CA2282766C - Amine cured foundry binder systems and their uses - Google Patents

Amine cured foundry binder systems and their uses Download PDF

Info

Publication number
CA2282766C
CA2282766C CA002282766A CA2282766A CA2282766C CA 2282766 C CA2282766 C CA 2282766C CA 002282766 A CA002282766 A CA 002282766A CA 2282766 A CA2282766 A CA 2282766A CA 2282766 C CA2282766 C CA 2282766C
Authority
CA
Canada
Prior art keywords
foundry
binder system
weight percent
foundry binder
hydroperoxide
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
CA002282766A
Other languages
French (fr)
Other versions
CA2282766A1 (en
Inventor
James J. Archibald
Matthew S. Sheridan
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Ineos Composites IP LLC
Original Assignee
Ashland Licensing and Intellectual Property LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Ashland Licensing and Intellectual Property LLC filed Critical Ashland Licensing and Intellectual Property LLC
Publication of CA2282766A1 publication Critical patent/CA2282766A1/en
Application granted granted Critical
Publication of CA2282766C publication Critical patent/CA2282766C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22CFOUNDRY MOULDING
    • B22C1/00Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds
    • B22C1/16Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents
    • B22C1/20Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents of organic agents
    • B22C1/22Compositions of refractory mould or core materials; Grain structures thereof; Chemical or physical features in the formation or manufacture of moulds characterised by the use of binding agents; Mixtures of binding agents of organic agents of resins or rosins

Abstract

The subject invention relate to a foundry binder system which cures in the presence of a volatile amine curing catalyst comprising (a) an epoxy resin, (b) an organic polyisocyanate, (c) a reactive unsaturate d acrylic monomer or polymer, and (d) an oxidizing agent. The foundry binders are used for making foundry mixes. The foundry mixes are use d to make foundry shapes which arc used to make metal castings.

Description

AMINE CURED FOUNDRY HINDER SYSTEMS AND THEIR USES
FIELD OF THE INVENTION
The subject invention relates to a foundry binder system which cures in the presence of a volatile amine curing catalyst comprising (a) an epoxy resin,(b) an organic polyisocyanate, (c) a reactive unsaturated acrylic.
monomer or polymer, and (d) an oxidizing agent. The foundry binders are used for making foundry mixes. The foundry mixes are used to make foundry shapes which are used to make metal castings.
BACKGROUND OF THE INVENTION
One of the major processes used in the foundry industry for making metal parts is sand casting. In sand casting, disposable foundry shapes (usually characterized as molds and cores) are made by shaping and curing a foundry mix which is a mixture of sand and an organic or inorganic binder. The binder is used to strengthen the molds and cores.
The two major processes used in sand casting for making molds and cores are the (a) cold-box process and the (b) no-bake process. In the cold-box process, a gaseous curing agent is passes through a compacted shaped mix to produce a cured mold and/or core. In t7e no-bake process, a liquid curing catalyst is mixed with the sand and shaped into a core cr and/or mold.
The major cold-box process is based upon po:yurethane forming binders. See for example U.S. Patents 3,909,579 and 3,676,392. These systems are cured with a gaseous tertiary amine catalyst. The polyurethane-forming binder system usually consists of a phenolic resin component and polyisocyanate component which are mixed with sand prior to compacting and curing to form a foundry mix.

