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ENGINEERING HANDBOOK ADIPRENE/VBRATHANE CASTABLE ELASTOMERS
Transcript
Page 1: Engineering handbook

ENGINEERING HANDBOOK

ADIPRENE/VBRATHANE CASTABLE ELASTOMERS

Page 2: Engineering handbook

PREFACE Rubber, as a material of construction, is important to the engineer. When designing rubber products, he must utilize properties and use terminology that differ considerably from those pertaining to metals, concrete and plastics. Rubber is extensible and deforms easily, properties changing as the part is stressed. Knowledge of rubber properties and their interaction is essential in the design of parts. The first sections deal with each physical property of rubber as it exists at ambient conditions; the second sections shows how different environmental conditions influence and alter those properties. This information is required when specifications are written and products are designed. This series has been written from an engineering viewpoint and should be used in the design of products of ADIPRENE® urethane rubber. While a myriad of compounds can be produced, properties from specific polymers, at increasing incremental hardnesses, are presented for the sake of simplicity. Each property is discussed separately, but its relation to other properties should be considered. Compounding and processing conditions do have a significant effect on the physical properties of ADIPRENE. As with all elastomers, however, improvement in certain properties results in a change in others. For those not familiar with rubber technology, a short discussion of each property precedes the data. Definition of common terms used to describe rubber products, their compositions, and performance is included as a separate section.

INTRODUCTION The combination of many outstanding properties within a single material makes a urethane distinctive from conventional rubbers and plastics. In fact, one can consider urethane elastomers as a bridge between rubber and structural plastics because they combine many of the desirable properties of both. It would be more logical, however, to classify urethanes as a new kind of engineering material, rather than to approach their use in terms of prior experience with rubbers, plastics or metals. To achieve best results, the engineer should use ADIPRENE urethane rubber, not as a substitute for another material, but as new material with unique properties which permit him to take a new design approach. ADIPRENE urethane rubber is a thermosetting material characterized by unusual toughness. It combines resilience and high load bearing capacity with resistance to impact, abrasion and compression set and degradation by oxygen, ozone and oil.

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Page 3: Engineering handbook

In addition to the unique combination of properties distinguishing it from conventional elastomers, ADIPRENE also differs in its physical form. It is a liquid polymer which is mixed with a curing agent and can be fabricated by casting.

CLIMATIC CONDITIONS, TESTING AND MOISTURE EQUILIBRATION Water, liquid or vapor, are nearly always present and in contact with rubber parts in service. Therefore, it is important to know what effect water has on properties. The overall strength of ADIPRENE urethane rubber is reduced slightly when exposed to water. This is a reversible effect and properties are regained when parts are dried. ADIPRENE, a polyether urethane is very resistant to degradation by moisture upon long-term aging. Changes in atmospheric conditions, during mixing and after curing, do not cause significant changes in properties of ADIPRENE. Temperatures from 70°F to 90°F with 35% to 88% RH when mixing, and 70°F to 100°F with 20% to 90% RH when after-curing, have no effect on properties. Even with all of these ambient conditions, vulcanizates attain 90% of their ultimate properties within four days after being mixed, regardless of the processing conditions over the range listed, provided initial cure requirements are met. (RH – Relative Humidity)

All elastomers absorb moisture. The gain or loss in weight from 50% RH to equilibration at 100% and 0% respectively is plotted for three polymers of ADIPRENE in Figure 1. Approximately seven days are required to stabilize weight gain or loss of atmospheric moisture.

FIGURE 1WEIGHT CHANGE WITH HUMIDITY

-1

-0.5

0

0.5

1

1.5

0 25 50 75 100

Relative Humidity, %

Weight Gain,

%

Weight Loss,

%

Testing values can be altered considerably by humidity; therefore, comparisons should be made at the same humidity conditions. Humid service conditions can influence

properties and for that reason performance in static type applications. Dynamic applications usually generate heat within the part, tending to dry it and minimize the effects of moisture.

