coreactive compound," is a monomer, oligomer, or polymer that is reactive with the imide oligomer that is formed by hydrolyzing the imide polymer. Suitable resinous components include bismaleimides and derivatives thereof, polyimides, diols and diacids, diacids and diamines, phenolic resins, capped isocyanates, and polyepoxides. Bismaleimides are formed by reacting maleic anhydride with an aromatic polyamine. The polyamine is a compound having at least two amine groups; preferably, it has exactly two amine groups because those compounds are more readily available. Derivatives of bismaleimides include bismaleimides that have been partially reacted with aromatic diamines or with unsaturated derivatives of bisphenol A. The reaction of the oligomer of this invention with diols and diacids will produce a partially interpenetrating network of a polyester-modified polyamide-imide. The reaction of the oligomer of this invention with diacids and diamines will produce a partially interpenetrating network of a polyamide-imide modified polyamide-imide. Since the reaction of the oligomer of this invention with diols and diacids, diacids and diamines, phenolic resins, and capped isocyanates evolves volatiles, these resin systems are limited to applications such as wire enamels and other coating applications. A polyepoxide is any type of epoxy resin having at least two epoxide groups. It may be cycloaliphatic, novolac, an epoxy prepared from methylene dianiline, an epoxy prepared from para-aminophenol, or a brominated epoxy. The preferred epoxy resins are the diglycidyl ethers of bisphenol A, however, as they are readily available.

The imide polymer which is hydrolyzed to produce the imide oligomer of this invention should have sufficient amic acid groups to be soluble in the solvent. However, if too many amic acid groups are present, the product will have deficient properties, and if too few amic acid groups are present, the polymer will tend to be insoluble. About 5 to about 50% of the total of amic acid plus imide groups along the polymer should be amic acid groups, and 50 to 95% imide groups, as it is the imide groups which enhance the properties of an impregnating resin.

The solvent should be an organic compound which is highly aprotic in order to dissolve the imide polymer. Suitably solvents include N-dimethyl formamide (DMF), N-methyl-2-pyrrolidone (NMP), and dimethyl sulfoxide. The preferred solvent is N-dimethyl acetamide (DMAC) because it is easily removed during B-staging. Mixtures of solvents can also be used. In addition, up to about 5% (all percentages herein are by weight based on total composition weight, unless otherwise indicated) of a hydrocarbon solvent such as xylene, toluene, or Solvesso, can be added to reduce the cost of the solvent. Sufficient water must also be present to hydrolyze substantially all of the amic acid groups in the imide polymer. Typically, the other components in the composition contain sufficient water as an impurity to perform this function, but if they do not, additional water must be added so that at least about the stoichiometric amount required for hydrolysis is present. With some resinous components, it is also possible to hydrolyze the imide polymer prior to its addition to the composition.

The composition comprises about 5 to about 95 phr (parts by weight per hundred parts by weight resin, where "resin" means the resinous component plus the imide polymer, based on total solids) of the imide polymer and about 5 to about 95 phr of the resinous component. Preferably, the composition comprises about 50 to about 80 phr of the resinous component and about 20 to about 50 phr of the imide polymer. The actual ratio of resinous component to imide polymer used is determined by the desired glass transition temperature, since a higher imide content will result in a higher glass transition temperature. The total composition is preferably about 10 to about 80% by weight solids, the remainder being the solvent. The composition may also include about 0.1 to about 0.7 phr of a catalyst, if desired, to shorten the gelation time. Suitable catalysts for polyepoxides and bismaleimides include tertiary amines such as 2-methylimidazole, and benzyl dimethyl amine; the preferred catalyst is 2-methylimidazole (2-MI). Catalysts, if needed, for other resinous components are well known in the art.

Other optional ingredients include about 0.1 to about 25% (based on total solids weight) of a filler such as alumina trihydrate. The filler performs the function of reducing the amount of resin required, which is expensive, and in addition, makes the composition less flammable. A final optional ingredient is about 0.1 to about 5% (based on total solids weight) of a pigment.

In preparing the composition, the resinous component, the imide polymer, the solvent, and the filler and pigment, if used, are cooked until no more amic acid functional groups are present. This can be usually accomplished by heating at about 100.degree. to about 150.degree. C., typically for about a half hour. Of course, the lower temperatures are used for longer times and the higher temperatures are used for shorter times. During hydrolysis, the water present in the composition decomposes the amic acid functional groups to form carboxylic acid and amine groups: ##STR1##

The resulting imide oligomer is an aromatic compound having a molecular weight which depends upon the number of amic acid groups in the imide polymer. The imide oligomer necessarily contains both amine groups and carboxylic acid groups, as a result of the hydrolysis, as well as at least one fully formed imide ring.

