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Patent 2175574 Summary

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(12) Patent Application: (11) CA 2175574
(54) English Title: ANTICORROSION ADHESIVE COMPOSITION AND METHOD
(54) French Title: COMPOSITION ADHESIVE ANTICORROSION ET PROCEDE DE LIAISON
Status: Dead
Bibliographic Data
(51) International Patent Classification (IPC):
  • C09J 163/00 (2006.01)
  • C09J 11/04 (2006.01)
  • C23F 11/18 (2006.01)
(72) Inventors :
  • LAMON, ALAIN H. (France)
(73) Owners :
  • MINNESOTA MINING AND MANUFACTURING COMPANY (United States of America)
(71) Applicants :
(74) Agent: SMART & BIGGAR
(74) Associate agent:
(45) Issued:
(86) PCT Filing Date: 1994-11-04
(87) Open to Public Inspection: 1995-05-11
Availability of licence: N/A
(25) Language of filing: English

Patent Cooperation Treaty (PCT): Yes
(86) PCT Filing Number: PCT/US1994/012734
(87) International Publication Number: WO1995/012647
(85) National Entry: 1996-04-01

(30) Application Priority Data:
Application No. Country/Territory Date
08/147560 United States of America 1993-11-05

Abstracts

English Abstract


An adhesive composition comprising particles of an inorganic oxide of silica or alumina having cations bound thereto, which particles
inhibit or prevent corrosion of metal when the cured adhesive composition is in contact therewith. A method of bonding is also described


French Abstract

L'invention concerne une composition adhésive comprenant des particules d'un oxyde inorganique de silice ou d'alumine des cations. Ces particules inhibent ou empêchent la corrosion du métal lorsque la composition adhésive durcie se trouve en contact avec ledit métal concerné. L'invention concerne par ailleurs un procédé de liaison.

Claims

Note: Claims are shown in the official language in which they were submitted.


WHAT IS CLAIMED IS:
1. A curable, structural epoxy adhesive composition comprising:
(a) an epoxy resin having an average epoxide functionality of greater
than one;
(b) a base curing agent in an amount sufficient to cure the epoxy
resin through reaction of a nucleophilic or electrophilic group contained
in the base curing agent with the epoxy ring contained in the epoxy
resin;
(c) particles comprising an inorganic oxide of silica or alumina
having cations bound thereto, the particles being of a type which and
present in an amount effective to inhibit or prevent corrosion of metal to
which the epoxy adhesive composition has been applied.
2. A composition according to Claim 1, wherein the cation is selected
from the group consisting of Ca2+, Zn2+, Co2+, Pb2+, Sr2+, Li+, Ba2+ and
Mg2+.
3. A composition according to Claim 1, wherein the cation is selected
from the group consisting of Ca2+ and Zn2+.
4. A composition according to Claim 1, wherein the particles comprise
a calcium ion-exchanged amorphous silica gel.
5. A composition according to Claim 1, further comprising a
toughening agent having an epoxide compatible component substantially soluble
in the epoxy resin and an epoxide incompatible component substantially
insoluble in the epoxy resin.
6. A composition according to Claim 1, further comprising an
accelerator to increase the cure rate of the epoxy adhesive composition.
-27-

7. A method for inhibiting or preventing corrosion of a metal substrate
which has been bonded to another substrate, the method comprising including
particles comprising an inorganic oxide of silica or alumina having cations
bound thereto in the adhesive composition being employed to bond the metal
substrate to the other substrate, the particles being of a type which and present
in the adhesive , in an amount effective to inhibit or prevent
corrosion of the metal substrate in the area thereof which is in contact with the
adhesive composition.
8. A method according to Claim 7, wherein the other substrate is also
metal.




-28-

Description

Note: Descriptions are shown in the official language in which they were submitted.


W09S1126.17 21 7~74 PCT/US9~11273~
Ant~corroslon adhes~Ye compos~t~on and method
FJFT n OF TE~ ~VEI`lTION
This invention relates to adhesives containing an agent to resist corrosion
S on metal surfaces.
BACKGROUI~D OF T~TF. I~VF.l~lTION
Corrosion resistant treatments for metals are well known in the art and
play an important role in l,, the bond between a coating, such as
10 paint, or an adhesive to the metal over long periods of time, especially in
corrosive ~I.vil~ The most commonly ~ corrosive
CIIV;I~ ' include exposure to salt water from oceans, road treatments for
ice containing corrosive chemicals and/or salt, acid rain, and the like.
There are methods of treating metal surfaces before applying paints and
15 adhesives to protect the metal surface from corrosion. The methods generally
involve a conversion coating in which a protective oxide is formed on the metal
surface, or an etching process to form a protective oxide. The etching process
may further include processes of anodizing and/or priming.
One well known method of preparing aluminum is referred to as an
20 "FPL _tch" which has been used in the aerospace industry since the early
1950's. Tbe FPL etch process includes the steps of optionally degreasing the
aluminum part with solvent, degreasing with an alkaline solution at 180F,
immersing the part in an aqueous solution of sulfuric acid and sodium
di~lu~ at 160F, rinsing, and drying the part at room i , and
25 elevated ~I~ ldlUlC. Although the process has been useful, there are
.,vil~ ' and health concerns in using chromates and corrosive acids.
Conversion coatings known in the art include phosphate conversion
coatings, chromate conversion coatings, and cobalt conversion coatings.
Other methods of improving corrosion resistdnce include adding a
30 corrosion inhibitor to adhesives. Inhibitors currently used include chromate
salts, such as barium chro~ate, stro~tium chromate, l~.-g~ ~ . chromate, etc.

