# Patent

## Title
Epoxy-terminated polyester

## Abstract

An epoxy terminated polyester having the structure




    
    
        wherein R1— is
    
    






    
    
        G— is
    
    






    
    
        j is 0 to 5, —R2— is a divalent organic group, —R22— is a divalent alkyl group, and —R22— is a divalent alkyl group.

## Background
Epoxy-terminated compounds are useful for a variety of purposes. For example, epoxy-terminated compounds may undergo chemical reactions either with themselves or with one or more co-reactant to form polymers that have high molecular weight and/or are crosslinked. Such polymers are often useful for one or more of a wide variety of purposes, such as, for example, as adhesives.
US 2008/0081883 describes polyester polyols that are reaction products of 2,5-furandicarboxylic acid and polyepoxides. It is desired to provide epoxy terminated compounds that react well with polyamines to form useful adhesive compositions, such as, for example, laminating adhesives. It is also desired to provide epoxy terminated compounds that have desirably low viscosity over the temperature range of from approximately 25° C. to approximately 70° C.
The following is a statement of the invention.
The first aspect of the present invention is an epoxy terminated polyester having the structure




R1— is




G— is





j is 0 to 5, —R2— is a divalent organic group, —R21— is a divalent alkyl group, and —R22— is a divalent alkyl group.

The following is a detailed description of the invention.
As used herein, the following terms have the designated definitions, unless the context clearly indicates otherwise.
An epoxy terminated compound is a compound that contains one or more structure I




A diepoxide is a compound having exactly two groups of structure I. A glycidyl ether terminated compound is a compound that contains one or more structure II





An ester linkage is the structure III




A polyester is a compound that has two or more ester linkages. A polyol is a compound that has two or more —OH groups. A diol is a compound that has exactly two —OH groups. A polyamine is a compound that has two or more amine groups; the amine groups may be primary or secondary or a mixture thereof. A diamine is a compound that has exactly two amine groups; a diamine may have two primary amine groups, two secondary amine groups, or one primary amine group and one secondary amine group. A dicarboxylic acid is a compound having exactly two —COOH groups.

An aliphatic group is a chemical group that contains only carbon and hydrogen atoms and that contains no aromatic rings. A cycloaliphatic group is an aliphatic group that contains one or more cyclic structures. An alkyl group is an aliphatic group that has no double bonds. Alkyl groups include, for example, monovalent and divalent alkyl groups such as, for example, methylene groups, methyl groups, ethylene groups, ethyl groups, and larger alkylene and alkyl groups. A cycloalkyl group is an alkyl group that contains one or more cyclic structures. An aromatic group is any group having an aromatic ring.
An aliphatic amine is an amine in which the nitrogen atom of each amine group is bonded to a carbon atom that is part of an aliphatic group. An aromatic amine is an amine in which the nitrogen atom of each amine group is bonded to a carbon atom that is part of an aromatic ring.
When a ratio is said herein to be X:1 or greater, it is meant that the ratio is Y:1, where Y is greater than or equal to X. For example, if a ratio is said to be 3:1 or greater, that ratio may be 3:1 or 5:1 or 100:1 but may not be 2:1. Similarly, when ratio is said herein to be W:1 or less, it is meant that the ratio is Z:1, where Z is less than or equal to W. For example, if a ratio is said to be 15:1 or less, that ratio may be 15:1 or 10:1 or 0.1:1 but may not be 20:1.
The composition of the present invention is an epoxy terminated polyester having structure IV




In structure IV, the two —R1 groups may be identical or different. Each R1 group has the structure V





The group —R2— is a divalent organic group having fewer than 50 carbon atoms. The group G— has the structure II defined herein above. The number j is 0 to 5. The group —R21— is a divalent alkyl group. The group —R22— is a divalent alkyl group.

The composition of the present invention may also contain, in addition to one or more compounds having structure IV, one or more compounds having structure IVA




where —B1— has the structure





—B2— has the structure





-Q- has the structure

—R21O—R22j 

j is 0 to 5, and n is 1 to 6. The group —R21— is a divalent alkyl group. The group —R22— is a divalent alkyl group.

Preferably, —R2— is a group having structure VI




The number p is 0 to 20. Preferably p is 0 to 10; more preferably 0 to 5. Each —R3—, each —R4—, and each —R5— is, independent of the other, a divalent organic group. Within a single —R2— group, if p is 2 or greater, the various —R3— groups may be identical to each other or different from each other. Within a single —R2— group, if p is 2 or greater, the various —R4— groups may be identical to each other or different from each other.

Preferably, —R3— is selected from one or more divalent aliphatic groups, one or more divalent aromatic hydrocarbon groups, or a mixture thereof. Among aliphatic groups, preferred are alkyl groups; more preferred are linear or branched alkyl groups; more preferred are linear alkyl groups. Among aliphatic groups, preferred are those with 1 or more carbon atoms; more preferred are those with 2 or more carbon atoms; more preferred are those with 3 or more carbon atoms. Among aliphatic groups, preferred are those with 12 or fewer carbon atoms; more preferred are those with 8 or fewer carbon atoms; more preferred are those with 6 or fewer carbon atoms. Among aliphatic groups, preferred is —CH2CH2CH2CH2—.
Among aromatic groups, preferred are those with the structure




including mixtures of isomers; more preferred is





The groups that are suitable and preferred for —R5— are the same as those for —R3—. The group —R5— may be different from all of the —R3— groups, or —R5— may be the same as one or all of the —R3— groups.
Preferably, —R4— is either an aliphatic group or is an aliphatic ether group. An aliphatic ether group has the structure VII

—R8—O—R9r—O—R10—  VII

where —R8— and —R9— (if present) and —R10— are aliphatic groups, and where r is 0 to 10. The groups —R8— and —R9— (if present) and —R10— may be identical or may be different from each other. When —R4— is an aliphatic ether group, the following preferences apply to —R8—, —R9— (if present), —R10—, and r. Preferably, —R8— and —R9— (if present) and —R10— are identical. Preferably —R8— and —R9— (if present) and —R10— are linear or branched alkyl groups. Preferably —R8— and —R9— (if present) and —R10— each have 4 or fewer carbon atoms; more preferably 3 or fewer carbon atoms; more preferably exactly 2 carbon atoms. Preferably, r is 0 to 10; more preferably 0 to 5; more preferably 0 to 2; more preferably zero. When —R4— is an aliphatic group, —R4— is preferably an alkyl group; more preferably a linear alkyl group. When —R4— is an aliphatic group, —R4— has 1 or more carbon atom. When —R4— is an aliphatic group, —R4— preferably has 6 or fewer carbon atoms; more preferably 4 or fewer carbon atoms; more preferably 3 or fewer carbon atoms; more preferably exactly 2 carbon atoms.