When the two components of the polyurethane-forming binder system are mixed with the sand to form a foundry mix, they may prematurely react prior to curing with the gaseous catalyst. If this reaction occurs, it will reduce the flowability of the foundry mix when it is used for making molds and cores, and the resulting molds and cores will have reduced strengths. This reduced flowability and decrease in strength with time is related to the benchlife of the foundry mix.
Sufficient benchlife of the foundry mix is important to the commercial success of these binders. Benchlife is the time interval between forming the foundry mix and the time when the foundry mix is no longer useful for making acceptable molds and cores. A measure of the usefulness of the foundry mix and the acceptability ef the molds and cores prepared with the foundry mix is the tensile strength of the molds and cores. If a foundry mix is used after the benchlife has expired, the resulting molds and cores will have unacceptable tensile strengths.
Because it is not always possible to use the foundry mix immediately after mixing, it is desirable to prepare foundry mixes with an extended bench life. When polyurethane-forming cold-box binders are used, generally a ccmpound which improves the bencr: life of the foundry mix must be added to the binder, usually the polyisocyanate component of the binder.
A.~nong the compounds useful to extend the bench life of the foundry mix are organic and/cr inorganic phosphorus containing compounds. Examples of organic phosphorus-containing compounds used as benchlife extenders with polyurethane-forming binder systems are disclosed in U.S.
Patent 4,436,881 which discloses certain organic phosphorus containing compounds such as dichloroarylphosphine, chlorodiarylphosphine, arylphosphinic dichloride, or diarylphosphinyl chloride, and U.S. Patent 4,683,252 which discloses organohalophosphates such as mono-phenyldichlorophosphate.
Examples of inorganic phosphorus-containing compounds which extend the bench life of polyurethane-forming binder systems are disclosed in U.S. Patent 4,540,729 which discloses inorganic phosphorus halides such as phosphorus oxychloride, phosphorus trichloride, and phosphorus pentachloride, and U.S. Patent 4,602,069 which discloses inorganic phosphorus acids such as orthophosphoric acid, phosphoric acid, hypophosphoric acid, metaphosphoric acid, pyrophosphoric acid, and poly-phosphoric acid.
Carboxylic acids, such as citric acid, are also used to extend the benchlife of polyurethane-forming foundry binders. See U.S. Patent 4,760,101.
As cap be seen, there are numerous benchlife extenders for polyurethane-forming cold-box binders which reflects the interest in extending the benchlife of the fou:.d=y m:x.
Despite the cited word:, there is still a need for amine-cured binder systems with longer benchlife.
SUMMARY OF THE INVENTION
The invention relates to a foundry binder system which will cure in the presence of a volatile amine curing catalyst comprising:
(a) from ' to RO weigh:. percer.~ of an epoxy resin;
(b) from 5 to 80 weight percent of an o:gan~c polyisocyanate;
(c) from 5 to 75 weight percent of a reactive unsaturated acrylic monomer or polymer; and (d) from 2 to 45 weight percent of an oxidizing agent, where (a), (b), (c), and (d) are separate components or can be mixed with another component, provided (b) or (c) is not mixed with (d), and where said weight percents are based upon the total weight of (a), (b), (c), and (d).
Generally, the weight percent of (a) is 5 to 50, the weight percent of (b) is 5 to 50, the weight percent of-(c) is 5 to 50, and the weight percent of (d) is 5 to 15.
Preferably, the weight percent of (a) is 5 to 40, the weight percent of (b) is 10 to 50, the weight percent of (c) is 10 to 50, and the weight percent of (d) is 5 to 15.
More preferably, the weight percent of (a) is 5 to 90, the weight percent of (b) is 20 to 40, the weight percent of lc) is 15 to 90, and the weight percent of (d) is 5 to 15.
The foundry binders are used for making foundry mixes. The foundry mixes are used to make foundry shapes which are used to make metal castings. The foundry binder systems described herein have considerably longer benchlife than the previously cited phenolic urethane binders. The foundry mixes produce cores and molds with adequate tensile strengths for commercial use. Castings, made with an assembly of cores and/or molds made with the binders, are acceptable for commercial use. Additionally, the binder does not contain any free phenol o~ free formaldehyde, and has zero or low volatile organic compounds (VOC). The binders are not photochemically reactive and the used sand is reclaimable.
BEST MODE AND OTHER MODES OF PRACTICING THE INVENTION
The subject binder must contain an epoxy resin. The weight ratio of epoxy resin to organic polyisocyanate generally is from 1:10 to 10:1, preferably from 1:5 to 5:1, most preferably from 1:2 to 2:1.
For purposes of this disclosure, "epoxy resin" is defined as a thermosetting resin which contains more than one reactive epoxide group per molecule. Such resins have either a mixed aliphatic-aromatic or exclusively non-aromatic (i.e., aliphatic or cycloaliphatic) molecular structure. The mixed aliphatic-aromatic epoxy resins generally are prepared by the well-known reaction of a bis-(hydroxy-aromatic)alkane or a tetrakis-(hydroxy-aromatic)alkane with a halogen-substituted aliphatic.
epoxide in the presence of a base such as, for example, sodium hydroxide or potassium hydroxide. Examples of the halogen-substituted aliphatic epoxides include epichlorohydrin, 9-chloro-1,2-epoxybutane, 5-bromo-1,2 epoxypentane, 6-chloro-1,3-epoxyhexane and the like. In general, it is preferred to use a chloride substitute terminal denoting that the epoxide group is on the end of the alkyl chain.
The most widely used epoxy resins are diglycidyl ethers of bisphenol A. These are made by reaction of epichlorohydrin with bisphenol A in the presence of an alkaline catalyst. By controlling the operating conditions and varying the ratio epichlorohydrin to bisphenol A, products of different molecular weight can be made. Other epoxy resins include (a) the diglycidyl ethers of other bisphenol compounds such as bisphenol B, F, G, and H, (b) epoxy resins produced by reacting a 2.. novolac resin with a halogen-substituted aliphatic epoxide such as epichlorohydrin, ~-ct:loro-i,2-epoxybutane, 5-b.-c.:.o-~, 2-epoxypentane, ~~-chlcro-., :s-epoxyt:exane ar:d thc-ike, (c) epoxid~zed polybutadiene resins, ar:d (.ii epcxidized drying oils.