WO 95112647 2~ P~ 7 ~ PCTNS91/1273
Certain cations, such as zinc and calcium, have been used as corrosion
inhibitors in protective coatings such as paints. The cations are typically usedin the form of spanngly water soluble salts.
Shieldex'U anti-corrosion pigment is an io.. CAC.II~lLlgC~i silica said to be
5 useful in paints and coatings.
SUMMARY OF THE INVENTION
The present invention provides a curable, structural epoxy adhesive
c ~ , "~,,
(a) an epoxy resin having an average epoxide functionality of greater
than one;
(b) a base curing agent in an amount sufficient to cure the epoxy
resin through reaction of a, ~ 1 ..l.l.;li- or electrophilic group contained
in the base curing agent with the epoxy ring contained in the epoxy
resin;
(c) particles comprising an inorganic oxide of silica or alumina
having cations bound thereto, the particles being of a type which and
present in an amount effective to inhibit or prevent corrosion of metal to
which the epoxy adhesive ~ has been applied.
The present invention further provides a method for inhibiting or
preventing corrosion of a metal substrate which has been bonded to another
substrate, the method comprising including particles ~c~pn~in~ am inorgamic
oxide of silica or alumina having cations bound thereto in the adhesive
being employed to bond the metal substrate to the other substrate,
25 the particles being of a type which and present in the adhesive cu~ o~ , in
an amount effective to inhibit or prevent corrosion of the metal substrate in the
area thereof which is in contact with the adhesive
DF-~CRIPTION OF TT~F. INVENTION
The present invention provides epoxy adhesive ~ ;r ~ c that are
useful as structural adhesives that provide corrosion resistance to the substr2te
-2-

WO 95/12647 2 1 ~7~; 7~ PCI/I~S94/1273J
from salt solutions. The adhesives are y~ULi~;ulAlly useful for metal substratessuch as aluminum and steel and the preferred v,~ do not contain
hl.' heavy metal elements such as chromium.
Structural adhesives form strong integral bonds between substrates.
S Bonds formed with structural adhesives have a room t~ u.c bond strength,
as measured by a test well known in the industry, referred to as a T-peel test,
of at least 10 pounds per lineal inch (pli) on a bond line thickness of 0.010 inch
(0.2~imm). The upper limit on the structural bond strength would be the
cohesive failure of the substrate or yielding of the substrate. The adhesive
10 . , -- - of the present invention form room t~ Lu,c; T-peel bond
strengths on a bond line thickness of 0.010 inch (.254 mm) of at least 12 pli,
with preferred ~ ;"Ac having bond strengths greater than about 14 pli,
and the most preferred ~ having bond strength greater than 17 pli.
Structural adhesive bonds can also be ~ I by a room
15 t ~ modulus, as measured by a test known in the industry as the
overlap shear test, of at least 3 megaPascals (MtPa). The upper limit of the
overlap shear strength would be the cohesive failure of the substrate, or
yielding of the substrate. The adhesive of the invention form
bonds with overlap shear strengths at room i , c of at least S MPa, with
20 preferred , forming overlap shear strength bonds of at least 7 mPa,
and with the more preferred r~ ; forming overlap shear strength bonds
of at least 10 MPa, and with the most preferred r~ forming overlap
shear strength bonds of at least 14 MPa.
Structural bonds typically have a thickness grcater than 2 mils (0.5 mm).
25 In the practice of the invention, bond lines formed are typically greater than S
mils (0.127 mm).
Epoxides that are useful in the adhesive ~. ~ of the present
invention can be any organic compound having at least one epoxy ring that is
pol~..._.i~11~ by ring opening. Preferred are organic ~ , having an
30 average epoxy fimAtion~ y greater than one, and preferably at least two. The
epoxides can be ~ or polymeric, and aliphatic, ~J~
-3 -

W095/126~7 2~5~74 `` PCT/US9-1/12734 --
uuy~ , aromatic or mixtures thereof. The more preferred epoxides are
aromatic and contain more than 1.5 epoxy groups per molecule and most
preferably more than 2 epoxy groups per molecule.
The useful materials have a molecular weight of about 150 to 10,000
5 and preferably from about 300 to l,OOû. Useful materials include linear
polymeric epoxides having terminal epoxy groups (e.g., a diglycidyl ether of a
polyoxyalkylene glycol), polymeric epoxides having skeletal epoxy groups
(e.g.,p.~lybu~l;_l._ PUIY~UAY)~ and polymeric epoxides having pendant epoxy
groups (e.g., a glycidyl ".~ LI,a. ly polymer or ,u~ulylll~,.), and mixtures
10 thereof.
Useful epoxide containing materials include ~u"lr ' having the
required molecular weight of the general Formula I:
R' ~OG~CH-GH~d I

wherein:
R' is alkyl, alkyl ether, or aryl, preferably aryl and n is an integer
20 between 2 and 6. Preferred are aromatic glycidyl ethers such as those prepared
by reacting a polyhydric phenol with an excess of epichlorohydrin. Examples
of useful phenols include resorcinol, catechol, llyd-~l o, and the
pol~..u_l~u phenols including p~p'-d;i~ydluAy-l;b~ yl~ p~p~-dil~ydluAy~ ' yl~
p~p~-dil~ydluAy~ ' yl sulfone, p~p~-dil~ydluAy~ , 2,2'-dihydroxy-
25 1,1-' , ' y' , and the 2,2', 2,3', 2,4', 3,3', 3,4', and 4,4' isomers of
~lihyJluAy~ y , ~ llUAy~ ,i; yl~ ,LI-yl
llillyllluAy~ Jh~ Llly y~ UAy~ h_.~yll.. _,llyl~lu~yll~. - Lll~ule~
y~lluAy~ h ~lyl~,~llyli' y' '- ', d;l~yllluAy~ Jh-~yllJlu~yl~ ylll~
llilly~llUAy~ yll~u~yl~ llyl~ lihylluAy~ yl~ulyllll~
30 dihJI~uAyJ;~ yl~uly y , dil~yllluA~ yl li~ y~ Aylll~
and dillylluAyd ~II_.~yl~;y~,lu~l~ A~U~C. Also preferred are polyhydric phenolic
~ .