In some embodiments (herein called “mixed polyester” embodiments), p is greater than 1, and some of the —R3— groups are not identical to other —R3— groups. In some mixed polyester embodiments, —R2— has the structure VIII




The groups —R3— and —R4— and —R5— are as defined herein above, and q is 1 or higher. Preferably q is 0 to 9; more preferably 1 to 4. The suitable and preferable groups for —R6— are the same as those for —R4—. The suitable and preferable groups for —R7— are the same as those for —R3—. In some mixed polyester embodiments (herein called “MP1” embodiments), —R5— is identical to —R3—, —R6— is identical to —R4—, and —R7— is different from —R3—. In some MP1 embodiments, all the —R4— groups are identical to each other; in other MP1 embodiments, some —R4— groups are different from other —R4— groups. In some mixed polyester embodiments (herein called “MP2” embodiments), —R5— is identical to —R7—, —R6— is identical to —R4—, and —R7— is different from —R3—. In some MP2 embodiments, all the —R4— groups are identical to each other; in other MP2 embodiments, some —R4— groups are different from other —R4— groups.

Preferred embodiments are selected from the following:

    
    
        (a) embodiments in which p=0;
        (b) embodiments in which p is 1 or greater and in which all the —R3— groups are identical to each other, all the —R4— groups are identical to each other, and —R5— is identical to —R3—;
        (c) MP1 embodiments; and
        (d) MP2 embodiments;
    
    


In structure V, j is preferably 1 or more. In structure V, j is preferably 5 or less; more preferably 4 or less; more preferably 3 or less; more preferably 2 or less. In structure V, j is most preferably 1.
In structure V, —R21— is a divalent alkyl group. Preferably, —R21— has 2 or more carbon atoms; more preferably 3 or more carbon atoms. Preferably, —R21— has 6 or fewer carbon atoms; more preferably 5 or fewer carbon atoms; more preferably 4 or fewer carbon atoms. Most preferably, —R21— has 3 carbon atoms. Among embodiments in which —R21— has 3 carbon atoms, preferably —R21— is selected from structures XX, XXI, and XXII:




In some embodiments, a mixture of polyesters will be present in which one polyester will have —R21— that is one of XX, XXI, or XXII, and another polyester will be present in which —R21— is a different one of XX, XXI, or XXII.

In structure V, if j is 1 or more, the suitable and preferred structures for —R22— are the same as those for —R21—. The group-R22— may be the same as —R21— or different from —R21—. If j is 2 or more, each —R22— may be the same as every other —R22— or some —R22— groups may be different from other —R22— groups. Preferably, every —R22— has the same number of carbon atoms as every other —R22—. Preferably —R21— has the same number of carbon atoms as every —R22— group. Preferably, every —R22— has three carbon atoms. Preferably, at least one —R22— has structure XXI or XXII.
The epoxide terminated polyesters of this invention will preferably have an Epoxide Equivalent Weight (EEW) of 275 or higher; more preferably 350 or higher; more preferably 400 or higher. The epoxide terminated polyesters of this invention will preferably have an Epoxide Equivalent Weight (EEW) of 3500 or lower; more preferably 2500 or lower; more preferably 2000 or lower. The number-average molecular weight of the epoxy terminated polyester of the present invention will preferably be 500 or higher; more preferably 1000 or higher. The number-average molecular weight of the epoxy terminated polyester of the present invention will preferably be 8000 or lower, more preferably 6000 or lower, and more preferably 3500 or lower.
It is useful to characterize the level of low molecular weight (≦1000 Daltons) species present in the composition of the present invention. The level of low molecular weight species is defined as the percentage by weight of species having molecular weight of less than or equal to 1000 Daltons, based on the total weight of the composition. The level of low molecular weight species is preferably 55% or less; more preferably 30% or less; more preferably 25% or less.
The composition of the present invention may be made by any method. A preferred method includes reacting at least one diepoxide with at least one dicarboxylic acid. The diepoxide has the structure IX

G—Q—G  IX

G— is defined as in structure V. Q is defined as in structure IVA. The dicarboxylic acid has the structure X





The group —R2— is defined as in structure IV. Sufficient amount of compound having structure IX is used so that the reaction produces compound having structure IV.