The carboxylic acid and amine groups in the imide oligomer then react with groups on the resinous component to form a new polymer containing all three groups. That this occurs is shown by infrared spectrographic analyses of samples of the composition taken at 5 minute intervals as it is being heated. When the resinous component is a polyepoxide, the spectrographic analysis shows the disappearance of both the amic acid peak and the epoxy peak and the growth of a new intermediate peak for the new polymer. Efforts to form the same new polymer by simply mixing the polyepoxide with the original imide polymer were not successful because the two polymers are not compatible and will not dissolve in each other. Nor could the new polymer be formed by first hydrolyzing the imide polymer, then adding the polyepoxide, because the imide portion of the hydrolyzed imide polymer is not soluble in the mixture. After cooling, the optional catalyst can be added if desired. In addition, at this time, additional solvent can be added to reduce the viscosity further, if desired.

In the next step in the process of making a laminate according to this invention, a substrate is impregnated with the composition containing the new polymer. The substrate may be of any fibrous material including glass, cotton, quartz, polyamide, polyaramid, paper, graphite, carbon, or mixtures thereof and may be in many forms including woven cloth, mat, or rovings as used in pultrusion or filament windings. The preferred substrate material is, of course, dependent upon laminate end use. The amount of resin solids impregnated into the substrate depends upon the type of substrate used in the application. Typically, about 20 to about 60% by weight resin solids are impregnated with about 40 to about 80% by weight of the substrate.

In the next step in the process of making a laminate according to this invention, the impregnated substrate is heated to B-stage the resin. The time and temperature required for B-staging depends upon the particular resin used, but generally speaking, the impregnated substrate is heated to the boiling point of the solvent or slightly higher. This results in the evaporation of the solvent and the advance of the resin to the B-stage, the point at which it is non-tacky and can be handled. The resulting article is a prepreg.

In the next step of the process of making a laminate according to this invention, the prepregs are stacked and heated under pressure to form a laminate. Copper foil may be placed on either or both surfaces of the stack to form a laminate suitable for making printed circuit boards. The temperature, time, and pressure used depend upon the materials and the properties desired, but about 150.degree. to about 220.degree. C. for one hour at 1,000 psi is typical.

The composition can also be used to make a wire enamel. In this case, the wire is simply run through the composition after the imide polymer is hydrolyzed, excess composition is removed by dies, wiping or other means, and, in a single step, the composition is cured to the C-stage and the solvents are evaporated. In addition, the composition can be used to make filament wound composite launch tubes, laminates used as components for ship propulsion room equipment, such as sub-base structures, generator covers, and gearcase components, and laminates used as electromagnetic launcher components.

The following is a description of the materials used in the examples:

"Epon 829"--a diglycidyl ether of bisphenol-A made by Shell Chemical Co. by reacting epichlorohydrin with bisphenol-A. In addition to the diglycidyl ether, "Epon 829" contains an unspecified level of a proprietary phosphonium halide catalyst. The material is supplied at 96.5% solids in xylene and contains a maximum 0.03 wt.% hydrolyzable chlorine on an as-is basis.

"Torlon 4000T"--a low acid value, high molecular weight poly(amide-imide) resin containing some amic acid functionality, supplied at 100% solids as a free flowing crumb by the Amoco Chemicals Corporation. The material was developed primarily as a high performance injection molding resin and has the following generalized structure: ##STR2##

"Tritherm 981"--a poly(amide-imide) wire enamel supplied at 26% total solids in 65/35 (by weight) NMP/xylene by the P. D. George Company.

"MY720"--a Ciba-Geigy high performance, tetrafunctional epoxy resin with the following structure: ##STR3## The material has an epoxide equivalent weight of 125 gm/equiv and is supplied at 100% solids.

"PLYOPHEN 94-308"--a monomeric, aromatic bismaleimide sold by Reichhold Chemicals Corp., made by condensing methylene dianiline and maleic anhydride. "IM-AD94-394"--a two component polyimide laminating resin sold by Reichhold Chemical Corp. One component is "PLYOPHEN 94-308" and the other is an unsaturated phenolic novolac oligomer.

"COMPIMIDE 183"--a totally aromatic two component polyimide impregnant sold by The Boots Company, PLC, Nottingham, England. It is made by reacting bismaleimides with m-aminobenzoic acid hydrazide at 100% solids.