2175~
WO95/12617 ' PCTtUS9~i/12731
~ ~ ~ yJ~ products as well as polyglycidyl ethers that contain
as reactive groups only epoxy groups or hydroxy groups.
Cnmro~ c of the above general Formula 1, but wherein n=l, are
useful as optional additives in the c ~ of the instant invention so long
5 as, in the preferred ~ bol~ t, the average epoxy ~ ;ly relative to the
total number of epoxy ~ r employed is greater than one.
Useful materials include diglycidyl ethers of bisphenol A and of novolak
resins, such as described in "Handbook of Epoxy Resins" by Lee and Nevill,
McGraw-HIll Book Co, New York (1967), '--, ' ' herein by reference
10 Epoxides with flPYihiii7PA backbones are also useful. Preferred materials
include diglycidyl ethers of bisphenol A and diglycidyl ethers of bisphenol F,
and most preferably diglycidyl ethers of bisphenol A, because of the desirable
structural adhesive properties that these materials attain upon curing
Examples of ;ally available epoxides useful in the invention
15 include diglycidyl ethers of bisphenol A (e g, those available under the
tr~iPm~ c Epon 828, Epon 1001, and Epon 1510 from Shell Chemical Co,
and DER-331, DER-332, and DER-334 available from Dow Chemical Co );
diglycidyl ethers of bisphenol F (e.g., EpiclonTM830 available from Dai Nippon
Ink and Chemicals Inc ); silicone resins containing diglycidyl epoxy
20 r.. 1;.. 1;l~, flame retardant epoxy resins (e g, DER 580, a b.~ '
bisphenol type epoxy resins available from Dow Chemical Co ); and 1,4-
butanediol diglycidyl ethers
In the practice of the invention, a base curing agent is used in an amount
sufficient to cure the epoxy adhesive ,: , The amount can vary from
25 an ~ ' amount based on the type of epoxy resin used to
an excess of either the epoxy or the base curative, depending upon the end use
of the epoxy adhesive. The amount typically ranges from about 1,5 to 200
parts by weight of curing agent per 100 parts of the total amount of epoxide
used Preferably, the base curing agent will be present in an amount of about
30 2,5 to 75 parts by weight of the curing agent per 100 parts of epoxide
--5 -

WO 95/126 17 ~ 1 : ; PCI/US9.1/1273.1
217~5~4
The base curing agent contains at least one ~ ~rhili~ or ~ -ct~rhilir
group which reacts with the epoxy ring to cross-link the adhesive ~
Suitable base curing agents include polyamide resins, aliphatic amines,
polyether diamines, aromatic amines, pOl,ya~ C:" POI~
5 polyeth~.J;,.~ , phenol c.~ and mercaptan resins. Examples of
primary amines include di-(4~ u~ ..yl)sulfone, di-(4-all.inu~ lyl)-ethers,
and 2,2-bis(4-(,.~; ~pl "~I)propane, ethylene diamine, I ' yl~ diamine,
isomers of l~ .dl~ C diamine, diethylene triamine, triethylene tetramine,
L~L-~l~,Lllyl_~., pentamine, ~ triamine, N,N'-Bis (3-~ JlUltJ.Yl)-
10 1,2-ethane diamine, N-(3-A r u~J~1)-1,3-propane diamine N-(2-aminoethyl)-
1,3 propane diamine, isomers of c.~Iûll~ m~ diamine, 4,4'-methylene
k ' , 4,4'-methylene bis[2-1l.~ , ' ' ], isophorone
diamine. Examples of useful tertiary amines are di~ ,Ll~yl~lll;l~ulJIu~
and pyridine.
Examples of useful aromatic amines include di-(4-d.. li.. op'.~ l)sulfone,
di (~ ~' yl)ether, 2,2-bis(4-d,..illu~ l)propane, 4,4'-diamino
lliJ ' y' ~, 3,3'-dimethyl(4,4'-~ 1 methane, m-phenylene
diamine, p-phenylene diamine, m-xylylene diamine, toluene diamine, 4,4'-
methylene dianiline benzidine, 4,4'-i ' lin~, 4-methoxy-1,3-~ll.,..,yl-lid.l.il~c,
20 2,6-~" rJ.iJ;,I~, and ~
Examples of polyether diamines include 4,9 ,~ 1,12-
diamine, 4,7,10-T - 1,12-diamine, bis(3-amino
propyl)~l~i ' yJ~uru~S of varying molecular weights, and w.. ~;~lly
available from Texaco Chemical Co. under the Jeffamine trade name as D230,
25 D400, D2000 and T403.
Suitable polyamido amines are the reaction products of pcl~ and
dimer acids. Dimer acids are prepared by dimerizing Cl8 or C22 fatty acids
from vegetable oils or animal fats. The dimer acids are then reacted further
with ~1~ by a c. .- -~ ' ;. . reaction to produce the polyamido amine
30 oligomers. These oligomer are described by V. Brytus, Modern Paint and
CQatin~s. Vol. 74 No.10, p. 172 (198*.
-6-

