EPOXY CURATIVE COMPOSITION AND COMPOSITIONS THEREFROM

Abstract

An epoxy curative is provided comprising: a) a Lewis base, b) calcium nitrate, and c) a polyamine amide salt. The present disclosure additionally provides a composition which is a mixture obtained by mixing the epoxy curative and a curable epoxy resin. The present disclosure additionally provides cured compositions which result from cure of such a mixture.

Claims

1. A composition which is an epoxy curative comprising: a) a Lewis base, b) calcium nitrate, and c) a polyamine amide salt.

2. A composition which is a mixture obtained by mixing: I) a curable epoxy resin, II) an epoxy curative comprising: a) a Lewis base, b) calcium nitrate, and c) a polyamine amide salt.

3. A composition which results from cure of the mixture according to claim 2.

4. A composition according to claim 3 which additionally comprises a fire retardant.

5. A composition according to claim 3 which additionally comprises a low density filler.

6. A composition according to claim 3 having a density of less than 1.0 gram/cm3.

7. A composition according to claim 3 having a density of less than 0.7 gram/cm3.

8. A composition according to claim 3 having a compression strength of greater than 30 MPa.

9. A composition according to claim 3 having an overlap shear strength of greater than 8 MPa.

10. A composition according to claim 5 having a density of less than 1.0 gram/cm3.

12. A composition according to claim 5 having a density of less than 0.7 gram/cm3.

13. A composition according to claim 5 having a compression strength of greater than 30 MPa.

14. A composition according to claim 5 having an overlap shear strength of greater than 8 MPa.

15. A composition according to claim 10 having a compression strength of greater than 30 MPa.

16. A composition according to claim 10 having an overlap shear strength of greater than 8 MPa.

17. A composition according to claim 11 having a compression strength of greater than 30 MPa.

18. A composition according to claim 11 having an overlap shear strength of greater than 8 MPa.

19. A composition according to claim 14 having an overlap shear strength of greater than 8 MPa.

20. A composition according to claim 16 having an overlap shear strength of greater than 8 MPa.

Description

EXAMPLES

[0028] Unless otherwise noted, all reagents were obtained or are available from Sigma-Aldrich Company, St. Louis, Mo., or may be synthesized by known methods. Unless otherwise reported, all ratios are by weight percent.

The following abbreviations are used to describe the examples: [0029] F.: degrees Fahrenheit [0030] C.: degrees Centigrade [0031] cm: centimeters [0032] in/min: inches/minute [0033] Kg: kilograms [0034] KPa: kilopascals [0035] Kpsi: kilo pounds per square inch [0036] lbs: pounds [0037] MPa: megapascals [0038] mg: milligrams [0039] mil: 10-3 inches [0040] mls: milliliters [0041] mm: millimetres [0042] mm/min. millimeteres/minute [0043] psi: pounds per square inch

Materials Used.

[0044] ANCAMINE K54: Tris-2,4,6-dimethylaminomethyl-phenol, obtained from Air Products and Chemicals, Inc., Allentown, Pa., USA. [0045] APYRAL SM 200: White aluminium trihydroxide, obtained from Nabaltech AG, Schwandorf, Germany. [0046] BYK-W 966: 52% solids solution of unsaturated polyamine amides and acidic polyesters, obtained from BYK-Chemie GmbH, Wesel, Germany. [0047] BYK-W 9010: 100% solids phosphoric acid ester having an acid value of 129 mg potassium hydroxide/gram, obtained from BYK-Chemie GmbH. [0048] CALCIUM NITRATE TETRAHYDRATE: Obtained from Acros Organics, BVBA, Geel, Belgium. [0049] CRYSTAL VIOLET: Obtained from Sigma-Aldrich, St. Louis, Mo., USA. [0050] DISPARLON 6500: A polyamid wax, obtained from King Industries, Norwalk, Conn., USA. [0051] DUALITE MS 700: Polymeric microspheres, obtained from Lehman & Voss Company, Hamburg, Germany. [0052] EPIKOTE 232: A low-medium viscosity epoxy resin consisting of a blend of a bisphenol A and a bisphenol F resin, obtained from Momentive Performance Materials Holdings, LLC, Columbus Ohio. [0053] EPODIL 757: 1,4-Cyclohexandimethanoldiglycidylether, obtained from Air Products and Chemicals Inc., Allentown, Pa., USA. [0054] GLASS BUBBLES D32/4500: Glass bubbles having a density of 0.32 grams/cm.sup.3 and an isostatic crush strength of 4,500 pounds/inch2 (31.03 MPa). [0055] TITANIUM DIOXIDE: Obtained under the trade designation KONOS 1230 from Kronos Worldwide, Inc., Dallas, USA. [0056] TTD: 4,7,10-Trioxa-1,13-tridecane-diamine, obtained from BASF, Ludwigshafen, Germany. Z6040: 3-glycidoxypropyltrimethoxysilane, obtained from Dow Corning GmbH, Wiesbaden, Germany