Particularly preferred are epoxy resins with a weight per epoxy group of 175 to 200. Although the viscosities of the epoxy resins are high, usually greater than 5,000 cps at 25° C, the epoxy component viscosity is reduced to a workable level when the epoxy resin is mixed with the oxidizing agent. Useful epoxy resins are disclosed in U.S.
Patent 4,518,723 which is hereby incorporated by reference into this disclosure.
Oxidizing agents which are used in component (a) include peroxides, hydroperoxides, hydroxy hydroperoxides, ketones, peroxides, peroxy ester oxidizing agents, alkyl oxides, chlorates, perchlorates, chlorites, hydrochlorides, perbenzoates, permanganates, etc. -Preferably, however, the oxidizing agent is a peroxide, hydroperoxide or a mixture of peroxide or hydroperoxide with hydrogen peroxide. The organic peroxides may be aromatic or alkyl peroxides. Examples of useful diacyl peroxides include benzoyl peroxide, lauroyl peroxide and decanoyl peroxide. Examples of alkyl peroxides include dicumyl peroxide and di-t-butyl peroxide. Hydroperoxides particularly preferred in the invention include t-butyl hydroperoxide, cumene hydroperoxide, paramenthane hydroperoxide, etc. Mixtures of one or more of the above organic peroxides or hydroperoxides can be utilized with hydrogen peroxide as curing or hardening agents or accelerators.
Although not necessarily preferred, the epoxy component (a), may contain an aromatic hydrocarbon solvent such as be::zene, toluene, xylene, ethylbenzene, naphthalenes, mixtures thereof, and the like. If a solvent is used, sufficient solvent should be used so that the resulting viscosity of component (a) is less than 1,000 centipoise, preferably less than 300 centipoise.
Generally, however, the total amount of aromatic hydrocarbon solvent is used in an amount of 0 to 25 weight percent based upon the total weight of the epoxy resin.
Although not necessarily preferred, a phenolic resin can be added to the epoxy component (a), preferably a polybenzylic ether phenolic resole resin. Polybenzylic ether phenolic resole resins are well known in the patent literature and are specifically described in U.S. Patent wo 98r~9m9 pcrnrs98ro~raa 3, 485, 797.
They are prepared by reacting an aldehyde and a phenol in a mole ratio of aldehyde to phenol of at least 1:1, generally from 1.1:1.0 to 3.0:1.0 and preferably S from 1.1:1.0 to 2.0:1.0, in the presence of a metal ion catalyst, preferably a divalent metal ion such as zinc, lead, manganese, copper, tin, magnesium, cobalt, calcium, or-barium. If a polybenzylic ether phenolic resin is used, an appropriate solvent may be used with it. Appropriate solvents and their amounts are disclosed in U.S. Paten:
3,985,797 which was mentioned previously.
The organic polyisocyanate component of the binder system comprises an organic polyisocyanate having a functionality of two or more, preferably 2 to 5. It may be aliphatic, cycloaliphatic, aromatic, or a hyb:~c polyisocyanate. Mixtures o° such polyisocyanates may be used.Representative examples of organic polyisocyana~es are a'_iphatic polyisocyanates such as hexa:rethy!ene diisocyanate, alicyclic polyisocyanates such as 4,4'-dicyclohexylmethane diisocyanate, and aromatic polyisocyanates such as 2,9- and 2,6-toluene diisocyanate, diphenylmethane diisocyanate, and dimethyl derivatives thereof. Other examples of suitable organic polyisocyanates are 1,-naphthalene diisocya:~ate, tr~phenylr.ethane ~:iisocyanate, xylylene dizsocyanate, a..~.d the methyl derivatives thereof. polymethylenepolyphenyl isocyanates, chlorophenylene-2,4-diisocyanate, and the like. The organic polyisocyanate is used in a liquid form. Solid or viscous polyisocyanates must be used in the form o: organic solvent solutions, the solvent generally being present in a range of up to 80 percent by weight of the solution.
The acrylic component of the polyisocyanate component (b) is a reactive unsaturated acrylic monomer or polymer or mixtures thereof. Examples of such materials include a wide variety ef monofunctional, difunctional, trifunctional and tetrafunctional acrylates. A
representative listing of these monomers includes alkyl acrylates, hydroxyalkyl acrylates, alkoxyaikyl acrylates, acrylated epoxy resins, cyanoalkyl acrylates, alkyl methacrylates, hydroxyalkyl methacrylates, alkoxyalkyl methacrylates, cyanoalkyl methacrylates, N
alkoxymethylacrylamides, N-alkoxymethylmethacrylamides, and difunctional monomeric acrylates. Other acrylates which can be used include trimethylolpropane triacrylate, methacrylic acid and 2-ethylhexyl methacrylate.
Examples of unsaturated reactive polymers include epoxy acrylate reaction products, polyester/urethane/acrylate reaction products, polyether acrylates, and polyester acrylates. Unsaturated polymers include commercially available materials such as, acrylated urethane oligomers 'rom Thio};ol and CMD 1700, an T\i acrylated ester of an acrylic polymer and CELRAD '701, an acrylated epoxy :esin boat: available fro:. Celanese.
The weight ratio o.' organic polyisocyanate to reaot:ve unsaturated acrylic monomer or polymer generally is from 10:1 to 1:10, preferably from 1:5 to 5:1.
Although so'_vents are not required for the crganic polyisocyanate component, typical solvents which can be used are general'_y these wh:cr have been classified in the art as 2'~ ccupling solvents and include fur:ura'_, fur:uryi alcohol, TM 'I'~1 ~IVf Cellosolve acetate, butyl Cellosolve, butyl Ca=bitcl, Th, diacetone alcohol, and Texanol. Othe.- pola: so:veat~
include l:qu~c? d:all:yl esters suc:~ as diolkyl phthalate of the type disclosed in U.S. Patent 3,905,93 and other dialkyl esters such as dimethyl glutarate. Suitable aromatic solvents are benzene, toluene, xylene, ethylbenzene, and mixtures thereof. Preferred aromatic solvents are mixed solvents that have an aromatic content of at least 90~ and a boiling point range of 138°C to 232°C.
B