WO951126.17 i~ 7~ PCTIUS9~/12734
Examples of phenol c~ u~ include phenol, substituted adicyl phenols
(nonyl phenol), diphenols sueh as eateehol, ~ind aiicyl substituted catechol,
resorcinol, lly ilu~luii~u~
Examples of mereaptan resins include a'iicyl di..._.~ij~.~ such as ethane
5 dithiol, nonane dithiol, renta erythritol tetra (3-mercapto propionate),
trimethylol propane tri(3-mercapto propionate), glyeol dimereapto acetate, thiolterminated polyethers and thiol terminated puly~ul~
Also useful are boron rCl~rlr~yr~ and in particuiar, boron eomplexes
with "~ " ~ imidazoles such as 2-ethyl-4-methyl imidazole;
10 guanidines such as t~ llyl guanidine; substituted ureas sueh as toluene
C~ u~.~ urea; ~' y, l-~ , and aeid anhydrides sueh as 4-
yll~idl~ u~Ly~ ic acid anhydride, 3-1~ lL~id~yJIu~y~ la~iic aeid
arihydride, and ' ylllu~b~ h ~ acid anhydride. Mixtures of more
than one curative may be used. Preferred curatives for one-part adhesive
15 cr~ ~ are amines, acid anhydrides, ell~nillinr~c ' yr l ~ ir~ and
mi,ctures t~iereof.
Speeific examples of base curing agents are A "rMSeries,
~ iially available from Air products and Chemica'i Company, and the
SchereY Series, cu...lll~.uially available from S.h~i.lg 3~1u~g.
A. ~ nown in the art can a'iso be added to increase the cure rate
of the eroxy adhesive. Such 2. ' include , ' that ean act as a
curative when used a1ione, but when combined with a different class of
euratives, will accelerate the curing of the epoxy adhesive ~
Examples of useful ~ include phenolic . ', tertiary amines,
25 d;~ y " I imidazole, substituted imidazole hexakis imidazole nickel
phthadate eomplex, substituted ureas arid edcium ~iinuulull~ lyl~ulr~
These: ' may be used alone or in together to
sccelerate the cure of an ej~oxy adhesive . ' Some examples of
useful ~- include phenolic , ' with tertiary amines,
30 ~'ii. y, .~ witi'i imidazole and/or substituted ' ' . di~y~
with substituted ureas, ~iiuy~ with hexakis imidazole nickel phthdate
-7-

W095/12647 217 5 5 7 4 , ` ~ PCT/US9~/1273~ ~
complex and calcium llilluulu~ 1 sulphonate with ' ' A preferred
curing agenV~ i.),, is toluene .lii,u~,~ urea and
d;c~ ' ' The preferred amount of the accelerator is from about 0.5 to
15 percent by weight of the adhesive system.
Tbe epoxy adhesive OI l~ includes a partieulate ion exchange
corrosion inhibiting additive. The additive particles are formed from an
inorganic oxide of silica or alumina and have cations chemically bound to them
that are useful for corrosion inhibition. The useful cations include calcium
(Ca2+), zinc (Zn2+), cobalt (Co2+), lead (Pb2+), strontium (Sr2+), lithium
10 (Li+), barium (Ba2+), and m~nrCi~.m (Mg2+). Preferred cations include
calcium and zinc.
The additive partides will preferably have an average diameter of about
0.1 to 200 rnicrons. More preferably, the particles have an average diameter of
about 1 to 50 mierons. Suitable additive particles include a calcium ion
15 exchanged amorphous silica gel c~llll,l~l.;ally available from W. R. Grace &
Co. under the tradename "Shieldex".
The epoxy adhesive ~,,...I,, c:l;,,,~ preferably includes a toughening agent,
and in partieular, a polymeric toughening agent or a ~ ;. " of polymerie
Luu~h~.~.g agents. Useful toughening agents have an epoxide; u ~, ';l.l~
20 component s~lh~t~nt~ ly insoluble in the epoxy resin and an epoxide compatible
component 5~hct~nti~11y soluble in epoxy resin.
The toughening agents which are useful in the present invention include
polymeric eu~ o~ having both a rubbery phase and a ~ phase,
such as graft ~u~ having a pùl~ i~i diene rubbery core and a
25 pOl~ yla~G ûr P~ G shell; graft l,V~ having a rubbery core
with a polyacrylate or pol~ Ll~ y- shell; and ~ particles
pOIylll~.iL~ in situ in the epoxide from free-radical poly..,~liL~Lle monomers
and a ~ulJol~",. lic stabilizer.
Specific examples of useful toughening agents include graft wlJolyl,.
30 having a pul~ I;L~I diene rubbery backbone or core which is grafted to a
shell of an acrylic aeid ester or ..~ .11~..,l~1;. aeid ester, monovinyl aromatic
-8-

WO 951126~7 21 7 ~ 5 7 ~ PCTIUS9~/1273~
llydlu~lJull, or a mixture thereof, such as disclosed in U.S. Patent
No.3,496,250. Preferable rubbery backbones comprise pul~ ~ butadiene
or a pol~ li~l mixture of butadiene and styrene. Preferable shells
comprising pùlyl..v~ lic acid esters are lower alkyl (Cl-C4)
S substituted Ir~lllll .y' Preferable monovinyl aromatic llydlu~ulJolls are
styrene, alpha~ .lh.~l~L~.clle, villy I , vi~ ylv;~ b~
ia~lu~la~yl~ U~iyl~ , d;~.lllulualyl~ , and ethylchlulua~yl~
Further examples of useful IUU~ ..UI.~6 agents are acrylate core-shell
graft culJul~ ,.a wherein the core or backbone is a pul~lyl~k polymer
10 having a glass transition t~ laLul~; (T8) below about 0C, such as polybutyl
acrylate or ~ul.~;~ùùu~yl acrylate to which is grafted a polymer (shell) having a
Tg above 25C such as pùly ' yl~
Still further examples of luu~ agents useful in the invention are
; ' particles that have a Tg below about 25C and have bcen
15 ,ool~ i~i in situ in the epoxide before mixing with the other ~ r of
the r These ~ particles, commonly referred to as
"organosols", are ~ol.~ i from free-radical pul~ li~l,le monomers and a
~u~ u~y ' ' polymeric stabilizer that is soluble in the epoxide. The free-
radical pul~ monomcrs are ethylenically I ' monomers or
20 J;;au~"~ combined with co-reactive ~--r '- 1 hydrogen ~ . ' such
as diols, diamines, and ~ Examples of these ~ particles
are disclosed in U.S. Patent No. 4,525,181.
Still other lu. ~' I,, agents are rubber modified liquid epoxy resins.
An example of such a resin is KratonTM r~P656s Rubber available from Shell
25 Chemical Company. The modified epoxy resin is made from 85% by weight
EponTM 828 and 15% by weight of a KratonTM rubber. The KratonTM rubbers
are known in the industry as Pl~ block culJul~ .la.
Toughening agents can also include liquid epoxies, liquid amines,
polyether diamines, polyhydlu~ , pul~v;..~ld~ ls, and liquid ~ly- l~
30 butadiene polymers, l,u~.li.;..e/..il-ile rubbers, ~.cubu~.y' I butadiene/nitrile
rubbers, amine-terminated butadiene/nitrile rubbers, carboxyl ~ ~
g