Preferred compounds of structure X have acid value (which is measured as described below) of 110 or higher; more preferably 120 or higher; more preferably 125 or higher. Preferred compounds of structure X have acid value of 260 or lower; more preferably 200 or lower; more preferably 175 or lower. Preferred compounds of structure X have molecular weight of 430 or higher; more preferably 560 or higher; more preferably 640 or higher. Preferred compounds of structure X have molecular weight of 1020 or lower; more preferably 940 or lower; more preferably 900 or lower. Mixtures of suitable Mixtures of suitable compounds of structure X are also suitable. are also suitable.
In the reaction of at least one diepoxide with at least one dicarboxylic acid, the stoichiometric ratio of epoxide groups to carboxylic acid groups will preferably be 3.1:1 or greater; more preferably 2.9:1 or greater; more preferably 2.7:1 or greater. The stoichiometric ratio of epoxide groups to carboxylic acid groups will preferably be 2:1 or less; more preferably 1.6:1 or less; more preferably 1.3:1 or less.
The reaction of diepoxide with dicarboxylic acid is optionally conducted in the presence of a catalyst. Preferred catalysts are triaryl phosphorous compounds with a soluble chromium catalyst, tetra-substituted phosphonium salts, quaternary ammonium salts, carbonate salt, hydroxide salts, and salts of carboxylic acids. More preferred are tetra-substituted phosphonium salts, carbonate salts, and salts of carboxylic acids.
When a triaryl phosphorous compound is used in combination with a chromium compound, the preferred triaryl phosphorous compounds are triaryl phosphines. Preferred triaryl phosphines are triphenyl phosphine tritolyl phosphine, trixylyl phosphine, and trinaphthyl phosphine. When a triaryl phosphorous compound is used in combination with a chromium compound, the preferred the preferred chromium compounds are chromium triacetate and chromium trichloride. Among the tetra-substituted phosphonium salts, preferred are alkyltriphenylphosphonium salts, tetraarylphosphonium salts, benzyltrialkylphosphonium salts, and tetraalkylphosphonium salts; more preferred are alkyltriphenylphosphonium salts and benzyltrialkylphosphonium salts. Among alkyltriphenylphosphonium salts, preferred are ethyltriphenylphosphonium acetate/acetic acid complex, and ethyltriphenlyphosphonium iodide; more preferred is ethyltriphenylphosphonium iodide. Among tetraalkylphosphonium salts, preferred is tetrabutylphosphonium acetate/acetic acid complex. Among benzyltrialkyl phosphonium salts, preferred is benzyltrimethyl phosphonium chloride. Among tetraarylphosphonium salts, preferred is tetraphenylphosphonium bromide.
Among the quaternary ammonium salts, preferred are benzyltrimethylammonium chloride, tetramethylammonium chloride, and diphenyldimethylammonium chloride. Among the salts of carboxylic acids, preferred are sodium or potassium salts of mono-carboxylic acids; more preferred are sodium acetate, potassium acetate, sodium propionate, potassium propionate, sodium benzoate, potassium benzoate, sodium citrate, potassium citrate, sodium lactate, potassium lactate, sodium tartrate, potassium tartrate, and sodium potassium tartrate. Among the inorganic bases, preferred are sodium carbonate, potassium carbonate, sodium hydroxide, and potassium hydroxide.
The preferred catalysts for the preparation of epoxy terminated polyesters are ethyltriphenlyphosphonium iodide, benzyltrimethylammonium chloride, sodium carbonate, and sodium acetate.
When tin or titanate compounds are used in the preparation of carboxylic terminated polyester resins via the reaction of diol with dicarboxylic acid, the level preferably is in the range of 0.0001 to 0.05 wt %.
When the group —R2- has structure VI with p of 1 or greater, the compound having structure X is preferably made by one or more reaction of one or more dicarboxylic acid with one or more diol.
Embodiment (a) defined herein above is preferably made by reaction of a diepoxide with a dicarboxylic acid having the structure HOOC—R11—COOH. Suitable and preferred —R11— groups are the same as the suitable and preferred —R3— groups.
Embodiment (b) defined herein above is preferably made by reaction of a diepoxide with a dicarboxylic acid that is a polyester (herein called “PEb1”). PEb1 is preferably made by reacting a single dicarboxylic acid (“DAb1”) with a single diol (“DOb1”). DAb1 has the structure HOOC—R12—COOH. Suitable and preferred —R12— groups are the same as the suitable and preferred —R3— groups. DOb1 has the structure HOR13—OH, where —R13— has the structure VII. Suitable and preferred —R13— groups are the same as those described for structure VII. A sufficient amount of DAb1 is used so that the reaction with DOb1 will produce a polyester that is a dicarboxylic acid.
Embodiment (c) defined herein above is preferably made by reaction of a diepoxide with a dicarboxylic acid that is a polyester (herein called “PEc1”). PEc1 is preferably made by reacting a single dicarboxylic acid (“DAc1”) with an intermediate polyester (“PEc2”). DAc1 has the structure HOOC—R13—COOH. Suitable and preferred —R13— groups are the same as the suitable and preferred —R3— groups. PEc2 is preferably made by reaction of a dicarboxylic acid (“DAc2”) with one or more diol (“DOc1”). DAc2 has the structure HOOC—R14—COOH. Suitable and preferred —R14— groups are the same as the suitable and preferred —R3— groups. Preferably DAc2 is different from DAc1. DOc1 has the structure HOR15—OH, where —R15— has the structure VII. Relative amounts of DOc1 and DAc2 are used so that a significant amount of the product PEc2 is formed that has one terminal —OH group and one terminal —COOH group.
Embodiment (d) defined herein above is preferably made by reaction of a diepoxide with a dicarboxylic acid that is a polyester (herein called “PEd1”). PEd1 is preferably made by reacting a single dicarboxylic acid (“DAd1”) with an intermediate polyester (“PEd2”). DAd1 has the structure HOOC—R16—COOH. Suitable and preferred —R16— groups are the same as the suitable and preferred —R3— groups. PEd2 is preferably made by reaction of a dicarboxylic acid (“DAd2”) with one or more diol (“DOd1”). DAd2 has the structure HOOC—R17—COOH. Suitable and preferred —R17— groups are the same as the suitable and preferred —R3— groups. Preferably DAd2 is different from DAd1. DOd1 has the structure HOR18—OH, where —R18— has the structure VII. Relative amounts of DOd1 and DAd2 are used so that a significant amount of the product PEd2 is formed that has two terminal —OH groups.
Reactions between carboxylic acid groups and hydroxyl groups are preferably conducted in the presence of one or more catalyst. Preferred catalysts are tin compounds and titanate compounds. Among tin compounds, preferred are dibutyltins, tetrabutyltins, tin tetrachloride, dioctyltins, monobutyltins, and stannous tins; more preferred are hydroxybutyltin oxide, monobutyltin tris(2-ethylhexanoate), and stannous 2-ethylhexanoate. Among titanate compounds, preferred are tetraalkyltitanates; more preferred are tetra(iso-propyl) titanate and tetra(n-butyl) titanate.
For reactions between carboxylic acid groups and hydroxyl groups, when a catalyst is present, the preferred amount is 0.0001% to 0.05% by weight based on the sum of the weights of the compounds bearing carboxylic acid groups plus the compounds bearing hydroxyl groups.
The compositions of the present invention may be used for a wide variety of purposes. Preferably, a composition of the present invention is used as an ingredient in an adhesive composition that is used to bond a first substrate to a second substrate. Preferably, one or more composition of the present invention is mixed with a curative compound and optionally with a solvent; the mixture is applied to a first substrate to form a layer on the first substrate; solvent (if present) is evaporated or allowed to evaporate; a second substrate is brought into contact with the layer of the mixture; and the mixture is cured or allowed to cure.
Curative compounds are compounds that have two or more groups capable of reacting with epoxy groups. Preferred curative compounds are amino compounds. Preferred amino compounds are phenalkamines, phenalkamides, and amine-terminated amide resins. Amine-terminated amide resins are reaction products of dicarboxylic acids and diamines. For formation of amine-terminated amide resins, preferred dicarboxylic acids are dimer acids, which are the reaction products of two molecules of an unsaturated fatty acid. Unsaturated fatty acids have the structure R19—COOH, where R19— is an aliphatic group having eight or more carbon atoms one or more carbon-carbon double bond. Preferred diamines are ethylenediamine, diethylenetriamine, triethylenetriamine, tetraethylenepentamine, piperazine, aminoethylpiperazine, isophorone diamine, xylylenediamine, and mixtures thereof.
Preferred substrates are polymer films, metalized polymer films, metal foils, polymer-backed metal foils, ceramic coated polymer films, and combinations thereof.
The following are examples of the present invention.
Abbreviations used below are as follows:

    AV=Acid Value, measured by the method of ASTM D3644-06 (American Society for testing and Materials, Conshohocken, Pa., USA).
    OHN=Hydroxyl Number, measured by the method of ASTM E1899-08.
    Amine Value=measured by the method ASTM D2074-07 for Test Methods for Total, Primary, Secondary, and Tertiary Amine Values of Fatty Amines by Alternative Indicator Method.
    Visc.=Viscosity, which is measured by employing a Brookfield RV DV-II+ Viscometer with a thermostated small sample adapter with a spindle #27 and varying the temperature over a range of 25 to 70° C. in increments of 5° C. and allowing the sample to stabilize at temperature for 20 to 30 mins prior to recording viscosity. Viscosity is reported in milliPascal*seconds (mP*s), which is equal to centipoise.
    PO-DE1=reaction product of dipropylene oxide and epichlorhydrin, containing a mixture of products including the following:






    PO-DE2=reaction product of dipropylene oxide and epichlorhydrin, containing a mixture of products including the following:






    The DER 736, from Dow Chemical, has the flowing properties: EEW is 182.9, (SEC Analysis Mn 500, Mw 600, Mz 800, Polydispersity 1.2, Wt Fraction ≦500 Dalton 44.6%, Wt. Fraction ≦1000 Daltons 92.0%.)
    FascatTM 9100=hydroxybutyltin oxide, from Arkema, Inc., commercial grade
    UnidymeTM 22=dimerized fatty acid, from Arizona Chemical, AV=192.9.
    CardoliteTM NC-541LV=phenalkamine curing agent, from Cardolite Corporation; Amine Value is 340, Active Hydrogen Equivalent is 125.
    PolypoxTM H015=Mannich base curing agent, from The Dow Chemical Company; Amine Value of 375; Active Hydrogen Equivalent is 75.
    PolypoxTM P370=polyaminoimidazoline hardener for epoxy resins, from The Dow Chemical Company; Amine Value of 485; Active Hydrogen Equivalent is 95.
    EpikureTM 3140=polyamide curing agent, reaction product of dimerized fatty acid and polyamines, from Momentive; Amine Value of 375; Active Hydrogen Equivalent of 95.
    Coex PP (75SLP)=Exxon Mobil Bicor SLP Oriented Polypropylene, Non-Heat Sealable, thickness 19 micrometers (0.75 mils).
    Coex PP (70SPW)=Exxon Mobil Bicor SPW Coextruded Polypropylene, thickness 18 micrometers (0.70 mils).
    PET=DuPont, Polyester, Poly(ethylene glycol-terephthalate), thickness 23 micrometer (92 Gauge) thick polyester film.
    PE (GF-19)=Berry Plastics Corp., High slip low density polyethylene film, thickness 25.4 micrometers (1.0 mil).
    Nylon=Honeywell Capran Emblem 1500, Biaxially Oriented Nylon 6 Film, thickness 15 micrometers.
    PET-Met=FILMTech Inc., Metallized Polyester film, thickness 25.4 micrometers.
    OPP-Met=AET Films, Metallized Oriented Polypropylene Film, MT Film, Heat Sealable, thickness 18 micrometers.
    Backed Foil=12 micrometer (48 Gauge) Polyester (PET) Film laminated to 0.00035 mil Al Foil with Adcote 550/Coreactant F at 3.26 g/m2 (2.00 lbs/ream).
    PET (92LBT)=DuPont, Polyester, Poly(ethylene glycol-terephthalate), thickness 23 micron (92 Gauge).
    Mn=number-average molecular weight
    Mw=weight-average molecular weight
    EEW=epoxy equivalent weight, which is the mass per mole of epoxy groups
    Active Hydrogen Equivalent=mass per mole of active hydrogens; an active hydrogen is a hydrogen atom attached to the nitrogen atom of an amine group.




EXAMPLE 1
Polyester Preparation












Item
Monomer/Intermediate
Charge

















1
Isophthalic Acid
1023.35


2
Diethylene Glycol
572.30


3
Ethylene Glycol
315.60


4
Fascat 9100 (Hydroxybutyltin oxide)
0.5842


5
Adipic Acid
1349.81









Charged Items 1-4 to vessel at Ambient Temperature (25-30° C.). Heated resin to 100° C. under Nitrogen with stirring. Heated resin to 225° C. and hold at 225° C., When ca.50% of theoretical water was off. Monitored AV and In-Process Viscosity. Maintained at 225° C. until AV<ca. 80. Cooled Resin to <125° C. Added Item 5; Maintained at 125-135° C. for 0.50 Hrs. Increased Temp to 225° C. and Maintained at 225° C. Monitored AV and Visc; Maintained at 225° C. until AV<ca. 200. Cooled Resin to about 150° C.; Filtered and Packaged. The final resin had the following properties: Acid Value (AV) 199, Mn 650, Mw 1250, Mz 2050, Wt. Fraction ≦500 Daltons 22.3%, Wt. Fraction ≦1000 Daltons 49.5%, Viscosity at 24.5° C. of 515,000 mPa*s.
EXAMPLE 2
Polyester Preparation












Item
Ingredient
Charge (g)

















1
Isophthalic Acid
451.50


2
Diethylene Glycol
1081.30


3
Fascat 9100 (Hydroxybutyltin oxide)
0.5543


4
Adipic Acid
1600.78









Charged Items 1-3 to vessel at Ambient Temperature (25-30° C.). Heated resin to 100° C. under Nitrogen with stirring. Heated resin to 225° C. and held at 225° C., When ca.50% of theoretical water was off. Monitored AV and In-Process Viscosity. Maintained at 225° C. until AV<ca. 75. Cooled Resin to <125° C. Add Item 4; Maintained at 125-135° C. for 0.50 Hrs. Increased Temp to 225° C. and Maintained at 225° C.; Applied Vacuum at 400 mm as needed as to decrease AV to final target property. Monitored AV and Visc; Maintained at 225° C. until AV<ca. 155. Cooled Resin to about 150° C.; Filtered and Packaged. The final resin had the following properties: Acid Value (AV) 149.73, Mn 950, Mw 1750, Mz 2550, Wt. Fraction ≦500 Daltons 10.6%, Wt. Fraction ≦1000 Daltons 32.1%, Viscosity at 25° C. of 29500 mPa*s.
EXAMPLE 3
Polyester Preparation












Item
Ingredient
Charge (g)

















1
Isophthalic Acid
451.94


2
Diethylene Glycol
567.80


3
Ethylene Glycol
316.34


4
Fascat 9100 (Hydroxybutyltin oxide)
0.6028


5
Adipic Acid
1601.83









Charged Items 1-4 to vessel at Ambient Temperature (25-30° C.). Heated resin to 100° C. under Nitrogen with stirring. Heated resin to 225° C. and hold at 225° C., When ca.50% of theoretical water was off. Monitored AV and In-Process Viscosity. Maintained at 225° C. until AV<ca. 75. Cooled Resin to <125° C. Added Item 5; Maintained at 125-135° C. for 0.50 Hrs. Increased Temp to 225° C. and Maintained at 225° C.; Applied Vacuum at 436 mm as needed as to decrease AV to final target property. Monitored AV and Visc; Maintained at 225° C. until AV<ca. 155. Cooled Resin to about 150° C.; Filtered and Packaged. The final resin had the following properties: Acid Value (AV) 157, Mn 750, Mw 1500, Mz 2350, Wt. Fraction ≦500 Daltons 18.1%, Wt. Fraction ≦1000 Daltons 41.3%, Viscosity at 25° C. of 22,175 mPa*s.
EXAMPLE 4
Polyester Preparation












Item
Ingredient
Charge (g)

















1
Isophthalic Acid
940.17


2
Diethylene Glycol
572.60


3
Ethylene Glycol
316.00


4
Fascat 9100 (Hydroxybutyltin oxide)
0.3169


5
Adipic Acid
1238.98









Charged Items 1-4 to vessel at Ambient Temperature (25-30° C.). Heated resin to 100° C. under Nitrogen with stirring. Heated resin to 225° C. and hold at 225° C., When ca.50% of theoretical water was off. Monitored AV and In-Process Viscosity. Maintained at 225° C. until AV<ca. 80. Cooled Resin to <125° C. Added Item 5; Maintained at 125-135° C. for 0.50 Hrs. Increased Temp to 225° C. and Maintained at 225° C. Monitored AV and Visc; Maintained at 225° C. until AV<ca. 165. Cooled Resin to about 150° C.; Filtered and Packaged. The final resin had the following properties: Acid Value (AV) 169, Mn 950, Mw 2000, Mz 3250, Wt. Fraction ≦500 Daltons 12.5%, Wt. Fraction ≦1000 Daltons 31.0%, Viscosity at 25° C. of 221,750 mPa*s.
EXAMPLE 5
Polyester Preparation












Item
Ingredient
Charge (g)

