The following four resinous reactor products based upon various polyepoxide resin/poly(amide-imide) resin combinations were prepared: Resin       A        B        C       D ______________________________________ Epoxy       "Epon    "MY270"- "Epon 829" "MY270" Component(s) 829"     "Epon 829" Poly(Amide-Imide) "Torlon  "Torlon  "Tritherm "Torlon Component   4000T"   4000T"   981"    4000T" ______________________________________

The following is a description of the preparation of these reactor products. A typical charge for the preparation of an "Epon 829"/"Torlon 4000T" resinous reactor product (Resin A) is presented in the following table: Weight   Wt.         Compo- Charged  (gm)        sition Material  Function (gm)     NV**  Equiv. (Wt. %) ______________________________________ "Epon 829" Epoxy    483.3    466.4 2.48  80.0 Resin "Torlon 4000T" Poly     116.6    116.6 --    20.0 (amide imide) DMAC      Solvent  349.7    --    --    -- Xylene*   Solvent   (16.9)  --    --    -- Total Charge       949.6    583.0 2.48  100.0 ______________________________________ *Not charged separately  "Epon 829" solvent **Nonvolatile.

Dimethyl acetamide (349.7 gm) was charged into a 2,000 ml round bottom, three necked flask fitted with an agitator, nitrogen inlet tube, thermometer, reflux condenser and a means for heating. The flask was swept with N.sub.2 gas for 5 minutes and the flow rate adjusted to maintain a slight positive N.sub.2 pressure in the flask throughout the balance of the run.

The agitator was started and the DMAC was slowly heated to 60.degree. C. whereupon neat "Torlon 4000T" (116.6 gm) was slowly added to the hot DMAC at such a rate as to prevent clumping. After the addition of the "Torlon 4000T" was complete, the slurry was heated to 105.degree. C. to effect complete dissolution. The uniform, smooth "Torlon 4000T"/DMAC solution was then cooled to 100.degree. C. and "Epon 829" (483.3 gm/2.48 equiv) was slowly added to the flask over a 5 minute period. After the "Epon 829" addition was complete, a small amount of the reaction mixture was removed for Gel Permeation Chromatographic (GPC) analysis and "Epon 829"/"Torlon 4000T" compatibility testing. Compatibility testing was accomplished by casting a small amount of material on a glass slide (termed a "pill" in the following log) and driving off the DMAC. A "hazy pill" indicates that "Torlon 4000T" was not soluble in "Epon 829."

After the initial samples had been taken the flask was slowly heated to 140.degree. C. and held there. Sampling was continued during the 140.degree. C. hold and, when a clear pill had been attained, the reaction was cooled and the product set aside for evaluation. The product (Resin A) had a solids content of 61.4% and a viscosity of 420 cps (#2 @ 20 rpm on the Brookfield Model; RVF measured @ 25.degree. C.). The significance of the GPC/IR data and other information obtained during the run will be discussed in a later section of this example.

The following is a log of the preparation of this reactor product. Temp. Time (.degree.C.) Remarks ______________________________________ 11:07 RT      N.sub.2, heat on DMAC, stirrer on 11:10 60     Start "Torlon 4000T" in slowly 11:15 95     "Torlon 4000T" in, hold H.sub.2 O droplets on condenser 11:16 105     Stir, hold temp. until uniform 11:27 100     Solution uniform, begin "Epon 829" addition 11:32 63     "Epon 829" in, heat to 140.degree. C., pill-1, GPC sample-1 11:38 75     Continue heating 11:44 100     Take pill-2 (hazy), continue heating 11:53 120     GPC sample-2, pill-3 (hazy), continue heating 12:05 140     Hold, GPC sample-3, pill-4 (hazy), viscosity drop 12:20 140     GPC sample-4, pill-5 (hazy), continue heating 12:35 140     GPC sample-5, pill-6 (clear), begin cooling 12:48 45     Continue cooling 12:58 35     Pour/store for evaluation ______________________________________