3

Page 4: Engineering handbook

The moisture content of urethane vulcanizates at equilibrium with the atmosphere varies about 2% as the relative humidity changes from 100% to 0%. How tensile strength

varies with relative humidity at 75°F is shown in Figure 2. A change in relative humidity from 50% to 100% produces a 25% reduction in the tensile strength of ADIPRENE® L-100.

Other properties, such as tear and abrasion, have lower values with increasing humidity. Equilibration of test specimens with humidity over the range of 0% to 100% RH causes a significant change in tensile strength and successively smaller changes in 300% modulus, 100% modulus and tear strength (Figures 3 and 4).

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Page 5: Engineering handbook

STATISTICAL METHODS

Statistical methods allow large amounts of data to be easily studied and interpreted. With statistics, it is possible to show how various properties relate to one another (for example, how the change in one property can affect others). Statistical methods are used to make predictions of future data from small amounts of existing data. The average, the range (high and low value) and the variation of each property are used to predict results of future data. One use of these techniques is the construction of production quality controls, where existing data are used to predict what proportion of future production will be within specification limits for designated properties. In order to have some degree of confidence that the analytical result closely represents what we wish to measure, it is necessary to examine the variables. Two of these are: method of testing the material samples; and the person doing the testing. In a large sampling, there might also be introduced differences between batches of material. If a number of samples are taken from a continuous operation, variation due to time might also be a source of error. There is also the possibility of equipment differences if all material is not produced (or tested) on the same equipment. Size of the samples should be large enough to detect the different sources of variation. If too small a sample is analyzed, important sources of variation might not be observable. The standard deviation is one of the most commonly used indications of the degree of variability in a sample. It measures the spread of data around the central value. Standard deviation, usually represented by the Symbol ∆ is in the same units as the original data and has a direct interpretation in terms of the graphical representation of the observations. The value of every item in the sample affects the standard deviation. Greater weight is placed on the extreme values because of their deviation from the average. About 70% of the items in a normal sample lie within the range defined by the average ± one standard deviation and about 95% will lie within the range defined by the average ± standard deviations. Values for future data being within ± 2 standard deviations of the average of the known data are said to be the same as the known data with 95% confidence. An analysis of a small production run of ADIPRENE L-100 is used as an example. The statistical methods just discussed were used to describe some physical properties. Results of this analysis were: PROPERTY

SPECIFICATION LIMITS

AVERAGE VALUE

RANGE OF VALUES

STANDARD DEVIATION

Tensile Strength, psi 3000 Min. 3420 2620-4520 450 Elongation, % 450 Min. 620 480-690 40 100% Modulus, psi 750-1250 1040 754-1110 40

5

Page 6: Engineering handbook

From this information, Figures 5, 6, and 7 were prepared showing the probable limits of future production. Provided future production methods remain the same, 70% of production should be within one standard deviation of the average and 95% of production should be within two standard deviations of the average. Three standard deviations would encompass 99.8% of all production. From a practical standpoint, this can be considered to 100%. If specifications exist for the material being tested, the statistics above will enable an estimation of how much production will meet or exceed specification. In the production run, 17.5% of production can be expected to be below the 3000 psi specification minimum. All production would be above the minimum elongation of 450%, and all production would be within the specification limits for 100% modulus.

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Page 7: Engineering handbook

The samples used in the analysis were from different batches of material. Slabs from each batch were tested using a number of dumbbells from each test slab. Results were as follows:

∆B ∆S ∆t Tensile I I 445.0Elongation I 38.5 20.5100% Modulus I I 42.7

∆ I = Statistically insignificant when compared with experimental error ∆ B = Difference between batches ∆ S = Difference between slabs (within batches) ∆ t = Testing error – difference between dumbbells (within slabs) Except in the analysis of elongation, where statistically significant differences appear between slabs, most of the differences were due to testing error. The effect of changes in property can be illustrated by the following graphs. These show the influence of additional samples. Figure 8 indicates that, as tensile and/or elongation value increase, 100% modulus values decrease. This graph was plotted from batch data only and has few points. More points, from slab data, are used in the construction of Figure 9. The direction of the curves is similar, with an area of minimum 100% modulus appearing. This indicates that after certain values of either tensile or elongation are reached, 100% modulus values start to increase. Little change from slab data is observed when all points are graphed (dumbbells) in Figure 10. Figure 9 and 10 are very much the same. Therefore, more information is gained from adding the necessary points to graph the slab data; but little additional information is obtained when dumbbell data are included in the study.