1
Isophthalic Acid
908.62


2
Diethylene Glycol
1126.80


3
Fascat 9100 (Hydroxybutyltin oxide)
0.5730


4
Adipic Acid
1198.87









Charged Items 1-3 to vessel at Ambient Temperature (25-30° C.). Heated resin to 100° C. under Nitrogen with stirring. Heated resin to 225° C. and hold at 225° C., When ca.50% of theoretical water was off. Monitored AV and In-Process Viscosity. Maintained at 225° C. until AV<ca. 75. Cooled Resin to <125° C. Added Item 4; Maintained at 125-135° C. for 0.50 Hrs. Increased Temp to 225° C. and Maintained at 225° C.; Applied Vacuum at 394 mm as needed as to decrease AV to final target property. Monitored AV and Visc; Maintained at 225° C. until AV<ca. 135. Cooled Resin to about 150° C.; Filtered and Packaged. The final resin had the following properties: Acid Value (AV) 158, Mn 1150, Mw 2350, Mz 3750, Wt. Fraction ≦500 Daltons 8.5%, Wt. Fraction ≦1000 Daltons 23.6%, Viscosity at 25° C. of 175,000 mPa*s.
EXAMPLE 6
Polyester Preparation












Item
Ingredient
Charge (g)

















1
Isophthalic Acid
942.70


2
Diethylene Glycol
654.60


3
Ethylene Glycol
362.20


4
Fascat 9100 (Hydroxybutyltin oxide)
0.3168


5
Adipic Acid
1239.19









Charged Items 1-4 to vessel at Ambient Temperature (25-30° C.). Heated resin to 100° C. under Nitrogen with stirring. Heated resin to 225° C. and hold at 225° C., When ca.50% of theoretical water was off. Monitored AV and In-Process Viscosity. Maintained at 225° C. until AV<ca. 80. Cooled Resin to <125° C. Added Item 5; Maintained at 125-135° C. for 0.50 Hrs. Increased Temp to 225° C. and Maintained at 225° C.; Applied Vacuum at 327 mm as needed as to decrease AV to final target property. Monitored AV and Visc; Maintained at 225° C. until AV<ca. 105. Cooled Resin to about 150° C.; Filtered and Packaged. The final resin had the following properties: Acid Value (AV) 98, Mn 1200, Mw 2450, Mz 3900, Wt. Fraction ≦500 Daltons 7.6%, Wt. Fraction ≦1000 Daltons 22.2%, Viscosity at 25° C. of 271,500 mPa*s.
EXAMPLE 7
Polyester Preparation












Item
Ingredient
Charge (g)

















1
Isophthalic Acid
1158.60


2
Diethylene Glycol
720.90


3
Ethylene Glycol
398.30


4
Fascat 9100 (Hydroxybutyltin oxide)
0.4089


5
Adipic Acid
1525.85









Charged Items 1-4 to vessel at Ambient Temperature (25-30° C.). Heated resin to 100° C. under Nitrogen with stirring. Heated resin to 225° C. and hold at 225° C., When ca.50% of theoretical water was off. Monitored AV and In-Process Viscosity. Maintained at 225° C. until AV<ca. 80. Cooled Resin to <125° C. Added Item 5; Maintained at 125-135° C. for 0.50 Hrs. Increased Temp to 225° C. and Maintained at 225° C.; Applied Vacuum at 435 mm as needed as to decrease AV to final target property. Monitored AV and Visc; Maintained at 225° C. until AV<ca. 160. Cooled Resin to about 150° C.; Filtered and Packaged. The final resin had the following properties: Acid Value (AV) 153, Mn 650, Mw 1550, Mz 2650, Wt. Fraction ≦500 Daltons 19.2%, Wt. Fraction ≦1000 Daltons 42.8%, Viscosity at 25° C. of 173,750 mPa*s.
EXAMPLES 8-26
Preparations of Epoxide Terminated Polyester Resins
The preparations in Examples 8-26 were similar. Diepoxide, one or more diacid, and catalyst were charged to the reactor. Slowly Heated to 135-140° C. Maintained at 135-140° C. for ca. 0.50 Hrs and then heated to 150-155° C. and maintained at 150-155° C. for ca. 1.5 to 2 Hrs and then monitored AV and Viscosity. Maintained at 150-155° C. and monitored AV and Visc until AV<1.0. Transferred Resin and Package.









TABLE 1









Example Number:















8
9
10
11
12
13
14


















Ingredient (g)









DER 736
425.36
426.94
600.93
503.22
1593.93
1900.35
1900.42


Isophthalic Acid
92.92
93.00


348.83
333.00
299.80


Adipic Acid


114.00



29.24


Polyester Resin of



373.19


Ex. 1


EthylTriphenyl-
0.2486
0.2575
0.3061
0.3640
0.9532
0.7590
0.4035


phosphonium


Iodide


Properties


EEW
544.71
482.29
472.88
771.14
487.37
416.73
411.51


Acid Value
0.11
≦0.05
≦0.05
≦0.05
0.1
0.09
0.07


Mn
1000
550
1200
1950
1400
1150
1050


Mw
3800
1400
3100
4400
4400
3750
3850


Mz
9600
2850
6350
7600
10500
9500
10350


Wt. Fraction ≦500
16.8
28.8
13.0
4.8
10.1
15.6
17.4


(%)


Wt. Fraction ≦1000
28.0
54.2
24.2
11.1
20.9
27.6
28.9


(%)


Viscosity at 25° C.
18425
16300
3850
30400
18500
5025
6100


(mPa * s)


Viscosity at 70° C.
535.0
467.5
345.0(a)
1665.0(a)
900.0(a)
365.0(a)
430.0(a)


(mPa * s)





(a)Viscosity at 60° C.















TABLE 2









Example Number:














15
16
17
18
19
20

















Ingredient (g)








DER 736
1953.00
1041.90
1002.17
1008.19
784.08
792.79


Isophthalic Acid
427.40


Polyester Resin of Ex. 2



839.04
770.69


Polyester Resin of Ex. 3


753.53


Polyester Resin of Ex. 4

655.66


Polyester Resin of Ex. 5





780.42


EthylTriphenylphosphonium
1.4638
0.5199
0.5067


Iodide


Benzyltrimethylammonium



0.5630


Chloride


Sodium Carbonate




0.5571


Sodium Acetate





0.5346


Properties


EEW
482.29
492.53
598.00
634.90
802.95
694.54


Acid Value
0.04
0.04
0.06
0.05
0.04
0.03


Mn
1600
1500
1550
1550
2100
2000


Mw
5500
4750
4800
4700
13400
10100


Mz
14050
9000
8950
8700
44500
26900


Wt. Fraction ≦500 (%)
7.5
10.9
10.5
10.4
6.9
7.6


Wt. Fraction ≦1000 (%)
20.1
19.2
17.1
17.6
13.2
15.1


Viscosity at 25° C. (mPa * s)
18325
6512
6100
6000
23025
21800


Viscosity at 70° C. (mPa * s)
700.0(a)
320.0
342.5
345.0
1025
890.0





(a)Viscosity at 65° C.