Drying oils, for example those disclosed in U.S. Patent 4,268,425, may also be used in the polyisocyanate component.
Drying oils may be synthetic or natural occurring and include glycerides of fatty acids which contain two or more double bonds whereby oxygen on exposure to air can be absorbed to give peroxides which catalyze the polymerization of the unsaturated portions.
The addition of free radical scavengers or inhibitors such as benzoquinone is useful in improving the benchlife of foundry mixes made with the binder system. Benzoquinone acts as an free radical inhibitor/scavenger to inhibit the premature cure of the foundry binder system. Representative examples of inhibitors/retarders include but is not limited to 9-methoxyphenol, hydroq;~i.~.one, t-butylcatechol , pyrogallol, nitrobenzene, x,3,5 trinitrobenzene, chloranil, aniline, phenol, etc. The amount of benzoquinone used is generally from 0 to 3 weight percent, preferably 0 to weight percent based upon the total weight of the binder.
The benzoquinone may be incorporated into either the epoxy component (a) or the polyisocyanate component (b), or both.
Various types of aggregate and amounts of binder are used to prepare foundry mixes by methods well known in the art. Ordinary shapes, shapes for precision casting, and refractory shapes can be prepared by using the binder 2_'. systems and proper aggregate. The amount of binder and the type of aggregate used is known to those skilled in the art.
The preferred aggregate employed for preparing foundry r;,ixes is sand wherein a: leas abcut 7C weigr.:. percent, anc preferably at least about 85 weigrt percent, of the sand is 3C silica. Other sui:.able aggregate materials for ordinary foundry shapes include zircon, olivine, aluminosilicate, chromite sands, and the like.
In ordinary sand type foundry applications, the amount of binder is generally no greater than about loo by weight 35 and frequently within the range of about 0.5o to about 7$ by WO 98139119 PCTlUS98/03644 weight based upon the weight of the aggregate. Most often, the binder content for ordinary sand foundry shapes ranges from about 0.6~ to about 5~ by weight based upon the weight of the aggregate in ordinary sand-type foundry shapes.
Although the aggregate employed is preferably dry, small amounts of moisture, generally up to about 1 weight percent based on the weight of the sand, can be tolerated.
This is particularly true if the solvent employed is non-water-miscible or if an excess of the polyisocyanate necessary for curing is employed since such excess polyisocyanate will react with the water.
It wil? be apparent to those skilled in the art that other additives such as silanes, silicones, bench life extenders, release agents, defoamers, wetting agents, etc.
can be added to the aggregate, or foundry mix. The particular additives chosen will depend upon the specific purposes of the formulator.
The foundry mix is molded into the desired shape and whereupon it is cured by the cold-box process. Curing by the cold-box process is carried out by contacting the foundry shape with a gaseous tertiary amine as described in U.S. Patent 3, 409, 579.
Examples of volatile tertiary amines which can be used include trimethylamine, demethylethylamine. methyldiethylamine, triethylamine, and dimethylethanolamine, and the like.
EXAMPLES
The examples will illustrate specific embodiments of the invention. These examples along with the written description will enable one skilled in the art to practice the invention. It is contemplated that many other embodiments of the invention will be operable besides these specifically disclosed. All parts are by weight and all temperatures are in °C unless otherwise specified. The 1 C;