Example 1

Preparation of Part A

[0057] 28.5 grams TTD and 9.5 grams Epikote 232 in a glass reactor and the mixture stirred for 15 minutes at 23 C. The mixture was then heated to 80 C. and held, with continuous stirring, for 60 minutes. 2 grams calcium nitrate tetrahydrate and 14 grams of Ancamine K5 were added and stirring continued for another 30 minutes, after which the mixture was allowed to cool back to 23 C. 1 gram BYK W-966 was dispersed until homogeneous using a high speed mixer, model DAC 150 FVZ, obtained from Hauschild Engineering & Co. KG, Hamm, Germany, for 1 minute at 3,000 rpm. 29.4 grams Apyral SM 200, 0.01 gram Crystal Violet, 14.5 grams D32/4500 glass bubbles and 1 gram Dualite MS700 were added in one minute intervals and dispersed until homogeneous. Part A was subsequently degassed prior to use.

Preparation of Part B

[0058] 1.2 gram Disparlon 6500 was dispersed for 1 minute in 18.8 grams Epikote 232 using the high speed mixer at 3,000 rpm and 23 C. The mixture was then heated to 90 C. and held at this temperature for 60 minutes in an oven, after which it was removed and allowed to cool back to 23 C. 1.5 grams BYK W-9010, 18 grams Epodil 757, 3 grams Z6040, 34.5 grams Apryal SM 200, 1 gram titanium dioxide, 21 grams D32/4500 glass bubbles and 1 gram Dualite MS 700, were added in one minute intervals and dispersed until homogeneous using the high speed mixer at 3,000 rpm. Part B was subsequently degassed prior to use.

Comparative Example 2 and Example 3

[0059] Comparative Examples 2 and Example 3 were prepared per the method generally described in Example 1, according to the compositions listed in Table 1.

TABLE-US-00001 TABLE 1 Part A and Part B Compositions (grams) Comparative Part A Example 1 Example 2 Example 3 TTD 28.5 28.5 28.5 Epikote 232 9.5 9.5 9.5 Calcium Nitrate Tetrahydrate 2.0 2.0 2.0 BYK W-966 1.0 0 1.0 Apryal SM 200 29.4 29.4 29.4 Crystal Violet 0.01 0.01 0.01 Ancamine K54 14.0 14.0 14.0 D32/4500 Glass Bubbles 14.5 14.5 0 Dualite MS 700 1.0 1.0 0 Comparative Part B Example 1 Example 2 Example 3 Epikote 232 18.8 18.8 18.8 Disparlon 6500 1.2 1.2 1.2 Epodil 757 18.0 18.0 18.0 Epoxy Silane Z6040 3.0 3.0 3.0 BYK W-9010 1.5 1.5 1.5 Apryal SM 200 34.5 34.5 34.5 Titanium Dioxide 1.0 1.0 1.0 D32/4500 Glass Bubbles 21.0 21.0 0 Dualite MS 700 1.0 1.0 0

Test Methods.

[0060] The following tests were performed on the adhesive Examples. Results reported in Table 2 represent an average of three test specimens per adhesive.

Compression Strength and Compression Modulus.

[0061] The compressive strength was measured according to ASTM D695 as follows. A 200 ml, 2:1 dual-chamber cartridge, obtained from Mix Pac Systems, AG, Rotkreuz, Switzerland, was manually filled with Part B and Part A in a 2:1 ratio. A mixing nozzle, type MC 13-18, was fitted to the cartridge and approximately 50 grams of the mixture extruded, at a pressure of 4 bars (400 kiloPascals) into a Teflon-coated mold having the dimensions 12.7 mm (height)12.7 mm (width)25mm (length). The mixture was then allowed to cure for a minimum of 7 days at 23 C. in the mold before removing. The cured test sample was inserted into a tensile compression instrument, model Z030 obtained from Zwick GmbH & Co, and compressed along its 25 mm axis at a constant crosshead speed of 0.05 inches/minute (1.27 mm/minute). The compressive strength was determined by dividing the ultimate load by the cross sectional area and reported in Kpsi. The compressive modulus was determined by drawing a straight line tangent to the initial linear portion of the load-deflection curve, and then dividing the slope of the straight line by the cross sectional area of the specimen.