The same equipment but slightly different procedures were utilized to prepare Resins B, C, and D. Processing parameters and reactor charges for these materials are presented in the following Tables: Reactor Charge For Resin B Weight Charged Wt. (gm)  Composition Material Function (gm) NV   Equiv. (Wt. %) __________________________________________________________________________ "Epon 829" Epoxy Resin 342.0 330.0 1.753 55.0 "MY270" Epoxy Resin 120.0 120.0 0.960 20.0 "Torlon 4000T" Poly(amide- 150.0 150.0 --   25.0 imide) DMAC    Solvent 388.0 --   --   -- 1,000.0 600.0     100.0 __________________________________________________________________________ Processing Parameters For Resin B __________________________________________________________________________ Reaction Temperature - 140.degree. C. Reaction Time @ 140.degree. C. - 0.5 hr Wt. % Solids - 60.0% Viscosity - 1,086 cps (#2 @ 20 rpm) __________________________________________________________________________ Reactor Charge For Resin C Weight Charged        Composition Material  Function   (gm)     Equiv. (Wt. %) ______________________________________ "Epon 829" Epoxy Resin 420.0    2.23  70.0 Solids "Tritherm 981" Poly(amide 180.0    --    30.0 Solids    imide) NMP*      Solvent    370.5    --    -- Xylene*   Solvent    214.7    --    -- 1,185.2        100.0 ______________________________________ Processing Parameters For Resin C ______________________________________ Reaction Temperatures - 140.degree. C., 160.degree. C. Reaction Times - 0.5 hr @ 140.degree. C., 0.5 hr. @ 160.degree. C. Wt. % Solids - 50.6% Viscosity - 1,680 cps (#2 @ 20 rpm) ______________________________________ *Not charged  "Epon 829"/"Tritherm 981" solvents. Reactor Charge For Resin D Weight Charged        Composition Material  Function   (gm)     Equiv. (Wt. %) ______________________________________ "MY720"   Epoxy Resin 420.0    3.36  70.0 "Torlon 4000T" Poly(amide 180.0    --    30.0 imide) DMAC      Solvent    733.3    --    -- 1,333.3        100.0 ______________________________________ Processing Parameters For Resin D ______________________________________ Reaction Temperature - 140.degree. C. Reaction Time @ 140.degree. C. - 0.5 hr Wt. % Solids - 45.0% Viscosity - 1,010 cps (#2 @ 20 rpm) ______________________________________

Note that a 160.degree. C. processing temperature is required to achieve compatibility between "Epon 829" and "Tritherm 981" in Resin C. Heating is not required to achieve compatibility between "MY720" and "Torlon 4000T" (Resin D) for the specified composition. However, heating at 140.degree. C. is required to bring about the reduction in viscosity necessary for laminating applications.

Although no examples are provided, tetrabrominated polyepoxides such as Dow's "DER 542," "DER 521A75," and the like would have utility in the practice of this invention. Similarly, multifunctional epoxy resins other than "MY720" (such as epoxy novolac resins) would have application. In like manner, nondiglycidylether bisphenol-A resins such as Union Carbide's cycloaliphatic epoxy resin line could be utilized in the preparation of the disclosed amide-imide modified laminating resins.

Compositional data along with varnish properties for a series of laminating varnishes which demonstrate the utility of our disclosure is presented in the table which follows. The varnishes were formulated by charging an appropriate amount of Resin A, B, C, or D into a stainless steel beaker fitted with a propeller type agitator. A catalyst of 2-methylimidazole (0.28 wt.% on total resin solids) was charged and mixed until it had dissolved. Additional solvents, filler, pigments, and/or catalysts and the like could have been added at this stage in the formulation scheme. The varnishes were stirred 15 minutes prior to impregnation onto style 7628 glass cloth. Laminate     A    B       C      D Resin        A    B       C      D Wt. % "Epon 829" 74.77 54.83   69.80  -- Wt. % "MY720" --   19.94   --     69.80 Wt. % "Torlon 4000T" 19.94 24.93   --     29.92 Wt. % "Tritherm 981" --   --      29.90  -- Wt. % 2-MI    0.29 0.29    0.30   0.28 Impregnating Solids, 61.6 53.4    51.0   45.0 Wt. % Impregnating Solvents DMAC DMAC/Methyl Xylene/NMP DMAC/Xylene Cellosolve Varnish Viscosity, cps 350  400     1,665  1,010 Set-Time, Mins @ 153.degree. C. 32.8 17.0    40.4   25.1 __________________________________________________________________________

Note that in the above table the individual polyepoxide/poly(amide-imide) resins are presented in terms of composition. As an example, Laminate A contains 74.77% "Epon 829" and 19.94% "Torlon 4000T." The ratio of these numbers corresponds to the composition of Resin A. The same holds true for Laminate B; i.e., the ratio of tabulated "Epon 829"/"MY720"/"Torlon 4000T" corresponds to the composition of Resin B.

Style 7628 glass cloth was utilized to prepare 15".times.15" prepregs from the varnishes outlined in the above table. The wet prepregs were B-staged at 160.degree. C. for 10 minutes. After B-staging, the prepregs were approximately 40% resin and 60% glass cloth.

The B-staged prepregs were cut into 7".times.7" squares and press laminated by stacking nine (9) individual pieces between steel caul plates with Tedlar mold release sheets between the caul plates and prepreg stack. The molding packs were loaded into a cold press with five layers of kraft paper between the press platens and caul plates. Individual molding packs were then heated to 180.degree. C. under 1,000 psi in 45 minutes with an hour hold at 180.degree. C. Cooldown was accomplished under pressure.