examples set forth describe various embodiments of the invention, but they are not intended to imply that other embodiments will not work effectively.
The following abbreviations are used in the Examples:

ABBREVIATIONS AND DEFINITIONS
TM
T~, Epoxy resin DER 331 - epoxy resin DER 331, the epoxy resin used in the examples which is prepared by and sold commercially by Dow Chemical.

CHP - cumene hydroperoxide.
DMEA - N,N-dimethylethylamine gas as catalyst.
I50CURE~ 305/605 binder - a polyurethane cold-box binder cured with DMEA, sold by Ashland Chemical Company.
n, Mondur MR - organic polyisocyanate sold by Bayer AG.
TM.PTA - :.rimethylolpropane triacrylate.
In order to carry out the examples, the Part I was firs mixed with sand and then the Part II was added. The polyisocyanate component used in the examples was a TM
polymethylene polyphenyl isocyanate (MONDUR MR sold by BAYER
AG;.
The resulting foundry mixes were compacted ~ntc a dogbone shaped core box by blowing and were cured using the cold-box process as described in U.~. Patent 3,909,579. In this instance, the compacted mixes were then contacted with a r"ixture of N,N-dimethylethylamire (DMEA? gas in nitrogen 3~ at 20 psi for 3.0 seconds, followed by purging wit~ 60 psi nitrogen for about 6 seconds, thereby forming AFS tensile test specimens (dog bones! using the standard AFS procedure.
Measuring the tensile strength of the dog bone shapes enables one to predict how the mixture of sand and binder will work in actual foundry operations. Lower tensile strengths for the shapes after extended benchlife indicate that the binder components reacted more extensively after mixing with the sand prior to curing with amine gas.
In the examples which follow, dog bone samples were formed from the foundry mix immediately after mixing (zero bench), three hours after mixing (three hour benchlife), five hours after mixing (five hour benchlife), and 24 hours after mixing (24 hour benchlife). Then tensile-strengths of the various cured samples were measured immediately (IMM) and 24 hours after curing. Some of the (U dog bone samples that were formed from freshly prepared (zero bench) foundry mixes were stored for 24 hours at a relative humidity (RH) of 90~ and a temperature of 25°C
before measurement of the tensile strength. The test conditions are set forth in Table I. The components used in examples 1-2 are specified ~n Table IT_, and the tensile strengths of the dog bone samples prepared with tt~e formulations of examples ?-2 are given in the Table TII.
TAHLE I
TEST CONDITIONS
2 0 Sand: 4000 g Manley ILSW at about 25°C
CT' Room: 50g, Relative Humidity, 25°C
Sand Lab: 33~ Relative Humidity, 22°C
Part A/Part B weight ratio: 37/63 Binder level (bos): 1.75~t.
2 5 Catalyst: DMEA
Gas time (seconds): 3.0 Purge time (seconds): 7.0 (Ambient Airt TABLE II

EXAMPLE DER CHP MONDUR TMPTA

1 75.7 29.3 62.8 37.2 2 89.0 16.0 60.C 30.0' ' CT = constant temperature room.
2 Formulation 2 also contained 10% by weighs of an acrylic ester of bisphenol A epoxy in the Part II component of the binder.

TABLE III
(TENSILE STRENGTH IN PSI) BENCHLIFE HR HR
BENCHLIFE BENCHLIFE

IMM 24 29 HR @ 90$ IMM 24 IMM 24 HR RH HR HR

Example 1 and 2 are the same except the levels of the components were varied in the Part A and Part B. Examples 1-2 illustrate that the subject binders can be used for at least 29 hours to make dogbones samples with adequate tensile strengths without the use of a benchlife extender.
A comparison test was conducted to compare the benchlife of a binder within the scope of this invention to ISOCURECh% LF 305/605 binder, a commercial phenolic urethane binder available from Ashland Chemical Company which contains an organophosphorous compound as a benchlife extender. The test conditions are the same as given in Table I except benzoq:Iinone has been added in formulation 4 to increase bench life even further. The formulations and results are shown in Table IV.
TABLE IV
(TENSILE STRENGTH IN PSI) !1 B HR 4 HR

BENCHLIFE HENCNLIF

DFR CHf BZQ M~~lDUf :'KPTA

I 2 4 I ~ 4 tit Hk I~".HR

EXAt~LE3 MR

3 75.5 29.5 0.0 49.8 50.2 96 171 44 75 4 75.5 29.3 0.2 49.8 50.2 122 210 90 123 The results in Table IV indicate that the foundry mixes prepared with the binders of Examples 3 and 9 have much better benchlife than the ISOCURE binder, and that

Claims (26)