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9

SECTION I PHYSICAL PROPERTIES

TYPICAL PHYSICAL PROPERTIES ADIPRENE polymers can be cured to a tough, rubbery, solid by reaction of the isocyanate groups with polyamine or polyol compounds. ADIPRENE polymers offer the best properties when cured with MBCA curing agent. Typical vulcanizate properties for all the ADIPRENE polymers are shown in Table 1.

Page 10: Engineering handbook

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TABLE 1 TYPICAL PHYSICAL PROPERTIES

COMPOUND L-42 L-83 L-100 L-167 L-200 L-213 L-315ADIPRENE 100 100 100 100 100 100 100MBCA 8 10.3 12.5 19.5 23.2 25 26Mix Temperature, °F (°C) 212 (100) 212 (100) 212 (100) 185 (85) 185 (85) 150 (66) 150 (66) Cure, Min. at °F (°C) 60/212

(100) 60/212 (100) 60/212 (100) 60/212 60/100 60/212 60/212

Post Cure Hr. °F (°C) 16/158(70) 16/158(70) 16/158(70) 16/158(70) 16/158(70) 16/212 16/212 Hardness, Durometer A 80 85 90 95 - - - Hardness, Durometer D - - - 48 58 73 73 100% Modulus, psi 400 700 1000 1800 3000 3900 4650 300% Modulus, psi 625 1200 2100 3400 7800 - - Tensile Strength, psi 3000 4400 4500 5000 8300 8800 9000 Elongation at Break, % 800 580 450 400 320 240 210 Tear Strength, Split, 1 lb./in. 70 85 75 150 135 145 110 Abrasion Resist NBS Index, % 110 200 175 300 370 500 400 Compression Set, Method B 22 hrs. at 158°F

45

35

27

40

40

-

-

Compression Set, Method A 22 hrs. at 158°F, 1350 psi

-

-

9

10

-

30

10

Resilience – Yerzley, % 70 - 65 - - - - Resilience – Bashore, % 60 50 45 40 - 50 45Specific Gravity 1.075 1.08 1.10 1.13 1.14 1.19 1.21 MBCA is an acronym for 4,4’-Methylene-bis-(2-chloroaniline).

Page 11: Engineering handbook

11

HARDNESS

Page 12: Engineering handbook

HARDNESS Hardness, as applied to elastomers, is defined as the relative resistance of a surface to indention by an indenter of specified dimension under a specified load. The most commonly used measuring instrument is a durometer. Numerical hardness values are derived from the depth of penetration. The harder the sample, the further it will push back the indenter point and the higher the readings. On the durometer A scale, 0 is very soft, and 100 is infinitely hard. Values are usually read immediately after firm contact has been established. The hardness range of elastomers is so broad that a single durometer cannot indicate practical measurable differences of hardness. For this reason durometers are available in more than one scale model, (e.g., A and D scale durometers). The A scale durometer is widely used throughout the rubber industry. The durometer D model, which has a stiffer spring and a more pointed indenter, is used to measure the hardness of hard rubbers. Mechanical limitations of durometers and the way people use them cause hardness measurements to be inconsistent. It is not uncommon to find a difference of 5 points in individual hardness readings of an elastomer specimen. Table-top durometers can measure hardness more accurately, but they are not as convenient and are not used routinely. Frequently, hardness is assumed to correlate with stiffness (modulus), but this is not always true. Variations of a few points in hardness can show a marked difference in compression-deflection. A statistical determination has been made of the relationship between hardness and 100% modulus of Adiprene measured with durometers on the A and D scales. As expected as shown in Table II, the A scale is more reliable for predicting the modulus of the softer stocks; the D scale should be used with the harder stocks. The values in Table II are graphically shown in Figures 1 and 2.