General properties for the laminates are presented in the following table. Laminate     A        B        C      D Glass Transition, 149.4    157.0    159.0  205.7 DSC, .degree.C. Z-Direction* Expan. 60.6 .times. 75.4 .times. 75.1 .times. -- sion, In./In./.degree.C. 10.sup.-6 10.sup.-6 10.sup.-6 Solder Float 60+      60+      60+    60+ Sec. @ 525.degree. F. Acetone Resistance Excellent Excellent Excellent Excellent DMF Resistance Excellent Excellent Excellent Excellent ______________________________________ *Z-direction expansion coefficient measured from 40.degree. C. to Tg.

From the data in the abve table, it is apparent that a broad range of Tg values can be produced without the addition of external crosslinking agents. It is further apparent that the epoxy component as well as the poly(amide-imide) component can influence laminate Tg. Note that the utilization of "My720" in Laminate B and D results in Tg values higher than the 149.4.degree. C. shown for Laminate A. Laminate C, based upon "Tritherm 981," provides a higher Tg laminate (159.0.degree. C.) than Laminate A, based upon "Torlon 4000T" (149.4.degree. C.).

Laminate samples were placed in uncovered aluminum pans and aged in a vented, forced air oven at 225.degree. C. Weight losses observed during thermal aging are presented in the following table. Note that a production G-10 laminate was also heat aged at 225.degree. C. NEMA grade FR-4 laminate was also aged at 225.degree. C. but delaminated in 24 hours. LAMINATE A G-10              Wt.    B         C Hrs @ Wt. %   Hrs @   %    Hrs @ Wt. % Hrs @ Wt. % 225.degree. C. Loss    225.degree. C. Loss 225.degree. C. Loss  225.degree. C. Loss ______________________________________ 24   1.29     24     0.93  24   1.06   24   1.08 48   1.67     48     1.20  48   1.44   48   1.44 72   1.92     72     1.40  72   1.69   72   1.70 144   2.45     96     1.55  96   1.89   96   1.90 168   2.60    168     1.99 168   2.39  168   2.44 384   3.44    192     2.10 192   2.53  192   2.59 672   Failed  216     2.22 216   2.66  216   2.72 240     2.31 240   2.77  240   2.83 264     2.40 264   2.86  264   2.93 336     2.65 336   3.14  336   3.23 360     2.73 360   3.22  360   3.32 576     3.32 576   3.80  576   3.98 864     3.85 864   4.27  864   4.54 ______________________________________ Thermal aging at 225.degree. C. for Laminates A, B, and C was continued. *Resin content = approximately 40%.

After 864 hours at 225.degree. C. all of the polyepoxide/poly(amide-imide) based laminates were blister free and apparently retained their initial high degree of mechanical integrity.

A typical charge and accompanying log for the preparation of hydrolyzed "Torlon 4000T" is shown below. Material   Wt. Charged (Gm) Composition, Wt. % ______________________________________ "Torlon 4000T" 600.0       29.70 DMF        1,400.0       69.31 Deionized H.sub.2 O 20.0        0.99 2,020.0       100.00 ______________________________________ Tempera- Time  ture (.degree.C.) Remarks ______________________________________ 8:15  RT       Charge DMF/H.sub.2 O Into Reactor, Heat/N.sub.2 On 8:20  RT       Begin Charging T-4000 8:29   58      All T-4000 Charged 9:00  139      Refluxing-Gardner Vis. = Y @ 24.1.degree. C. 9:30  140      Gardner Viscosity = Q-R 10:00 140      Gardner Viscosity = N-O 10:15 140      Heat off - Cool & Store (Vis. = N-O) ______________________________________

Dimethyl formamide (1,400.0 gm) and deionized water (20.0 gm) were charged into a 3,000 ml round bottom flask fitted with an agitator, nitrogen inlet tube, thermometer, reflux condenser and a means for heating. The flask was swept wih N.sub.2 gas for 5 minutes and the flow rate adjusted to maintain a slight positive N.sub.2 pressure in the flash throughout the balance of the run. The agitator was started and the DMF/H.sub.2 O solution heated while the "Torlon 4000T" was added to flask at such a rate as to prevent clumping. After addition of the "Torlon 4000T" (58.degree. C.) the slurry was heated to 140.degree. C. and held until the solution viscosity dropped from Y to N-O. The resulting hydrolyzed product had a solids content of 29.5% solids and was utilized to prepare laminate 211184-42. Further heating would not have led to a further reduction in solution viscosity.

This example is provided to show that the "Torlon" hydrolysis product is resinous and can be processed utilizing conventional techniques.