Claims:
1. A foundry binder system consisting essentially of: (a) from 5 to 80 weight percent of an epoxy resin; (b) from 5 to 80 weight percent of an organic polyisocyanate; (c) from to 75 weight percent of a reactive unsaturated acrylic monomer or polymer; and (d) an effective amount of an oxidizing agent comprising a hydroperoxide, where (a), (b), (c), and (d) are separate components or mixed with another of said components, provided (b) or (c) is not mixed with (d), where said weight percents are based upon the total weight of (a), (b), (c), and (d),and where said binder cures by a cold- box process in the presence of a volatile aliphatic amine curing catalyst.
2. The foundry binder system of claim 1 wherein the weight percent of (a) is 20 to 40, the weight percent of (b) is 20 to 40, the weight percent of (c) is 15 to 40, and the weight percent of (d) is 5 to 15.
3. The foundry binder system of claim 2 wherein the weight ratio of organic polyisocyanate to reactive unsaturated acrylic monomer or polymer is from 1:5 to 5:1.
4. The foundry binder system of claim 3 wherein the reactive unsaturated acrylic monomer or polymer is a monomer and the monomer is trimethylolpropane triacrylate.
5. The foundry binder system of claim 4 wherein the oxidizing agent is a mixture of a hydroperoxide, and an oxidizing agent selected from the group consisting of peroxides, ketone peroxides, and mixtures thereof.
6. The foundry binder system of claim 5 wherein the epoxy resin is selected from the group consisting of epoxy resins formed from a diglycidyl ether of bisphenol A, bisphenol F, epoxy novolak resins and mixtures thereof, and said hydroperoxide is cumene hydroperoxide.
7. The foundry binder system of claim 6 wherein the epoxy resin component also contains a free radical scavenger.
8. The foundry binder system of claim 7 wherein the free radical scavenger is benzoquinone.
9. The foundry binder system of claim 8 wherein the weight ratio of organic polyisocyanate to reactive unsaturated acrylic monomer or polymer is from 1:2 to 2:1.
10. A foundry mix comprising: (a) a major amount of foundry aggregate; and (b) an effective bonding amount of the foundry binder system of claim 2, 3, 4, 5, 6, 7, 8, or 9.
11. The foundry binder system of claim 6 wherein said foundry binder system also includes a polybenzylic ether phenolic resole resin, provided said polybenzylic ether phenolic resole resin is not mixed with component (b).
12. A cold-box process for preparing a foundry shape comprising:
A. preparing a foundry mix comprising a major amount of a foundry aggregate and an effective bonding amount of a foundry binder comprising:
(1) from 5 to 80 weight percent of an epoxy resin;
(2) from 5 to 80 weight percent of an organic polyisocyanate;
(3) from 5 to 75 weight percent of a reactive acrylic selected from the group consisting of reactive unsaturated acrylic monomers, reactive unsaturated acrylic polymers, and mixtures thereof; and (4) an effective oxidizing amount of an oxidizing agent comprising a hydroperoxide, where (1), (2), (3), and (4) are separate components or are mixed with another of said components, provided (2) or (3) is not mixed with (4), and where said weight percents are based upon the total weight of (1), (2) , (3), and (4);
B. introducing the foundry mix obtained from step (a) into a pattern to form an uncured foundry shape;
C. curing the uncured foundry shape obtained by step B with a volatile amine curing catalyst to become self-supporting.
13. The process of claim 12 wherein the reactive unsaturated acrylic monomer is trimethylolpropane triacrylate.
14. The process of claim 13 wherein the oxidizing agent is a mixture of a hydroperoxide, and an oxidizing agent selected from the group consisting of peroxides, ketone peroxides, and mixtures thereof.
15. The process of claim 14 wherein the epoxy resin is selected from the group consisting of epoxy resins formed from a diglycidyl ether of bisphenol A, bisphenol F, epoxy novolak resins and mixtures thereof, and the oxidizing agent is cumene hydroperoxide.
16. The process of claim 15 wherein the epoxy resin component also contains a free radical scavenger.
17. The process of claim 16 wherein the free radical scavenger is benzoquinone.
18. The process of claim 12 wherein the organic polyisocyanate and unsaturated acrylic monomer or polymer are one component and the weight ratio of organic polyisocyanate to reactive unsaturated acrylic monomer or polymer is from 1:5 to 5:1.
19. A process of casting a metal article comprising:

a. fabricating a shape in accordance with claim 12;
b. pouring said metal while in the liquid state into said shape;
c. allowing said metal to cool and solidify; and d. then separating the molded article
20. A foundry binder system comprising:
(a) from 20 to 40 weight percent of an epoxy resin;
(b) from 20 to 40 weight percent of an organic polyisocyanate;
(c) from 15 to 40 weight percent of a reactive unsaturated acrylic monomer or polymer; and (d) an effective oxidizing amount of a hydroperoxide, where (a), (b), (c) , and (d) are separate components or are mixed with another of said components, provided (b) or (c) is not mixed with (d), where said weight percents are based upon the total weight of (a), (b), (c), and (d), and said binder cures by a cold-box process in the presence of a volatile aliphatic amine curing catalyst.
21. The foundry binder system of claim 20 wherein said hydroperoxide is used in an amount of from 5 to 15 weight percent based upon the total amount of (a), (b), (c), and (d).
22. The foundry binder system of claim 21 wherein the reactive unsaturated acrylic monomer is trimethylolpropane triacrylate.
23. The foundry binder system of claim 22 wherein said hydroperoxide is combined with an oxidizing agent selected from the group consisting of peroxides, ketone peroxides and mixtures thereof.
24. The foundry binder system of claim 23 wherein the epoxy resin is selected from the group consisting of epoxy resins formed from a diglycidyl ether of bisphenol A, bisphenol F, epoxy novolak resins and mixtures thereof, and the oxidizing agent is cumene hydroperoxide.
25. The foundry binder system of claim 24 wherein the epoxy resin component also contains a free radical scavenger.
26. The foundry binder system of claim 25 wherein the free radical scavenger is benzoquinone.
CA002282766A 1997-03-04 1998-02-25 Amine cured foundry binder systems and their uses Expired - Fee Related CA2282766C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US08/811,395 US5880175A (en) 1997-03-04 1997-03-04 Amine cured foundry binder system and their uses
US08/811,395 1997-03-04
PCT/US1998/003644 WO1998039119A1 (en) 1997-03-04 1998-02-25 Amine cured foundry binder systems and their uses