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13

Typical hardness values for Adiprene vulcanizates are: Vulcanizate Hardness Adiprene Polymer Curing Agent Durometer A Durometer D

L42 MBCA 78-80 - L-83 MBCA 83-85 - L-100 MBCA 88-93 40 L-167 MBCA 93-07 45-50 L-200 MBCA - 55-60 L-315 MBCA - 70-75 L-213 MBCA - 70-75

TABLE II

CORRELATION BETWEEN MODULUS AND HARDNESS

Hardness A

95% Confidence

Limits

Average 100%

Modulus psi

Hardness D

95% Confidence

Limits 55 105-205 150 - - 60 140-265 200 10 175-275 64 180-330 250 14 195-330 68 210-400 300 18 240-400 73 295-530 400 23 315-520 77 365-650 500 27 390-630 80 430-795 600 31 480-760 83 500-910 700 34 560-880 86 580-1060 800 36 630-1000 88 645-1200 900 38 700-1120 90 700-1350 1000 40 760-1250 92 800-1550 1150 43 900-1400

1500 49 1200-1900 2000 55 1650-2500 2500 59 2000-3100 3000 63 2400-3800 4000 69 3200-5100 5000 73 3900-6400

The reliability of predicting modulus from either A or D scale is approximately ± 33%, for 95% confidence limits. In the low modulus range of less than 500 psi, predictability is 25%. The A scale should be used with moduli of 500 psi and under. The D scale is more useful for predicting moduli of more than 1000 psi. Either scale may be used for the intermediate areas as in Table II. One hundred per cent modulus an be predicted to within ± 115 at a level of 400 psi, ranging up to ± 315 at 1150 psi using the A scale predictability ranges from ± 100 at 400 psi to ± 1200 at 5000 psi.

Page 14: Engineering handbook

A linear relationship between durometer A and D does not exist. Approximate equivalent readings for durometer A and durometer D are shown in Table III. Because of differences in indenter tip shape difference between A and D readings can vary widely for different materials.

Hardness above 95 on the A scale should not be specified because the upper accuracy limit of the instrument is being approached. Accuracy at the lower end of the D scale is also limiting and values below 25D are questionable. Most Adiprene compositions lie between durometer 58A and 75D as shown in Figure 3. No other types of rubber offers unique properties over this hardness range. Intermediate hardnesses can be made by

blending polymers. Softer polymers can be made by incorporation of plasticizers, changing curing agents, or by making cellular products.

TABLE III APPROXIMATE HARDNESS EQUIVALENTS

Durometer A Durometer D 50 - 60 - 70 18 75 25 80 30 85 35 90 40 95 48

Except where otherwise noted, the information contained herein is based on a limited amount of our own laboratory work, employing small-scale equipment but following generally known trade practices. Although this information is believed to be accurate, these limitations must be kept in mind, because use of different conditions or equipment might product different results. Because we cannot anticipate all variations in manufacturing equipment and methods, our products discussed herein are sold without warranty, express or implied, as to the results the user may obtain with them, and on the express understanding that purchasers will make their own tests to determine for themselves the suitability of such products for their particular purposes. Moreover, any statements herein concerning possible uses for our products are not to be considered a recommendation to use these products in the infringement of any patent.

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Page 15: Engineering handbook

15

STRESS STRAIN

Page 16: Engineering handbook

STRESS-STRAIN

Tensile strength and ultimate elongation, while sometimes useful for compound development and control are of lesser importance to the design engineer. Elastomeric parts are seldom loaded in tension and then only to a small fraction of their ultimate strength or elongation. Tensile strength and elongation generally cannot be correlated with performance in service. The relationship of stress to strain is more useful because it shows how an elastomer responds to loading.