TABLE 3









Example Number:














21
22
23
24
25
26

















Ingredient (g)








DER 736
775.25
763.54
679.89
600.32
1021.77
738.40


Polyester Resin of Ex. 4


520.90


Polyester Resin of Ex. 5
917.33


Polyester Resin of Ex. 6

923.08

1010.75


Polyester Resin of Ex. 7




762.94
918.60


Sodium Acetate
0.5677
0.5467
0.3591
0.5156
0.5338
0.5217


Properties


EEW
847.66
759.98
656.16
1244.17
665.79
1417.64


Acid Value
0.04
<0.1
<0.1
<0.1
<0.1
<0.1


Mn
2150
1700
1400
3200
850
3050


Mw
13250
10000
7600
23450
5550
48200


Mz
39550
31500
23000
82350
17150
248300


Wt. Fraction ≦500 (%)
6.5
9.6
12.0
3.4
19.5
3.6


Wt. Fraction ≦1000 (%)
12.2
15.6
20.4
8.0
28.4
8.3


Viscosity at 25° C.
58125
38550
21875
272500
13275
776667


(mPa * s)


Viscosity at 70° C.
1862
1328
805.0
6150
565.0
15000


(mPa * s)









EXAMPLE 27
Preparation of Amine Curative












Item
Monomer/Intermediate
Charge







1
Unidyme 22
435.94


2
Aminoethylpiperazine
242.56









Charged Item 1 and 2 to reactor, slowly heated to 200° C. Maintained at 200° C. for 2 Hr; monitor water evolution, the final resin is transferred and packaged. The final resin had the following properties: Amine Value of 217.15, Viscosity at 25° C. of 51100 mPa*s.
EXAMPLE 28
Preparation of Amine Curative












Item
Monomer/Intermediate
Charge

















1
Amine Curative of Example 6
200.84


2
POLYPOX P370
70.01









Charged Item 1 and 2 to reactor, slowly heated to 50° C., maintain at 50° C. for 4 Hrs. The resin is transferred and packaged. The final resin had the following properties: Amine Value of 185.58, Viscosity at 25° C. of 10488 mPa*s.
EXAMPLE 29
Preparation of Amine Curative












Item
Monomer/Intermediate
Charge

















1
Epikure 3140
252.23


2
POLYPOX P370
84.35









Charged Item 1 and 2 to reactor, slowly heated to 50° C., maintain at 50° C. for 4 Hrs. The resin is transferred and packaged. The final resin had the following properties: Amine Value of 377.45, Viscosity at 25° C. of 4825 mPa*s.
EXAMPLE 30
Preparation of Amine Curative












Item
Ingredient
Charge (g)







1
Unidyme 22
877.12


2
Aminoethylpiperazine
488.24









Charged Item 1 and 2 to reactor, slowly heated to 200° C. Maintained at 200° C. for 2 Hr; monitor water evolution, the final resin is transferred and packaged. The final resin had the following properties: Amine Value of 238.9, Viscosity at 25° C. of 49000 mPa*s.
EXAMPLE 31
Preparation of Amine Curative












Item
Ingredient
Charge (g)







1
Unidyme 22
810.77


2
Triethylenetetramine (TETA)
488.71









Charged Item 1 and 2 to reactor, slowly heated to 200° C. Maintained at 200° C. for 2 Hr; monitor water evolution, the final resin is transferred and packaged. The final resin had the following properties: Amine Value 169.64, Viscosity at 25° C. 54625 mPa*s.
The adhesion properties of the polyester-polyols and polyols were evaluated with Amine based resins using a series of laminate constructions. These two part adhesive systems were evaluated via a solvent hand casting method and laminator.
The following abbreviations are used to describe test results: as: adhesive split; ftr: film tear; fstr: film stretch; fsl: film sliver; at: adhesive transfer; sec: secondary; zip: zippery bond; pmt: partial metal transfer. Adhesion bond strengths were determined on a 15 mm wide strip of laminate on a Thwing-Albert Tensile Tester (Model QC-3A) with a 50 Newton load cell at a 10.0 cm/min rate.
Examples 32-61 were performed as follows: An epoxy terminated polyester was mixed with a curing agent at the mix ratio shown below, in ethyl acetate at 50% concentration by weight. The solution was coated on a first substrate to yield a dry coating weight of 1.6276 g/m2 (1.0 lb/ream). A second substrate was applied to the dried coating and the resulting laminate was cured at room temperature (approximately 25° C.). The bond strength was examined as a function of curing time and is reported below. The “Mix ratio” is the weight ratio of epoxy resin to curing agent, expressed as 100:X. In the column labeled “laminate structure,” the first substrate is listed, followed by the second substrate.
As an example, in the table below, Example number 32 was a mixture of epoxy resin made in Example 8, mixed with curing agent POLYPDX H015, at a weight ratio of epoxy resin to curing agent of 100:13.8. The bond strength on substrates CoexPP (75SLP)/CoexPP (70SPW) at 7 days was 3.19 Newton for a width of 15 mm, and the failure mode was film tear









TABLE 4









Example Number











32
33
34














Epoxy Resin
8
8
9


from Ex. No.


Curing agent
POLYPOX H015
Epikure 3140
Curing Agent Ex.





27


Mix Ratio
100:13.8
100:17.4
100:45.0











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
3.19, ftr
2.05, ftr
2.26, ftr
2.02, ftr
4.84, ftr
3.83, ftr


(75SLP)/


CoexPP


(70SPW)


CoexPP
1.65, as
1.75, as
1.16, as
2.76, ftr
6.54, ftr
6.00, ftr


(75SLP)/


PE (GF-19)


PET/PE
2.09, as
1.85, as
1.39, as
1.67, as
2.46, as
3.55, as


(GF-19)


Nylon/
1.39, as
1.81, as
1.66, as
1.39, as
6.49, ftr
5.29, ftr


PE (GF-19)


PET-Met/
1.26, as
1.35, as
1.18, as
1.19, as
2.59, ftr
2.90, ftr


PE (GF-19)


OPP-Met/
1.96, as
2.06, as
2.88, as
3.55, ftr
4.16, as
4.58, as


PE (GF-19)


OPP-Met/
1.85, as
2.10, as
2.49, as
2.08, ftr
1.34, as
2.61, ftr


CoexPP


(70SPW)


Backed Foil/
0.50, at,
0.70, at,
0.16, as
0.21, as
1.99, as
0.70, as


Nylon
sec
sec


Backed Foil/
0.69, at,
0.83, at,
0.22, as
0.22, as
2.21, as
2.42, as


PET
sec
sec


(92LBT)


Backed Foil/
1.02, at,
1.07, at,
0.96, as
0.68, as
2.98, as
2.95, as


PE (GF-19)
sec
sec


















TABLE 5









Example Number











35
36
37














Epoxy Resin
9
9
10


from Ex. No.


Curing agent
POLYPOX P370
Curing Agent
Curing Agent




Ex. 28
Ex. 28


Mix Ratio
100:20.0
100:38.5
100:39.2











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
2.22, ftr
2.59, ftr
2.42, ftr
2.76, ftr
2.58, ftr
1.73, ftr


(75SLP)/


CoexPP


(70SPW)


CoexPP
2.66, ftr
2.89, ftr
3.39, ftr
3.23, ftr
4.84, ftr
3.43, ftr


(75SLP)/


PE (GF-19)


PET/PE
2.38, as
2.36, as
2.73, as
2.30, as
1.40, as
2.00, as


(GF-19)


Nylon/
2.81, ftr
3.09, ftr
3.95, ftr
2.98, ftr
2.13, as
2.16, as


PE (GF-19)


PET-Met/
1.17, as
1.85, as
2.46, as
1.90, ftr
1.25, as
1.22, as


PE (GF-19)


OPP-Met/
1.21, as
2.03, as
2.57, as
3.08, as
2.95, as
3.46, as


PE (GF-19)


OPP-Met/
1.14, as
1.21, as
2.47, as
2.32, ftr
1.43, as
1.73, as


CoexPP


(70SPW)


Backed Foil/
0.25, as
0.00, as
0.94, as
0.56, as
0.46, as
0.09, as


Nylon


Backed Foil/
0.15, as
0.00, as
0.97, as
0.36, as
0.28, as
0.16, as


PET (92LBT)


Backed Foil/
0.42, as
0.57, as
2.30, as
2.23, as
0.78, as
1.12, as


PE (GF-19)


















TABLE 6









Example Number











38
39
40














Epoxy Resin
10
11
11


from Ex. No.