wo 951126~7 2 1 7 ~ 5 7 ~ - pCTlUS9~/1273~ --
I-u~l;~ 1iuile rubbers and the amine or carboxyl terminated adducts of the
polymers with epoxy resins. Amine-terminated and carboxyl t~.111;1._'~i
bul~ acrylonitrile rubbers are :U.I~ .I ially available from B.F. Goodrich
under the HYCAR tradename as ATBN and CTBN reactive liquid polymers.
5 t'11 11.;, '11111C of toughening agents may also be used to enhance the properties
of the cured epoxy adhesive.
The toughening agent is preferably used in an amount equal to about 3
to 35 parts by weight, and more preferably about 5 to 15 parts by weight per
100 parts by weight of the epoxy resin. The toughening agents of the present
10 invention add strength to the ~ul.,~ " after curing without interfering with
curing. The toughening agent may or may not react with the epoxide.
In some cases reactive diluents may be added to control the flow
;fS of the adhesive c~ ';-- Suitable diluents have at least one
reactive terminal end portion and preferably, a saturated or .... ~,, t .1 cyclic
5 backbone. Preferred reactive terminal ether portions include glycidyl ether and
vinyl ether. Examples of suitable diluents include the diglycidyl ether of
resorcinol, diglycidyl ether of . y.' ' ~' ' ~1, diglycidyl ether of
neopentyl glycol, triglycidyl ether of I ~1~1PIU1J~UIIS dipentene, and the
divinyl ether of c~ " ~' Commercially available reactive
20 diluents are "WC-68" from Rhone Poulenc, and RapicurerM CHVE, a divinyl
ether of ~ ~. ' ' " ' ' available from Allied-Signal Corp. of
r~ .. , NJ.
Various ûther adjuvants can be added to the epoxide ~ ;-,, to
enhance properties of the ' . before and after curing.
Included among useful adjuvants are nonreactive diluents; ~)L.,ii.,;4~.
such as ~UI1v~ iO..~I phosphates and phthalates; flame retardants such as
borates, '..1 aluminum hydroxide, m~nf-ci~1~ hydroxide, and bromine
J ~i~ thixotropic agents such as fumed silica to provide flow control;
pigments to enhance color tones such as ferric oxide, brick du$, carbon black,
30 and titanium dioxide; fillers such as talc, silica, , , calcium sulfate,
beryllium aluminum silicate; clays such as bentonite; glass and ceramic beads
-10-

.
W0951126~7 21 7Ss7~ , PCT/US9t~1273~
and bubbles; ~ c imparting X-ray opacity, such as barium .,.~
and reinforcing materials, such as woven and nonwoven webs of organic and
inorganic fibers such as polyester, polyimide, glass fibers, and ceramic fibers.Dispersing agents and wetting agents, such as silanes, can also be added so long5 as they do not interfere with the curing reaction of the epoxy adhesive
c~ The adjuvants can be added in an amount effective for the
intended purpose; typically, amounts up to about 50 parts of adjuvant per total
weight of ~ ' can be used.
Presently preferred ~ Of the invention or c~ to be
10 used in the methods of the invention are ~ c~n~ ly free of W..~,-lLiUII`~II
corrosion inhibitors such as aluminum phosphates and chromate salts. Further,
preferred methods of the invention rely on the use of an oxide of silica or
alumina having cations bound thereto, and do not involve the use of other
corrosion inhibitors such as aluminum phosphates or chromate salts either in the15 adhesive , or as a ~ t of one or both of the surfaces to be
bonded before application of the adhesive.
The epoxy adhesive ~ of the present invention may be
formulated in a variety of ways, including one-part and two-part adhesive
systems. By providing a two-part ~ ; l ;- . with the two parts being
20 combined prior to use of the c~ desirable shelf-life or pot-life of the
:1;.... is obt3ined. In some ,~ it is desirable to select the
amounts and the ,' ' of the ~gr-~' ' iri each part to provide viscosity
control and better mixing of the two parts. For exarnple, the fillers can be
divided so that each part contains a portion of the fillers used.
The epoxy L "' of the present invention can be cured by any
means which allow sufficient heat to start the curing reaction. The merins of
curing can include Cul.~ i ovens, induction heating, infrared radiation,
microwave radiation, immersion into liquid baths, or any -,...l. - ';.~1~ thereof.
For two part adhesive the curing can be effected at room
30 i , ~ for about 24 hours. Typicalily, the finai curing is conducted at a
~.lli.~ul~ in the range of about 15C to about 230C for a time ranging from
-Il-

WO 95/12647 ~17 ~ 5 7 4 : PCTIUS9111273 4
about 1 second to about 2 hours. Curing may be done in several stages, e.g.,
induction curing for 30 seconds, and oven curing at 215C.
The curing time will depend upon the particular process for curing.
Induction heating times typically range from about 1-60 seconds while oven
5 curing times can range from about 0.1 to about 2 hours.
The epoxy adhesive ' A ' - of the present invention are especially
useful for bonding metal to metal and plastic to metal, although it can be used
for bonding only plastic surfaces. ~xamples of metal surfaces include steel,
titanium, oily steel, aluminum, and ~ Plastic surfaces include sheet
10 molding -r ~, pOl~,~Ll~ c~ poly~l,. , polyester, pol~ cL}.~,~,
acrylonitrile butadiene styrene, and IIIC C( ~ ~ ~ yde. The epoxy adhesive can
be used in assembling parts such as for ~ c, aircraft"~
units, etc.
The following non-limiting examples serve to further illustrate the
15 present invention in greater detail.
TEST PROCE~DURLS
LAP SHEAR STRENGTH
This test measures the shear strength that an epoxy adhesive cl, 'l"~` ""'~
20 will achieve in a single overlap bond after being fully cured. The lap shear
strength is also referred to as the "overlap" shear strength. A test sample is
prepared by applying the adhesive to 2.54 cm x 10.16 cm U~
aluminum strips and curing as detailed below. The aluminum strips used in the
tests were:
A - 1.6 mm thick 6111 aluminum having a "mill finish", available
from Alcoa Aluminum Co.
B - 1.6 mm thick 5754-0 treated aluminum from Alcan.
C - 0.9 mm thick 6111 aluminum treated with Parker MP404 Lube
(treatment available from Parker Div. of Henkel Corp.)
D - 0.9 mm thick 6111 aluminum treated with Parker MP404 Lube &
Parker PL303 Wash (treatment available from Parker Div. of Henkel Corp.)
-12-