Tensile Strength is the force per unit of the original cross-sectional area which is applied at the time of the rupture of a specimen. Elongation or Strain is the extension between bench marks produced by a tensile force applied to a specimen and is expressed as a percentage of the original distance between the marks. Ultimate elongation is the elongation at the moment of rupture. Modulus is the stress in pounds per square inch (of original cross-section) required to produce a certain elongation.

If a tensile stress of 1800 psi produces an elongation of 300%, the compound is said to have a 300% modulus of 1800 psi. In rubber, unlike steel, stress and strain in tension are not proportional; and, therefore, the term modulus has a different meaning. When applied to steel, modulus is stress divided by strain – a ration and a constant. Applied to rubber, modulus means stress at a certain strain – not a ratio and not a constant, merely the coordinates of a point on the stress-strain curve. Procedures for conducting stress-strain tests are standardized and described in ASTM D-412. Dumbbell shaped specimens four or five inches long are die-cut from flat sheet and marked in the narrow section with bench marks one and two inches apart (Figure 1). Ends of the specimen are placed in the grips of a testing machine (Figure 2). The lower grip is power driven at 20 inches per minute and stretches the specimen until it breaks.

Figure 1 Standard Tensile Test Specimen

Figure 2 Testing Machine

As the distance between bench marks widens, measurement is made between their centers to determine elongation.

16

Page 17: Engineering handbook

Stress-strain properties are useful in compound development and for manufacturing control. As control tools, stress-strain properties reveal whether or not the ingredients have been mixed properly or if contaminants are present. Property changes by environmental conditions are easily detected by a change in stress-strain properties. For a product which has been put in production, modulus and elongation measurements can be used as quality control tools. They are sensitive to manufacturing variations and indicate if the product has been properly processed.

Natural rubber must be loaded with carbon black to obtain a modulus approaching that of Adiprene urethane rubber with no filler (Figure 3). Tensile stress-strain curves for compounds of Adiprene are shown in Figure 4. The tensile strength of commercial compositions of Adiprene L will vary from 2000 psi to over 11,000 psi. Elongation will vary from 250% to 800%. Generally, tensile strength increases with an increase in hardness. Figure 4 also shows that Adiprene elastomers retain extensibility at high hardness. Elongation at break of a 75 durometer D, achieved with Adiprene L-315 vulcanizates, is usually 250%.

The response of materials at low moduli is more important to the design engineer than the ultimate tensile strength. As show in Figure 5, tests from the same material can yield widely varying tensile strengths based on small differences in elongation. In this case, an elongation at break of only 50% can result in a 2200 psi change in tensile strength. The variability in tensile strength can be due to small voids in the specimen or a small invisible nick in the sample. Stress at 100% modulus yields very consistent results and are reproducible compared to other tensile properties.

17

Page 18: Engineering handbook

The stress-strain properties of many elastomeric compounds change with the addition of a reinforcing filler. Modulus and tensile values can increase significantly. Amine-cured Adiprene without filler has a stress-strain curve which closely resembles filler-reinforced elastomers (Figure 6). Polyol-cured Adiprene does not have this change with reinforcement. In many non-rubber materials, Young’s modulus may be taken in tension or compression, the value being approximately the same; it is the ratio of stress to strain, expressed in psi per unit strain. In rubber, the assumption that tension modulus equals compression modulus is valid only for extremely small deformation and for certain shapes, such as specified in ASTM D-797, “Young’s Modulus in Flexure of Natural and Synthetic Elastomers” and ASTM D-1053, (Sec/ 7) “Measuring Low-Temperature Stiffening by the Gehman Torsional Apparatus”. Modulus of elasticity in tension for three vulcanizates of Adiprene L with MBCA are given below. The values given are the slopes of the stress-strain curves, as near to the point of origin as could be measured and should be considered only approximate. The values were measured at 72°F (22°C).