A 161/2".times.491/2" swatch of style 7628 fiberglass cloth was continuously impregnated with hydrolyzed "Torlon 4000T" reactor product of Example 3. The wet swatch was then cut into three 161/2".times.161/2" sections and B-staged 7 minutes at 175.degree. C. to produce prepreg with a resin content of 32% by weight. The prepregs were cut into 151/2".times.71/4" strips and again impregnated with 211184-40. After B-staging 10 minutes at 175.degree. C., the prepregs had a resin content of 50.1% by weight.

A molding pack was constructed by stacking nine each 7".times.7" plys of prepreg between two silicone coated fiberglass bleeder plys. The molding pack was placed between steel caul plates and the whole loaded into a cold press with two layers of fiberglass cloth between the press platens and caul plates. The molding pack was then heated to 225.degree. C. under 1,000 psi in one hour with an hour hold at 225.degree. C. Cooldown was accomplished under pressure.

After lamination under the above conditions the resulting laminate was unitary and quite tough. A Tg value of 185.degree. C. was measured via Dynamic Mechanical Analysis (DMA). The evolution of cure volatiles during press lamination was not evident.

A 0.5 square inch section was cut from the laminate and placed into a sample jar containing 50 gms of DMF. After approximately one hour the resin had dissolved, thereby showing that the hydrolyzed "Torlon" remains essentially a thermoplastic after lamination. "Plyophen 94-308"

A typical charge and accompanying log for the preparation of an impregnating resin (211184-32) based upon hydrolyzed Torlon 4000T and Plyophen 94-308 is shown below. Wt.        Composition, Material     Wt. (Gm)  (Gm) NV    Wt. % ______________________________________ Hydrolyzed "Torlon" 600.0     196.2      50.0 (Example 3) "Plyophen 94-308" 196.2     196.2      50.0 796.2     392.4      100.0 ______________________________________ Temp. Time (.degree.C.) Remarks ______________________________________ 1:30 RT      N.sub.2, Agitator and Heat On 211082-127 and 94-308 1:40  90     Reaction Mixture Clear, .DELTA. .fwdarw. Reflux 1:54 142     Refluxing - Hold. Pill - Hazy 2:10 142     Pill - Still Hazy 2:22 143     Pill Hazy; .DELTA. .fwdarw. 150.degree. C. 2:55 150     DMF Off, Pill Slightly Hazy 3:02 153     27.1 gm DMF Off - Continue Heating 3:30 153     Heat Off - Pill Clear - Store Resin For Evaluation ______________________________________

Hydrolyzed "Torlon 4000T" (600.0 gm) and "Plyophen 94-308" (196.2 gm) were charged into a 2,000 ml round bottom, three necked flask fitted with an agitator, nitrogen inlet tube, thermometer, reflux condenser with Dean-Stark trap and a means for heating. The flask was swept with N.sub.2 gas for five minutes and the flow rate adjusted to maintain a slight positive N.sub.2 pressure in the flask throughout the balance of the run.

The agitator was started and the reaction mixture slowly heated to reflux. Compatibility testing was accomplished by casting a small amount of material on a glass slide (termed a "pill" in the log) and driving off the DMF. A "hazy pill" indicates that "Plyophen 94-308" is not soluble in the hydrolyzed "Torlon 4000T" solids. The reaction mixture was sampled during the 140.degree.-150.degree. C. hold and when a clear pill had been attained, the reaction was cooled and the product set aside for evaluation. The product had a solids content of 51.0%, a viscosity of 460 cps at 90.degree. C. and a gelation time of 45 minutes at 150.degree. C. The product was impregnated without further modification.

Approximately 400 gm of the impregnant from Example 5 was heated to 90.degree. C. and utilized to impregnate a 161/2".times.491/2" swatch of style 7628 fiberglass cloth. The wet swatch was cut into three 161/2".times.161/2" sections and B-staged 5 minutes at 170.degree. C. to produce prepreg with a 43.3% resin content. A molding pack was constructed by stacking nine each 7".times.7" plys of prepreg between two silicone coated fiberglass cloth bleeder plys. The molding pack was placed between steel caul plates and the whole loaded into a cold press with two layers of fiberglass cloth between the press platens and caul plates. The molding pack was heated to 225.degree. C. under 1,000 psi in 1 hour with a 1 hour and 15 minute hold at 225.degree. C. Cooldown was accomplished under pressure.