Cohesive Shear Strength.

[0062] A 100251.6 mm strip of aluminium, type 2024 T3 CLAD, obtained from Rocholl GmbH, Aglasterhausen, Germany, was etched for 15 min. at 70 C. in a chromic acid-sulfuric acid bath having the following composition:
27.5 weight percent sulphuric acid
7.5 weight percent sodium chromate dehydrate
65.0 weight percent desalinated water
0.5 grams/liter aluminium
1.5 grams/liter copper (II) sulphate pentahydrate
The etched aluminium strip was subsequently rinsed several times in deionized water and wiped dry. Using the MixPac system, approximately 5 grams adhesive was applied on one end of an aluminum strip according to the method used in the Compression Strength Test. A second aluminium strip was then pressed onto the adhesive to form an overlap of 10 mm. and excess adhesive removed using a clean spatula. The overlapped aluminum strips were clamped together at the overlapped section using capacity binder clips, and the clamped assembly then cured at 21 C. and ambient humidity for 7 days. The bonded strip was inserted into a tensile strength tester, model Z050 obtained from Zwick GmbH & Co. KG, Ulm, Germany, and the cohesive shear strength measured according to DIN EN 2243-1 (2005), at a crosshead speed of 10 mm/min. The cohesive strength is reported in kilo pounds per square inch (Kpsi).

Insert Pull-Out Test

[0063] A 0.5 inch (1.27 cm) hole was bored into the center of a 0.533-inch (1.277.627.62 cm) section of a honeycomb sandwich panel. An insert was placed into the hole, and a sample of adhesive injected into the gap between the fastener and the hole using the MixPac system described above. The adhesive was then cured at approximately 70 F. (21.1 C.) for 48 hours, followed by 1 hour at 120 F. (48.9 C.). After cooling to 70 F. (21.1 C.), a rod was threaded into the machine screw portion of the fastener, which was then attached onto a jaw of the tensile tester. The maximum peak force, reported in lbs., required to dislodge the fastener was then measured at a pull rate of 0.05 inches/minute (1.27 mm/min.).

Density.

[0064] Density of the cured compositions was measured according to ASTM D-1622. Results are reported in grams/cm.sup.3.

Flammability.

[0065] Using the MixPac system, a silicone mold measuring 1.271.2712 cm was filled with Example 1, cured at 70 F. (21.1 C.) for 48 hours, then subjected to a flammability test according to 14 CFR 25.853(a)(i).

TABLE-US-00002 TABLE 2 Comparative Test Example 1 Example 2 Example 3 Cured Density 0.66 0.66 1.20 (grams/cm.sup.3) Extrusion Rate 140 20 145 (grams/mm) Compression Strength 5.3/36.54 NM 5.0/34.47 (Kpsi/MPa) Compression Modulus 250/1,723 NM 156/1,076 (Kpsi/MPa) Overlap Shear Strength 1.5/10.34 NM 1.5/10.34 (Kpsi/MPa) Tensile Strength Coupon 288/130.6 NM 270/122.5 Pull-Out (lb/Kg) Flammability Passed NM Passed NM = Not Measured

[0066] The material of Example 1 included the polyamine amide salt (BYK-W 966) and the low density fillers (D32/4500 Glass Bubbles and Dualite MS 700). In comparison to the material of Example 3, which included the polyamine amide salt but not the low density fillers, the material of Example 1 exhibits a weight savings (reduction in density) of 45% while retaining similar strength characteristics. The material of Comparative Example 2, which included the low density fillers but not the polyamine amide salt, was highly viscous and therefore not practicable.

[0067] Various modifications and alterations of this disclosure will become apparent to those skilled in the art without departing from the scope and principles of this disclosure, and it should be understood that this disclosure is not to be unduly limited to the illustrative embodiments set forth hereinabove.