ADIPRENE L-100 7,000 psi ADIPRENE L-167 11,000 psi ADIPRENE L-315 52,000 psi

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19

COMPRESSION

AND SHAPE FACTOR

Page 20: Engineering handbook

COMPRESSION AND SHAPE FACTOR

When a load is applied to an elastomer, it “flows” in accordance with the force exerted on it and within the limits provided by the mass of the material itself or by the dimensions of its container. In rubber technology this is called compression. Although this term is correct in the framework of normal rubber usage, it may be misleading to the engineer. It does not mean that the elastomer will undergo a change in volume under pressure. Rather, it means the elastomer will deflect, or undergo a change in shape. This distinction is important. An elastomer is an incompressible fluid, capable of changing its shape to the limit of its strength under load. It will react to a load placed upon it by tending to exert force uniformly in all directions. This is illustrated in Figure 1.

Even though the elastomer is changed in shape under load, it is compelled by the characteristic of elasticity to return to its original shape once the load is removed. Compression strain can be considered to be extensions of tensile strain which are continuous through the origin. However, the compressive samples must be free to move, i.e., the faces must be lubricated. Generally, rubber in compression is bonded to the surface or surface friction restricts movement. Compression curves are usually smooth and do not exhibit the “S” shape usually found in tensile tests. Compressive strain (Figure 2) is limited to less than 100% and, therefore, the curve becomes asymptotic to the 100% line.

20

While the ability to deform under compressive stress and then recover is a characteristic property of elastomers, other factors, notably the shape of the part, affect the way an elastomer deforms in compression. To illustrate, consider two blocks cut from the same piece of rubber. One is a cylinder with the proportions of an ice-hockey puck, the other is a block of the same height and cross-sectional area, but rectangular in shape.

Page 21: Engineering handbook

If equal weights are placed on the blocks, subjecting them to the same compressive stress, the rectangular block will deflect more than the cylinder (Figure 3).

21

Since the blocks will not change in volume, the reduction in height is caused by the freedom of the sides to bulge. The rectangular block deflects more than the cylindrical one because the sides of the rectangular block provide a greater area free to bulge. The designer of elastomeric parts allows for this behavior by using a concept called shape factor. Shape factor describes the roll of the shape in determining how a part with parallel load faces will behave under compressive forces. The concept of shape factor is useful for the design engineer. If the elastomeric part does not deflect enough to do its job, the designer can reduce the

shape factor by increasing the thickness of the pad. In reality, he does no more than increase the area free to expand under load. If the pad deflects too much, he may decrease the area free to expand or he may increase the hardness of the elastomer.

URETHANES IN COMPRESSION

Urethane elastomers have higher load bearing capacity than do conventional and elastomers of comparable hardness. This permits design of smaller parts, with possible savings in weight and materials cost. Compression-deflection curves for Adiprene L and natural rubber vulcanizates of equivalent hardness (80 durometer A) are compared in Figure 1. This figure illustrates that urethanes can be loaded beyond conventional limits for rubber. Adiprene L-100 has sustained short-term loadings of greater than 20,000 psi and Adiprene L-167 has been loaded to 68,000 psi without fracturing.

Page 22: Engineering handbook

EFFECT OF LOAD SURFACE CONDITIONS When an elastomeric piece is compressed between parallel plates, the surfaces in contact with the plates tend to spread laterally, increasing the effective load bearing area. If this lateral movement of the surface is restricted, the compression-deflection behavior of the piece is changed. Restriction of lateral movement greatly stiffens the part.

22

Figure 2 illustrates this effect quite clearly. A lubricated surface offers essentially no resistance to lateral movement. Lubrication at the metal-rubber surface may excessively strain the part because extreme deformation may occur. A clean, dry loading surface offers some resistance due to friction; if the surface is bonded to the metal plates, no lateral movement is possible and insures reproducible compression values. These differences in contact surface result in three distinct compressive stress-strain relationships for the same piece of rubber. The load bearing capability of Adiprene can be altered by a factor of 5 to 1 by changing the surface conditions.