The resulting laminate was unitary, DMF resistant and had a Tg of 195.degree. C. as measured by DMA (FIG. 2). A portion of the laminate was post-baked 16 hours at 250.degree. C. Post-baking resulted in a 225.degree. C. Tg as measured via DMA. and "IM-AD 94-394"

An impregnating varnish based upon hydrolyzed "Torlon 4000T" and "IM-AD 94-394" was prepared via a kettling operation. The charge and accompanying log is shown below. Composition, Material    Wt. (Gm)  Wt. (Gm) NV Wt. % ______________________________________ Hydrolyzed Torlon 291.7      87.5       25.0 (Example 3) "IM-AD 94-394" 262.5     262.5       75.0 DMF         145.8     --          -- 700.0     350.0       100.0 ______________________________________ Temp. Time (.degree.C.) Remarks ______________________________________ 8:20 RT       Charge - 40 + DMF, Begin IM-AD 94-394 Addition, N.sub.2, Heat On 8:55  60      IM-AD 94-394 Addition Complete 9:06 130      Hold, Pill Taken - Hazy 9:10 135      Mantle Down, Cool to 130 - Pill - Hazy 9:13 132      Mantle Up 9:19 130      Pill - Hazy 9:32 134      Pill - Hazy; Heat Back 9:36 130      Pill Nearly Clear 9:37 130      Gardner Viscosity - Z-1 @ 25.5.degree. C., Transfer to Preparing Trough ______________________________________

Prepregs and a single nine ply laminate were prepared utilizing techniques described in Examples 3 and 4. The prepregs were staged 4 minutes at 150.degree. C. followed by five additional minutes at 170.degree. C. The resulting prepreg had a resin content of 41.6% and was laminated in a nine ply array under 1,000 psi for 1 hour at 225.degree. C. Cooldown was done under pressure. The resulting laminate was unitary, DMF resistant and had a Tg value of 225.degree. C. measured via DMA. Post bake would have resulted in increased Tg. and "Compimide 183"

The resin charge and accompanying log shown below pertains to the preparation of a laminating composition based upon hydrolyzed "Torlon 4000T" and "Compimide 183." Composition, Material    Wt. (Gm)  Wt. (Gm) NV Wt. % ______________________________________ "Compimide 183" 225.0     225.0       75.0 (Example 3) Hydrolyzed 4000T 250.0      75.0       25.0 DMF         125.0     --          -- 600.0     300.0       100.0 ______________________________________ Temp. Time (.degree.C.) Remarks ______________________________________ 8:45 RT       Charge - 40 + DMF; Heat, N.sub.2 On; Start 183 Addition 8:50  50      "Compimide 183" Addition Complete 8:54  80      183 Dissolved, .DELTA. .fwdarw. 130.degree. C. 9:02 130      Hold - Pill Taken, Slightly Hazy 9:17 129      Slightly Hazy Pill 9:26 129      Gardner Viscosity - M to N (330 cps @ 25.degree. C.) 9:41 130      Viscosity M-N 9:52 129      Heat Off, Cool - Hold For Evaluation ______________________________________

Prepreging and laminating techniques previously described were utilized with this resin. The resin was impregnated at 40.degree. C. and staged 3 minutes at 150.degree. C. followed by 4 additional minutes B-stage time at 170.degree. C. The resulting prepreg had a resin content of 38.0% and was laminated in a nine ply array at 225.degree. C. for 1 hour under 1,000 psi pressure. Cooldown was accomplished under pressure. The resulting laminate was unitary, well cured, DMF resistant and had a Tg of 212.degree. C. via DMA.

A varnish was prepared of the following composition. Wt.        Composition, Material     Wt. (Gm)  (Gm) NV    Wt. % ______________________________________ Hydrolyzed "Torlon 300.0     90.0       74.91 4000" (Example 3) Epon 829     31.09     30.0       24.97 2-MI         0.14      0.14       0.12 333.23    120.14     100.00 ______________________________________

The varnish was submitted for evaluation as an overcoat for current low cost polyester coated wire and was indicated in a pilot wire tower. The varnish had fast processing characteristics, and the coating exhibited good elongation and heat shock characteristics. The following table gives the results of some of these experiments. Sample A Sample B ______________________________________ Tower Speed       28        32 (Ft/min.) Quick Jerk        Passed    Passed Elongation + 1 .times. (%) Passed    Passed Electric Stress (KV) 7.0-8.0   6.5-8.3 1 .times. heat shock 200.degree. C. Passed    Passed 220.degree. C. Passed    Passed 240.degree. C. Passed    Passed 260.degree. C. Passed    Passed ______________________________________

## Claims

1. A laminate comprising a plurality of layers of a substrate imbedded within a cured resinous matrix, said resinous matrix comprising, in an uncured state: functionality to be soluble in said solvent, where about 5 to about 50% of the total of amic acid plus imide groups on said polyimide are amic acid groups, and about 50 to about 95% are imide groups; and functionality of said polymer.