Publications (2)

Publication Number Publication Date
CA2282766A1 CA2282766A1 (en) 1998-09-11
CA2282766C true CA2282766C (en) 2007-01-02

Family

ID=25206422

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002282766A Expired - Fee Related CA2282766C (en) 1997-03-04 1998-02-25 Amine cured foundry binder systems and their uses

Country Status (7)

Country Link
US (3) US5880175A (en)
EP (1) EP0973622A4 (en)
JP (1) JP3334093B2 (en)
AU (1) AU719259B2 (en)
BR (1) BR9807809A (en)
CA (1) CA2282766C (en)
WO (1) WO1998039119A1 (en)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5880175A (en) * 1997-03-04 1999-03-09 Ashland Inc. Amine cured foundry binder system and their uses
DE19738755C2 (en) * 1997-09-04 2002-01-17 Ashland Suedchemie Kernfest Phenolic resin and binder for the production of molds and cores using the phenolic resin-polyurethane process
ZA995240B (en) * 1998-09-02 2000-02-21 Ashland Inc Amine cured foundry binder systems and their uses.
AU6617600A (en) * 1999-08-19 2001-03-19 Ashland Inc. Amine curable foundry binder containing an ester of certain organic acids
US6342543B1 (en) * 1999-09-24 2002-01-29 Ashland Inc. Amine curable foundry binder system
US6429236B1 (en) * 2000-05-23 2002-08-06 Ashland Inc. Acrylic-modified phenolic-urethane foundry binders
DE10085198D2 (en) 2000-09-25 2003-08-21 Generis Gmbh Process for producing a component using deposition technology
WO2002066560A1 (en) * 2001-02-16 2002-08-29 Ashland Inc. Foundry binder systems containing an alkyl resorcinol and their use
DE10150564B4 (en) * 2001-10-15 2005-08-04 Intermet Neunkirchen Gmbh Method for binding pollutants
TW200306324A (en) * 2002-04-22 2003-11-16 Tokyo Ind Co Ltd Novolak resin solution, positive photoresist composition, and method of producing same
US20040051078A1 (en) * 2002-09-12 2004-03-18 Gernon Michael David Reactive amine catalysts for use in PUCB foundry binder
US7019047B2 (en) * 2003-07-25 2006-03-28 Ashland Licensing And Intellectual Property Llc Acrylate-free binders containing an epoxy resin and an alkyl silicate
US20050186258A1 (en) * 2004-02-20 2005-08-25 Shiping Wang Antimicrobial medical gloves
DE102006038858A1 (en) 2006-08-20 2008-02-21 Voxeljet Technology Gmbh Self-hardening material and method for layering models
US10426578B2 (en) 2006-10-16 2019-10-01 Natural Dental Implants, Ag Customized dental prosthesis for periodontal or osseointegration and related systems
US8366914B2 (en) * 2007-10-15 2013-02-05 Baker Hughes Incorporated Multifunctional scavenger for hydrocarbon fluids
DE102010006939A1 (en) 2010-02-04 2011-08-04 Voxeljet Technology GmbH, 86167 Device for producing three-dimensional models
DE102010056346A1 (en) 2010-12-29 2012-07-05 Technische Universität München Method for the layered construction of models
CN106424536B (en) * 2016-10-12 2018-07-27 山东科技大学 Novel triethylamine cold box process casting binder without dissociate aldehyde, free phenol
DE102017106686A1 (en) 2017-03-28 2018-10-04 Ask Chemicals Gmbh Molding compound containing additives to reduce casting defects
DE102018117651A1 (en) 2018-07-20 2020-01-23 Ask Chemicals Gmbh Sizing composition for casting molds for metal casting, their use and the casting composition provided with the sizing composition
US11225542B1 (en) * 2018-11-09 2022-01-18 ASK Chemicals LLC Erosion resistant foundry shapes prepared with an epoxy-acrylate cold-box binder
CN113438992A (en) * 2018-12-18 2021-09-24 隆萨解决方案股份公司 Isocyanate-free adhesives