EFFECT OF SHAPE Shape factor is defined as the ration of the area of one loaded surface to the total area of the unloaded surfaces which are free to bulge. Parts made from the same compound and having the same shape factor behave identically in compression, regardless of actual size or shape. Effective use of compression-deflection data is dependent on knowledge of test conditions under which the data were taken. The values presented are for normal room temperature and static or slow speed operation. Other temperatures and dynamic loadings would change these values completely. Shape factors below 0.25 may permit buckling; therefore, higher shape factors should be used. As shape factor increases, the unit load required to product a given strain also increases. There is, however, no mathematical relationship between shape factor and compressive modulus; the relationship must be determined empirically. Figures 3 and 4 show compression-deflection curves for Adiprene L urethane rubber covering a range of hardnesses and shape factors. These curves were obtained with bonded surface. The compression-deflection characteristics of a fabricated item of a particular hardness may vary up to ± 10% from the curves down. Deviations arise primarily from inaccuracies in measuring hardness of an elastomer compound.

Page 23: Engineering handbook

Deformations are usually limited from 15% to 25%, which is the predictable straight line portion of the shape factor curves. Deformations above 25% impose higher stresses which induce much higher set and increase creep in the part.

23

Page 24: Engineering handbook

USE OF COMPRESSION STRESS-STRAIN CURVES IN DESIGN The following examples show how the compression stress-strain curves can be used in the design of urethane parts. Shape factor for blocks and cylinders is calculated as follows: For rectangular shaped prisms:

)w1(t2

w1factorShape+

=

where: l = length w = width t = thickness d = diameter h = height For discs and cylinders:

h4

dfactorShape =

This relationship is limited to the following: 1. pieces which have parallel loading faces; 2. pieces whose thickness is not more than twice the smallest lateral dimension; and 3. pieces whose loading surfaces are restrained from lateral movement

EXAMPLE 1

Problem: Assume a pad 8 inches square by 1 inch thick, made of 70 durometer A, Adiprene L-100. How much will the pad deflect under 1000 psi compression stress?

Solution: (a) The shape factor of the piece is:

23264

)88()1()2(88

areaelgbufreetotalareasurfaceloadedone

==+

=

(b) In Figure 3 we find that the compressive stress-strain curve of a 70A durometer

urethane part with a shape factor of 2 crosses the 1000 psi stress abscissa at 11% strain. Therefore, the pad will deflect 11% of one inch or 0.11 inch.

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EXAMPLE 2 Problem: What happens if the pad thickness is doubled in Example 1? Solution: (a) Shape factor of the piece is now:

16464

)88()2()2(88

==+

(b) From Figure 3, the compressive strain at 1000 psi stress for a 70 durometer A part with a shape of 1 is 25%. In this case, the pad will deflect 25% of two inches, or 0.50 inch. (In practice, parts made of conventional elastomers are generally designed so that compressive strain does not exceed 15%).

EXAMPLE 3

Problem: Assume a pad which is one inch square by one-half inch thick and bears a 2500 lb.

compressive load. The pad may not deflect more than 0.05 inches because of space limitations. What hardness Adiprene vulcanizate should be specified?

Solution: (a) Shape factor of the piece is:

5.021

)11()2/1()2()1()1(

==+

(b) Unit compressive stress is:

psi2500)1()1(

2500=

(c) Compressive strain is:

%10100X5.0

05.0=

(d) On scanning the compressive stress-strain curves we find in Figure 4 that

vulcanizates which are 60d hard or harder will bear a compressive stress of 2500 psi with 10% or less deflection.

25

Page 26: Engineering handbook

As a general rule, the harder the elastomer, the greater its loading bearing capacity. The manner in which load-bearing properties of Adiprene change with hardness at various deformations is shown in Figures 5 through 7.