WO 95/12647 7S~ 7~ PCT/US9~/1273.1
~ - 1.6 mm thick 2024 T3 clad aluminum with surface prepared with an
FPL etch
The adhesive is mixed with about 1% glass beads ("Microbeadm 1405
Class IV r,.L;,.r. ;,~ Grade" measuring between 0.35 to 0.246 mm in
5 diameter, available from Cataphote, Inc.) to provide a 0.25 mm thick bond.
The adhesive is then applied, within 30 minutes of mixing, to a 1.27 cm area
on one end of one strip of aluminum and a second strip of aluminum is placed
so that 1.27 cm of one end overlaps the adhesive and with the uncoated ends of
each strip extending in opposing directions. The strips are clamped together
10 and cured according to the conditions detailed in the examples. The prepared
samples are cl~ A for at least two hours at between 21C and 23C
before testing to determine the initial (INIT) strength, and the aged samples are
subjected to the aging conditions described below, and: " ~ ' for 2 hours
at between 21C and 23C before testing. Llevated ~ shear tests are
15 run at the i , ci~ shown in the examples and samples are ~ ..,..ri at
the test i ~ for at least 15 minutes, but no more than 30 minutes,
before testing.
The lap shear is ~ i using a tensile tester according to ASTM
Test Method D1002-72 under one of two conditions as follows:
Shear Test I - The crosshead speed is run at the speed required to
maintain a rate of loading between 800 to 1000 N/minute.
Shear Test II - The crosshead speed is run at 1.27 cm/min.
The lap shear is reported in units of megaPascals (MPa).
The mode of failure is also recorded and noted as adhesive (A), wherein
25 the adhesive pulls away from one of the aluminum strips, cohesive (C), wherein
the adhesive splits leaving adhesive on each of the strips, or mixed (M),
wherein both modes of failure are observed. If corrosion is visible along the
edges of the aluminum strips or in extreme cases when there is an adhesive
failure and corrosion is exposed, the a~ v~ area of corrosion is also
30 noted as a percentage of the total area covered by the adhesive.
-13-

wo 95/126~7 217 5 5 7 4 PCT/USg~11273 1 ~1
The test results represent the average of at least three
samples involving a particular epoxy adhesive
AGING TESTS
Samples are prepared and tested as described above for overlap shear
except that the samples are aged in one or more of the following aging tests:
1) Water Soak
The samples are soaked in 23C deioni2ed water for 750 hours.
2) Salt Spray Test
The samples are subjected to a 5% salt spray at 35C according to
ASTM B117-90 and tested after .750 hours.
15 3) Elevated T, ~ /Humidity
The samples are aged at 50C and 95% RH for 750 hours.
4) Cyclic Corrosion Aging Test
Lap shear samples are prepared and cured according to the above-
20 described procedure The sampls are then immersed into a 5 % NaCI colutionat room ~.~ u1~ ~betweeen about 21 and 23) for 15 minutes. The
samples are then drip dried at room t~ Lu1~i for 105 minutes and placed in
a humidity chamber at 50C, 90% relative humidity for 22 hours. Each
immersion in the salt water solution marks the beginning of one cycle. On days
25 when the samples are not immersed in water, the samples are stored in the
heated humidity chamber detailed above and these days are not counted in the
total number of cycles.
If the samples are exposed to the above cyclic corrosion test under
stress, six lap shear samples are prepared for each adhesive Cu.l.~,u,;Liu... The
30 samples are loaded into a fixture which uses a ' . u ~ spring to exert a
tensile load on the lap shear coupons. The spring is then cu..l~ ,cd in a vise
-14-

WO 95/126~7 1 7 $ $ 74 PCT/US9~/12734
to the proper ~ to apply a tensile load of 2 MPa, S MPa, or 7 MPa,
and the fixture is tightened to maintain the desired load. The samples are then
exposed to the cyclic corrosion test conditions detailed above. The samples are
checked daily for joint failure. Failure is noted when lap shear joints break
S apart. The failed sample is then replaced in the fixture with a solid strip of aluminum of the ~ ,l length and the cyclic corrosion test is continued
until the third sample fails. Results are recorded as the number of days to
failure (DAYS TO FAILURE). The remaining three samples are then tested
for residual lap shear strength (RESIDUAL STRENGTH) according to the Lap
10 Shear Test procedure described above. Results are recorded in MPa.
Examyle I
A one-part epoxy adhesive ~ was prepared by mixing 10.73
parts of a methacrylate butadiene styrene h.l~vlyl~. l (Paraloid~EXL2691
15 available from Rohm & Haas) with 40.22 parts of a diglycidyl ether of
bisphenol A (Eponn'82g available from Shell Chemical Co.), and 13.4 parts of
a flexible resin (CIBATYXB4122 made by Ciba Geigy), and heating at about
80C for about 60 minutes with constant stirring. The mixture was then cooled
to about room ~ r, and the following were added and mixed with a high
20 shear mixer: 2.68 parts of aluminum powder, 4.29 parts fumed silica (Ca~-O-
SilD'TS-720 silica available from Cabot Corp.), 5.36 parts barium ~
(BUSAN 1l-M2 available from Buckman ~ ,), 16.09 parts alumina
tri-hydrate, 2.68 parts of calcium io.. ~ ~ ' silica gel (SHIELDE~ACS
available from W. R. Grace & Co.), 3.21 parts J;~,y-...l:.", -~. (Amicure CG
25 1200 available from Air Products, Inc.), and 1.34 parts hexakis (imidazole)
nickel phthalate. The d;~ y ' ' and hexakis(imidazole) nickel phthalate
were micronized to a particle size of about 10 l~ The adhesive
rt~mlu~si~ n was degassed, made into lap shear samples with substrate B, and
cured for 40 minutes at 170C. The samples were tested for initial lap shear,
30 and aged lap shear using Shear Test II. The samples were aged under the
-15-