Curing agent
Curing Agent
Curing Agent
Curing Agent



Ex. 27
Ex. 28
Ex. 27


Mix Ratio
100:45.9
100:24.1
100:28.2











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
2.45, ftr
1.82, ftr
2.38, as
2.52, ftr
2.37, as
2.11, as


(75SLP)/


CoexPP


(70SPW)


CoexPP
3.11, as
3.29, ftr
2.34, as
2.17, as
2.17, as
2.00, as


(75SLP)/


PE (GF-19)


PET/PE
2.18, as
2.35, as
3.31, as
2.63, as
2.19, as
2.76, as


(GF-19)


Nylon/
1.72, as
2.23, as
2.28, as
2.59, as
3.63, as
2.86, as


PE (GF-19)


PET-Met/
1.37, as
1.30, as
1.59, as
2.29, as
4.40, as
3.82, as


PE (GF-19)


OPP-Met/
2.42, as
3.11, as
2.50, as
3.00, as
2.25, as
3.06, as


PE (GF-19)


OPP-Met/
2.88, as
2.86, as
2.20, as
2.56, as
2.75, as
1.80, as


CoexPP


(70SPW)


Backed Foil/
1.23, as
1.29, as
0.00, as
0.71, as
1.06, as
0.61, as


Nylon


Backed Foil/
0.52, as
1.21, as
1.31, as
0.97, as
1.27, as
1.23, as


PET (92LBT)


Backed Foil/
1.20, as
1.46, as
2.18, as
1.75, as
2.34, as
2.11, as


PE (GF-19)


















TABLE 7









Example Number











41
42
43














Epoxy Resin
13
13
16


from Ex. No.


Curing agent
Epikure 3140
Curing Agent Ex
Curing Agent Ex




27
30


Mix Ratio
100:22.8
100:22.8
100:48.4











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
3.11, ftr
3.59, ftr
1.52, as
2.37, ftr
1.88, ftr
2.27, ftr


(75SLP)/


CoexPP


(70SPW)


CoexPP
2.23, as
2.46, as
1.93, as
1.99, as
3.52, as
2.99, as


(75SLP)/


PE (GF-19)


PET/PE
2.08, as
3.02, as
2.17, as
2.31, as
2.84, as
3.51, as


(GF-19)


Nylon/
1.39, as
1.64, as
1.54, as
1.45, as
4.97, as
1.92, as


PE (GF-19)


PET-Met/
0.38, as
0.40, as
2.12, as
0.25, as
0.87, as
1.33, as


PE (GF-19)


OPP-Met/
0.52, as
0.57, as
0.68, as
0.38, as
1.06, as
1.18, as


PE (GF-19)


OPP-Met/
0.48, as
0.70, as
1.09, as
0.38, as
1.12, as
0.97, as


CoexPP


(70SPW)


Backed Foil/
0.83, as
0.69, as
0.91, as
0.46, as
1.89, as
1.62, as


Nylon


Backed Foil/
0.36, as
0.37, as
0.93, as
0.25, as
1.51, as
1.91, as


PET (92LBT)


Backed Foil/
1.33, as
1.92, as
1.72, as
1.65, as
2.51, as
2.05, as


PE (GF-19)


















TABLE 8









Example Number











44
45
46














Epoxy Resin
16
17
17


from Ex. No.


Curing agent
Curing Agent
Curing Agent
Curing Agent



Ex 31
Ex 30
Ex 31


Mix Ratio
100:34.4
100:39.9
100:28.4











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
1.87, ftr
2.95, ftr
1.93, as
1.05, as
1.70, ftr
1.40, ftr


(75SLP)/


CoexPP


(70SPW)


CoexPP
3.84, ftr
4.03, ftr
1.55, as
0.73, as
1.99, as
2.18, as


(75SLP)/


PE (GF-19)


PET/PE
1.24, as
0.91, as
1.67, as
1.64, as
1.36, as
1.52, as


(GF-19)


Nylon/
1.65, as
1.71, as
1.36, as
1.37, as
0.31, as
1.40, as


PE (GF-19)


PET-Met/
0.43, as
0.33, as
0.97, as
1.17, as
0.40, as
0.61, as


PE (GF-19)


OPP-Met/
0.58, as
0.39, as
0.89, as
0.75, as
0.42, as
0.77, as


PE (GF-19)


OPP-Met/
0.49, as
0.64, as
1.10, as
0.98, as
0.49, as
0.42, as


CoexPP


(70SPW)


Backed Foil/
0.76, as
0.69, as
0.36, as
0.94, as
0.27, as
0.32, as


Nylon


Backed Foil/
0.90, as
0.17, as
0.46, as
0.79, as
0.26, as
0.22, as


PET


(92LBT)


Backed Foil/
1.18, as
1.21, as
1.55, as
1.89, as
0.77, as
1.31, as


PE (GF-19)


















TABLE 9









Example Number











47
48
49














Epoxy Resin
18
18
19


from Ex. No.


Curing agent
Curing Agent
Curing Agent
Curing Agent



Ex 30
Ex 31
Ex 30


Mix Ratio
100:37.6
100:26.7
100:29.7











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
1.42, as
1.03, as
1.79, as
1.77, ftr
1.11, as
1.06, as


(75SLP)/


CoexPP


(70SPW)


CoexPP
0.93, as
1.41, as
1.65, as
2.10, as
1.10, as
1.54, as


(75SLP)/


PE (GF-19)


PET/PE
1.34, as
1.60, as
1.59, as
1.41, as
1.84, as
1.74, as


(GF-19)


Nylon/
0.88, as
1.30, as
1.42, as
1.20, as
2.11, as
1.58, as


PE (GF-19)


PET-Met/
0.94, as
0.50, as
0.48, as
0.43, as
0.69, as
1.08, as


PE (GF-19)


OPP-Met/
0.29, as
0.37, as
0.38, as
0.59, as
0.80, as
0.72, as


PE (GF-19)


OPP-Met/
0.41, as
0.62, as
0.48, as
0.46, as
0.87, as
1.26, as


CoexPP


(70SPW)


Backed Foil/
1.18, as
1.85, as
0.66, as
0.79, as
1.13, as
1.83, as


Nylon


Backed Foil/
0.68, as
1.17, as
0.64, as
0.73, as
0.59, as
1.41, as


PET


(92LBT)


Backed Foil/
0.81, as
0.98, as
1.05, as
0.97, as
1.41, as
2.03, as


PE (GF-19)


















TABLE 10









Example Number











50
51
52














Epoxy Resin
19
15
20


from Ex. No.