2. A laminate according to claim 1 including a metal conductor bonded to at least one surface of said laminate.

3. A laminate according to claim 2 wherein said metal conductor is copper circuitry.

4. A laminate according to claim 2 wherein said metal conductor is copper foil.

5. A laminate according to claim 1 wherein said solvent is selected from the group consisting of dimethyl formamide, dimethylamine, N-methyl pyrrolidinone, dimethylsulfoxide, and mixtures thereof.

6. A laminate according to claim 1 which includes about 0.1 to about 5% of a hydrocarbon solvent.

7. A laminate according to claim 1 which includes about 0.1 to about 25%, based on solids, of a filler.

8. A laminate according to claim 7 wherein said filler is alumina trihydrate.

9. A laminate according to claim 1 which includes about 0.1 to about 5%, based on solids, of a pigment.

10. A laminate according to claim 1 which includes about 0.1 to about 0.7 phr of a catalyst.

11. A laminate according to claim 10 wherein said catalyst is 2-methylimidazole.

12. A laminate according to claim 1 wherein said polyepoxide is about 50 to about 80 phr and said polyimide is about 20 to about 50 phr.

13. A laminate according to claim 1 wherein said polyepoxide is a diglycidyl ether of bisphenol A.

14. An enameled wire comprising an elongated conductor coated with a cured composition which comprises polyimide having both a first functionality that is imide and a second functionality selected from the group consisting of amic acid functionality, hydrolyzed amic acid functionality, and mixtures thereof, where said second functionality is about 5 to about 50% of the total of said first and second functionalities, and a sufficient amount of said second functionality is present to solubilize said polyimide; said polyimide; and said polyimide, where said coreactive compound is selected from the group consisting of monomers, polymers, and mixtures thereof.

15. A filament wound cylinder comprising roving embedded within a cured resinous matrix, said resinous matrix comprising, in an uncured state: functionality to be soluble in said solvent, where about 5 to about 50% of the total of amic acid plus imide groups on said polyimide are amic acid groups, and about 50 to about 95% are imide groups; and

16. A filament wound cylinder according to claim 15 wherein said roving is glass.

17. A filament wound cylinder according to claim 15 wherein said solvent is selected from the group consisting of dimethyl formamide, dimethylamine, N-methyl pyrrolidinone, dimethylsulfoxide, and mixtures thereof.

18. A filament wound cylinder according to claim 15 which includes about 0.1 to about 5% of a hydrocarbon solvent.

19. A filament wound cylinder according to claim 15 which includes about 0.1 to about 25%, based on solids, of a filler.

20. A filament wound cylinder according to claim 19 wherein said filler is alumina trihydrate.

21. A filament wound cylinder according to claim 15 which includes about 0.1 to about 5%, based on solids, of a pigment.

22. A filament wound cylinder according to claim 15 which includes about 0.1 to about 0.7 phr of a catalyst.

23. A filament wound cylinder according to claim 22 wherein said catalyst is 2-methylimidazole.

24. A filament wound cylinder according to claim 15 wherein said coreactive compound is about 50 to about 80 phr and said polyimide is about 20 to about 50 phr.

25. A filament wound cylinder according to claim 15 wherein said polyepoxide is a diglycidyl ether of bisphenol A.

26. A method of making a laminate comprising: polyimide having both a first functionality that is imide and a second functionality selected from the group consisting of amic acid functionality, hydrolyzed amic acid functionality, and mixtures thereof, where said second functionality is about 5 to about 50% of the total of said first and second functionalities, and a sufficient amount of said second functionality is present to solubilize said polyimide; said polyimide; and said polyimide, where said coreactive compound is selected from the group consisting of monomers, polymers, and mixtures thereof; substantially eliminated; said composition, and form a prepreg;

27. A method according to claim 26 wherein said composition is heated in step (B) at about 100.degree. to about 150.degree. C. for about 1/2 hour.

28. A method according to claim 26 wherein additional solvent is added after step (B) to lower the viscosity of said composition.

29. A method according to claim 26 wherein said fibrous substrate is fiber glass cloth.

30. A method according to claim 26 wherein said impregnated substrate is about 20 to about 60% resin solids and about 40 to about 80% fibrous substrate.

31. A method according to claim 26 wherein said heating in step (F) is at about 150.degree. to about 220.degree. C. for about 1 hour at about 1000 psi.

32. A method according to claim 26 wherein said coreactive compound is a polyepoxide.

33. A method of making a laminate comprising said solvent, where about 5 to about 50% of the total of amic acid plus imide groups on said polyimide are amic acid groups, and about 50 to about 95% are imide groups; and functionality of said polyimide; substantially eliminated.

34. A laminate made according to the method of claim 33.