21~S5~4
WO 9~i/126 ~7
; ~r ; PC'I'IUS9J/1273
Cyclic Corrosion Exposure Test under stresses of 2 MPa, 5 MPa, and 7 MPa.
Test results are shown in Table 1.


-16-

~ WO 95/126~7 21 7 ~ 5 7 ~ ~CT/US9~/1273~
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--17--

WO 95/126~7 ~ ; " PCT/US9-111273-1
The data in Table I show that bonds made with the adhesive
. ù ~ of the invention last longer under a corrosive environment and
stress than bonds made with a state-of-the-art adhésive containing a well known
aluminum corrosion inhibition treatment.
C ^ Examvle Cl
A ~:u~ llly accepted toughened epoxy adhesive ~.. ,1,.,~:l;.. . having
strontium chromate as a corrosion inhibitor was used. The strips were tested
under a load of 7 MPa.
A one-part epoxy adhesive CC"'~I~J~ was prepared by mixing 41.7
parts EPD~OTEn'828 (also sold as EPON~828), 16.6 parts of a diglyciyl ether
of bisphenol F (EPIKOTEn'862 available from Shell Chemical Co.), 13.2 parts
1~ ' ~L 2600 I..~LI.~Iy' butadiene styrene terpolymer (available from
Rohm & Haas), and an adduct of diglycigyl ether of bisphenol A and carboxyl-
terminated butadiene rubber (EPIREZn'58006 available from Rhone Poulenc) at
about 80C for about an hour. The mixture was cooled to about room
t~ lr and the following were added using a high shear mixer: 2.6 parts
Aerosiln'200 silica (available from DeGussa), 0.7 parts glycerol, 4 parts
micronized d;~ n -l^~ 4 parts Ancamine~2014 S (available from Air
Products and Chemical Co.), 0.7 parts glass beads having a particle size
between about 90 - 150 IlPl~u~ t~.~ (available from Glaverbel, of Belgium)
and 3.3 parts Shieldex~^AC5. The adhesive , was degassed and
tested for lap shear strength and aging on substrate ~. The adhesives were
cured for 120 minutes at 130C under a heated platen at a pressure of 100
kiloPascals. Test results are shown in Table 2.
-18-

WO95/l26l7 1 7~S74 PCT/US9~/1273
Cn~nn ~r;Ve FY~ C C2 - C3
Adhesive ~ ,n ~ were prepared as in Example 2 except that
Example C2 had no corrosion inhibitor, and Example C3 had 3.3 parts of
strontium chromate which is a state-of-the-art corrosion inhibitor.


-19-

W0951126~7 217 ~ ~ ~ 4 ' ~ PCTIUS9~/1273~ --
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--20--

~ WO 95/12617 7$S 7,~ 1 ~ PCT/US9~11273~
The data in Table 2 show that the use of a calcium ion-exchanged silica
gel ~ the p~:lru."~ e of strontium chromate as a corrosion
inhibitor without the ~,..v;lu~ t~l hazards of heavy metals.
S FY~m~l~ 3
Part A of a 2-part adhesive . was prepared by mixing 4û
patts of a polyether diamine (sold by Minnesota Mining & r ~ ~ g Co.
as Part A [amine curativq of a Sco~ LwkLDTM22l6 BA Clear Amber
epoxy adhesive kit), 6.0 pafts 4,7,10-~ 1,13-diamine (TI~
lû available from BASF), 8.0 parts 2,4,6-tri-dil,.~ Ll,y ' yl phenol (K-54
available from Anchor Corp.), 3.0 parts ~ I ' butadiene rubber
(ATBN 1300X16 available from B. F. Goodrich Co.), and heating to a
t. ..,~.~lu,~ of about 70C to form a uniform mixture. The mixture was cooled
to about room ~111~ , and 20 parts amorphous silicon dioxide (GP-71) and
15 3.0 parts fumed silica (Cab-O-SilTM TS-720) were added with a high shear
mixer.
Part B of the 2-part epoxy adhesive , was prepared by mixing
together 15 parts of Ill.,Lll.l.lylal~ butadiene styrene IC~I~JUI~YIII~
(I` ' ~XL2691) with 80 parts of a diglycidyl ether of bisphenol A
20 (E~pon'Y828) and 20 parts diglycidyl ether of "~ l (Hdoxy
MK 107 made by Rhone Poulenc), and heating at about 80C for about 60
minutes with constant stirring. The mixture was then cooled to about room
t~ lll~l~lLI,.I, and the following were added and mixed with a high shear mixer:2.0 parts Ca(SO3CF3)~ (micronized to a nominal particle size of about 10
25 Il-i~lUII~ s), 2.5 parts epoxy silane (Z-6040 available from Dow Coming),
2.0 parts fumed silica (Cab-O-Siln'TS-720), 3.0 parts glass beads having an
average diameter of about 0.01 inch [0.25mm] (available from Cataphote, Inc.),
2û parts: .' silicon dioxide (GP-71 available from Harbison-Walker
Corp.), and 18 parts glass bubbles (1337/2000 available from Minnesota Mining
30 & r~ ~ ~, Co.), and 5.0 parts of calcium ion-exchanged silica gel
(SHIFT DEX~AC5).
-21-

W0951126-17 21~74 . PCT/US9~/1273-1 ~
An adhesive ~ was prepared by mixing a 2:1 volume ratio of
Part B:Part A. The adhesive was made into lap shear samples as described
above on substrates C and D at two cure conditions. Cure 1 indicates that the
curing was done with a 6-second induction heating cycle to a b,~ u~c of
5 135C and then oven cured for 20 minutes at 170C. Cure 2 indicates a room
~""~ c (between about 21~C to 23) cure for 20 to 24 hours and a
subsequent oven cure for 20 minutes at 170C. The test was conducted using
Shear Test 2. Test results are shown in Table 3.