Curing agent
Curing Agent
Curing Agent
Curing Agent



Ex 31
Ex 31
Ex 30


Mix Ratio
100:21.1
100:35.2
100:34.3











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
1.10, as
1.23, as
1.65, ftr
2.35, ftr
0.30, as
0.30, as


(75SLP)/


CoexPP


(70SPW)


CoexPP
2.13, ftr
1.54, as
3.09, ftr
2.06, ftr
0.42, as
0.42, as


(75SLP)/


PE (GF-19)


PET/PE
1.39, as
1.37, as
2.31, as
2.28, as
0.37, as
0.37, as


(GF-19)


Nylon/
1.23, as
1.28, as
1.16, as
1.71, as
0.23, as
0.23, as


PE (GF-19)


PET-Met/
0.54, as
0.71, as
0.25, as
0.33, as
0.58, as
0.58, as


PE (GF-19)


OPP-Met/
0.79, as
0.86, as
0.48, as
0.54, as
0.64, as
0.64, as


PE (GF-19)


OPP-Met/
0.76, as
0.79, as
0.47, as
0.57, as
0.35, as
0.35, as


CoexPP


(70SPW)


Backed Foil/
0.90, as
0.81, as
0.63, as
0.60, as
0.76, as
0.76, as


Nylon


Backed Foil/
0.80, as
0.70, as
0.35, as
0.33, as
0.52, as
0.52, as


PET


(92LBT)


Backed Foil/
1.00, as
1.06, as
0.85, as
1.22, as
0.90, as
0.90, as


PE (GF-19)


















TABLE 11









Example Number











53
54
55














Epoxy Resin
20
22
22


from Ex. No.


Curing agent
Curing Agent
Curing Agent
Curing Agent



Ex 31
Ex 30
Ex 31


Mix Ratio
100:24.4
100:31.4
100:22.3











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
0.94, as
2.29, ftr
0.52, as
0.82, as
0.92, as
1.96, fsl


(75SLP)/


CoexPP


(70SPW)


CoexPP
1.25, as
2.57, fsl
0.82, as
1.01, as
1.15, as
1.82, as


(75SLP)/


PE (GF-19)


PET/PE
1.56, as
1.87, as
0.76, as
0.87, as
1.11, as
1.45, as


(GF-19)


Nylon/
1.11, as
1.31, as
0.67, as
0.83, as
0.86, as
1.46, as


PE (GF-19)


PET-Met/
0.29, as
0.29, as
0.72, as
0.62, as
0.28, as
0.35, as


PE (GF-19)


OPP-Met/
0.52, as
0.47, as
0.92, as
0.80, as
0.46, as
0.47, as


PE (GF-19)


OPP-Met/
0.50, as
0.51, as
0.79, as
0.80, as
0.49, as
0.54, as


CoexPP


(70SPW)


Backed Foil/
0.72, as
0.80, as
1.04, as
1.08, as
0.86, as
0.90, as


Nylon


Backed Foil/
0.36, as
0.42, as
1.05, as
1.23, as
0.53, as
0.52, as


PET


(92LBT)


Backed Foil/
0.89, as
0.91, as
0.94, as
0.85, as
0.87, as
1.05, as


PE (GF-19)


















TABLE 12









Example Number











56
57
58














Epoxy Resin
23
23
25


from Ex. No.


Curing agent
Curing Agent
Curing Agent
Curing Agent



Ex 30
Ex 31
Ex 30


Mix Ratio
100:36.3
100:25.9
100:37.6











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
1.26, as
1.14, as
1.09, as
2.06, fsl
0.54, as
0.90, as


(75SLP)/


CoexPP


(70SPW)


CoexPP
1.63, as
1.35, as
1.68, as
3.27, ftr
1.49, as
1.70, as


(75SLP)/


PE (GF-19)


PET/PE
1.60, as
1.41, as
1.25, as
1.77, as
1.19, as
0.72, as


(GF-19)


Nylon/
1.15, as
1.64, as
1.61, as
2.56, as
1.17, as
1.19, as


PE (GF-19)


PET-Met/
0.50, as
0.61, as
0.25, as
0.36, as
0.56, as
0.52, as


PE (GF-19)


OPP-Met/
0.71, as
0.76, as
0.44, as
0.49, as
0.60, as
0.64, as


PE (GF-19)


OPP-Met/
0.73, as
0.85, as
0.43, as
0.51, as
0.69, as
0.51, as


CoexPP


(70SPW)


Backed Foil/
1.42, as
1.14, as
0.67, as
0.79, as
0.83, as
1.14, as


Nylon


Backed Foil/
1.12, as
1.16, as
0.31, as
0.44, as
0.52, as
0.80, as


PET


(92LBT)


Backed Foil/
1.11, as
1.12, as
0.85, as
1.10, as
0.94, as
1.03, as


PE (GF-19)


















TABLE 13









Example Number











59
60
61














Epoxy Resin
25
15
15


from Ex. No.


Curing agent
Curing Agent
PRIAMINE 1071
JEFFAMINE



Ex 31

D400


Mix Ratio
100:26.7
100:40.2
100:23.8











Laminate
Bond Strength (N/15 mm)













Structure
7 Days
14 Days
7 Days
14 Days
7 Days
14 Days





CoexPP
1.46, ftr
2.28, ftr
1.87, ftr
2.91, ftr
1.13, as
0.89, as


(75SLP)/


CoexPP


(70SPW)


CoexPP
1.13, as
1.33, as
2.62, ftr
2.56, ftr
1.36, as
2.07, as


(75SLP)/


PE (GF-19)


PET/PE
1.23, as
1.79, as
0.78, as
1.07, as
1.29, as
1.26, as


(GF-19)


Nylon/
0.83, as
0.30, as
1.45, as
1.49, ftr
1.04, as
0.67, as


PE (GF-19)


PET-Met/
0.25, as
0.00, as
0.23, as
0.00, as
0.00, as
0.17, as


PE (GF-19)


OPP-Met/
0.41, as
0.22, as
0.51, as
0.22, as
0.00, as
0.27, as


PE (GF-19)


OPP-Met/
0.41, as
0.42, as
0.39, as
0.24, as
0.38, as
0.25, as


CoexPP


(70SPW)


Backed Foil/
0.49, as
0.66, as
0.00, as
0.00, as
0.00, as
0.00, as


Nylon


Backed Foil/
0.00, as
0.00, as
0.00, as
0.00, as
0.00, as
0.00, as


PET


(92LBT)


Backed Foil/
0.78, as
0.75, as
0.74, as
0.65, as
0.27, as
0.78, as


PE (GF-19)

## Claims

1. An epoxy terminated polyester having the structure




wherein R1— is




G— is




j is 0 to 5, —R2— is a divalent organic group having the structure




wherein —R4— and —R5— is each independently a divalent organic group, and wherein said p is 0 to 20; wherein —R3— is either —(CH2)q— or




wherein q is 1 to 8;
and wherein —R21— is a divalent alkyl group, and every —R22— is a divalent alkyl group.

2. The polyester of claim 1, wherein said —R21— has 3 carbon atoms and every —R22— has 3 carbon atoms.

3. The polyester of claim 2, wherein at least one —R22— has the structure selected from

4. The polyester of claim 1, wherein said —R4— is either —CH2—CH2— or —CH2—CH2—O—CH2—CH2—.

5. The polyester of claim 1, wherein said —R21— has 5 or fewer carbon atoms, and every said —R22— has 5 or fewer carbon atoms.