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3485797A (en) * 1966-03-14 1969-12-23 Ashland Oil Inc Phenolic resins containing benzylic ether linkages and unsubstituted para positions
US3676392A (en) * 1971-01-26 1972-07-11 Ashland Oil Inc Resin compositions
CA1050726A (en) * 1973-04-14 1979-03-20 Ciba-Geigy Ag Method of making a foundry mould or core with an anaerobically cured adhesive
US4051092A (en) * 1975-11-13 1977-09-27 International Minerals & Chemical Corporation Foundry core composition of aggregate and a binder therefor
US4163815A (en) * 1977-09-19 1979-08-07 Ford Motor Company Catalyzed polyisocyanate coating compositions
GB2011432A (en) * 1977-11-17 1979-07-11 Ici Ltd Foundry Mixes, Foundry Products Obtained Therefrom, a Process for the Manufacture of the Foundry Products and Binder Compositions Used in Preparing the Mixes
PL124275B1 (en) * 1979-10-10 1983-01-31 Univ M Curie Sklodowskiej Method of manufacture of cured epoxy-acrylic resins
SE448833B (en) * 1980-01-07 1987-03-23 Ashland Oil Inc PROCEDURE FOR THE FORMATION OF CASTLE CORN OR FORMS USING A BINDING MATERIAL HARDENABLE BY FRERADICAL POLYMERIZATION
US4526219A (en) * 1980-01-07 1985-07-02 Ashland Oil, Inc. Process of forming foundry cores and molds utilizing binder curable by free radical polymerization
US4518723A (en) * 1982-08-05 1985-05-21 Cl Industries, Inc. Curable epoxy resin compositions and use in preparing formed, shaped, filled bodies
DE3305361A1 (en) * 1983-02-17 1984-08-23 Röhm GmbH, 6100 Darmstadt BINDING AGENT FOR FOUNDRY SAND
US5286765A (en) * 1989-09-15 1994-02-15 Bayer Aktiengesellschaft Process for the preparation of foundry cores and molds
US4974659A (en) * 1989-10-02 1990-12-04 Ashland Oil, Inc. Cold box process for preparing foundry shapes which use acrylated epoxy resins
US5169910A (en) * 1990-08-08 1992-12-08 Shell Oil Company Epoxy resin composition
IT1255279B (en) * 1992-05-20 1995-10-26 Sir Ind Spa RETICULABLE POLYESTER / ISOCYANATE COMPOSITIONS SUITABLE FOR THE PREPARATION OF COMPOSITE MANUFACTURED PARTICULARLY WITH INJECTION PROCESSES, PROCEDURE FOR THEIR PREPARATION AND USE
US5554692A (en) * 1994-01-06 1996-09-10 Ferro Corporation Blocked isocyanate crosslinkers based on pentaerythritol for use in thermosetting coatings
DE4416323A1 (en) * 1994-05-09 1995-11-16 Bayer Ag Thermosetting reactive resin mixtures and their use
US5733952A (en) * 1995-10-18 1998-03-31 Borden Chemical, Inc. Foundry binder of phenolic resole resin, polyisocyanate and epoxy resin
US5880175A (en) * 1997-03-04 1999-03-09 Ashland Inc. Amine cured foundry binder system and their uses

Also Published As

Publication number Publication date
WO1998039119A1 (en) 1998-09-11
BR9807809A (en) 2000-02-22
EP0973622A4 (en) 2010-01-06
AU6185498A (en) 1998-09-22
JP2000516859A (en) 2000-12-19
US6271284B1 (en) 2001-08-07
JP3334093B2 (en) 2002-10-15
US6037389A (en) 2000-03-14
US5880175A (en) 1999-03-09
CA2282766A1 (en) 1998-09-11
EP0973622A1 (en) 2000-01-26
AU719259B2 (en) 2000-05-04

Similar Documents

Publication Publication Date Title
CA2282766C (en) Amine cured foundry binder systems and their uses
AU678506B2 (en) Polyurethane-forming binder systems containing 2,2'-dipyridyl, 1,10-phenanthroline, and their substituted alkyl derivatives
AU743298B2 (en) Foundry binder of epoxy resin, acrylated polyisocyanate and acrylic monomer and/or polymer; and cold-box process
US4852629A (en) Cold-box process for forming foundry shapes which utilizes certain carboxylic acids as bench life extenders
EP0323962A1 (en) Polyurethane-forming binder compositions containing certain carboxylic acids as bench life extenders
AU729059B2 (en) Foundry binder systems which contain alcohol modified polyisocyanates
US5880174A (en) Amine modified polyisocyanates and their use in foundry binder systems
US6342543B1 (en) Amine curable foundry binder system
US6429236B1 (en) Acrylic-modified phenolic-urethane foundry binders
US6124375A (en) Foundry binder systems which contain alcohol modified polyisocyanates
US5338774A (en) Polyurethane-forming binder systems containing a polyphosphoryl chloride
CA2506017A1 (en) Phenolic urethane foundry binder
MXPA01002310A (en) Foundry binder of epoxy resin, acrylated polyisocyanate and acrylic monomer and/or polymer;and cold-box process
CA2165080C (en) Polyurethane-forming binder systems containing 2,2'-dipyridyl, 1,10-phenanthroline, and their substituted alkyl derivatives
WO1988003541A1 (en) Polyurethane-forming binder compositions containing certain phosphonic dihalides as bench life extenders
MXPA99004310A (en) Foundry binder systems which contain alcohol modified polyisocyanates

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed

Effective date: 20170227