-22-

W095/126~7 7$S74 ~ PCTNS9~/1273
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--23--

W0 951126~7 217 5 ~ 7 ~ -~ ` ` PCTIUS9~/12731 ~
Example 4
Part A of a two-part epoxy adhesive ~...,.l,..~ l,..,. was prepared by
mixing 29 parts polyeeher diamine (TTD) and 5.0 parts of a 2,4,6-tri-
d;~ Y1AIII~ yl phenol (DMP 30 available from Rohm & Haas), and
5 applying sufficient heat to form a uniform solution.
Part B of the 2-part epoxy adhesive C~ ,u~ ~i. n was prepared by mixing
together 20 parts of ~ .LIl~lyl~ butadiene styrene terpolymer
~ParaloidlYEXL2600) with 100 parts of a diglycidyl ether of bisphenol A
(Epon'U828) and heating at about 80C for about 60 minutes with constant
10 stirring. The mixture was then cooled to about room ~.llp~ldlul~ and the
following were added and mixed with a high shear mixer: 4.0 parts fumed
silica (Aerosiln' R202 available from DeGussa), 2.5 parts glass beads having a
particle size between about 90 - 150 Ill;. ~ (available from Glaverbel),
and ~.0 parts of calcium ion ~Aul-~l6c~ silica gel (SHIELDEXD'AC5 available
15 from W. R. Grace & Co.).
A 2-part adhesive was prepared by mixing Part B with Part A (in a 2:1
volume ratio and Part B:Part A) and preparing lap shear samples on substrate
E. The adhesive was cured for 24 hours at 23C under 100 IcPa pressure and
then oven cured for 60 minutes at 80C. The samples were tested for initial
20 lap shear and aged lap shear strength using Shear Test 1. Data is shown in
Table 4.
C~:, v~ Examples C4 - C5
Two-part epoxy adhesive c~ )c~ were prepared as in Example 4
25 except Example C4 had no corrosion inhibitor, and Example C5 had 5 parts of
Strontium chromate. Samples were tested as in Example 4 and test results are
shown in Table 4.
-24-

WO 951126~7 S~ 74 PCTIIJS9~/1273.1

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--25-

WO 95/126~7 ~ ~5~l ~ PCT/US9.1/1273
l~xample S
Part A of a 2-part adhesive ~ o~iLiu-- was prepared by mixing 40
parts of a polyether diamine (sold by Minnesota Mining & 1` ~ ' ~ as
Part A of Scol~HwklD~22l6 BA Clear Amber epoxy adhesive kit), 6.0
5 parts polyether diamine (H221 available from Union Carbide Inc.), 8.0 parts
2,4,6-tri d;ll~c Lll~ 1 phenol (K-54) 3.0 parts-amine terminated
butadiene rubber (ATBN 1300X16 available from B. F. Goodrich Co.), and 5
parts imidazole and heating to about 70C with constant stirring to form a
uniform mixture. The mixture was cooled to about room t~ Lulc: and 20
10 parts amorphous silicon dioxide (GP-71) and 3.0 parts fumed silica (Cab-O-
Siln'TS-720) with a high shear mixer.
Part B of the c~. l-u~ was prepared as in Fxample 3 except that
19.5 parts of glass bubbles were used.
An adhesive ~ was prepared by mixing 2 parts ûf Part B to
15 one part of Part A by volume.

-26-

Representative Drawing

Sorry, the representative drawing for patent document number 2175574 was not found.

Administrative Status

For a clearer understanding of the status of the application/patent presented on this page, the site Disclaimer , as well as the definitions for Patent , Administrative Status , Maintenance Fee  and Payment History  should be consulted.

Administrative Status

Title Date
Forecasted Issue Date Unavailable
(86) PCT Filing Date 1994-11-04
(87) PCT Publication Date 1995-05-11
(85) National Entry 1996-04-01
Dead Application 2002-11-04

Abandonment History

Abandonment Date Reason Reinstatement Date
2001-11-05 FAILURE TO PAY APPLICATION MAINTENANCE FEE
2001-11-05 FAILURE TO REQUEST EXAMINATION

Payment History

Fee Type Anniversary Year Due Date Amount Paid Paid Date
Application Fee $0.00 1996-04-01
Maintenance Fee - Application - New Act 2 1996-11-04 $100.00 1996-05-01
Registration of a document - section 124 $0.00 1996-08-01
Maintenance Fee - Application - New Act 3 1997-11-04 $100.00 1997-10-21
Maintenance Fee - Application - New Act 4 1998-11-04 $100.00 1998-10-16
Maintenance Fee - Application - New Act 5 1999-11-04 $150.00 1999-10-21
Maintenance Fee - Application - New Act 6 2000-11-06 $150.00 2000-10-23
Owners on Record

Note: Records showing the ownership history in alphabetical order.

Current Owners on Record
MINNESOTA MINING AND MANUFACTURING COMPANY
Past Owners on Record
LAMON, ALAIN H.
Past Owners that do not appear in the "Owners on Record" listing will appear in other documentation within the application.
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Document
Description 
Date
(yyyy-mm-dd) 
Number of pages   Size of Image (KB) 
Abstract 1995-05-11 1 24
Cover Page 1996-08-08 1 11
Description 1995-05-11 26 698
Claims 1995-05-11 2 35
International Preliminary Examination Report 1996-05-01 11 343
Fees 1996-05-01 1 46