26

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27

COMPRESSION SET, CREEP

AND STRESS RELAXATION

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28

COMPRESSION SET, CREEP AND STRESS RELAXATION

Compression set, creep and stress relaxation are related to the fluid characteristics of elastomers. Set is defined as the deformation remaining after removal of the deforming stress. Creep involves the increase in deformation with time under constant stress. Stress relaxation is the decrease of stress with time at a constant deformation. COMPRESSION SET Compression set tests, described in ASTM-D-395, are of two main types: Method A, compression set under constant load; and Method B, compression set at constant deflection of 25%. In Method A, specimens of standard dimension are compressed between parallel steel plates under a stress of 400 psi. The test assembly is then conditioned for a selected time at the selected test temperature (such as 22 hrs. at 158°F - 70°C) after which the specimens are removed and allowed to recover at room temperature for 30 minutes. Compression set is the difference between the original thickness of the specimen and the thickness after test, expressed as a percentage of the original thickness. In determining compression set by Method B, the specimen is compressed to 75% of its original thickness. The test assembly is then conditioned for the specified time at the selected test temperature. Compression set determined by Method B is the difference between the original thickness of the specimen and the thickness after testing, as a percentage of the deflection employed. Although the conditioning time and temperature are specified in the ASTM standard, other times and temperatures are frequently used. Compression set is applicable particularly to the compounds used in machinery, motor mountings and vibration damping. Compression set tests are intended to measure the ability of elastomeric vulcanizates to retain elastic properties during the prolonged action of compression stresses. The actual stressing in service may involve (1) the maintenance of a definite deflection, (2) the constant application of a known load, or (3) the rapidly repeated deformation and recovery from compression forces. There are applications where the temperatures and deformation conditions used in the permanent set test are approximated in actual service. These instances, where apparent similarity exists, have led to a widespread tendency to over-emphasize permanent set values. Since the short testing time will never approach the much greater span of desired service life, the test values will only suggest, not predict, what may be expected in service. For example, it is often thought that low compression set is always accompanied by high resilience and low creep. While trends of this type may be evident when considering extreme values for compression set, there are so many exceptions that acceptance of the general statement does more harm than good. Typical compression set values for Adiprene are shown in Table I. Lowest compression set is usually obtained with 90-95% theory MBCA curing agent.

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TABLE I COMPRESSION SET OF ADIPRENE AT VARIOUS HARDNESSES

Compound Hardness A 80 85 90 95 - - - Compound Hardness D

-

-

-

48

58

73 (L-213)

73 (L-315)

Compression Set Method B 22 Hours at 158°F

45

35

27

40

40

-

-

Compression Set Method A 22 Hours at 158°F

-

-

91

102

-

302

102

(1) @ 400 psi (2) @1350 psi CREEP When subjected to load, all elastomers exhibit an increasing deformation with time, known as creep or strain relaxation. This occurs at any stress level and takes place in compression, tension and shear loadings and varies for each type of loading. In service, creep can be minimized by using low working stresses and avoiding high temperatures. No rapid method has been developed for its measurement because there is no known way of accelerating time effects without introducing inaccuracies in predicting rate of creep. Creep is usually expressed in percent of deformation after the part is loaded rather than the unloaded dimension. Determination of creep takes place after some arbitrary short time interval such as one minute, five minutes or even one day after applying the load. Creep, expressed as a percent, equals total deformation minus initial deformation divided by initial deformation times 100. In the initial stage, creep occurs at a relatively high rate and then continues at a very slow rate.

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Failure can occur after an extended period of high stress. Figure 1 illustrates characteristic creep curves. AB in the high stress creep curve indicates the failure phase where actual fracture can occur. Below the failure zone, when stress is removed, the part will attempt to return to its original dimension; however, it will never fully recover. The unrecoverable portion is called permanent set. Loads will allow intermittent recovery will exhibit less creep than if continuously loaded. However, continuous vibratory loading will increase creep since internal heat is generated.

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Strain relaxation is important in applications such as engine mountings since it influences the alignment of various parts of the equipment. Yet, it is difficult to predict these properties for a given application without resorting to simulated service tests because several factors have an important effect on them. Chief among these are amount of strain, operating temperature and changes in these two resulting from vibration. The relative effects of variables have not yet been correlated so that results of tests under one set of conditions will permit accurate prediction of creep under another set of conditions. It has been established that the higher the initial strain, the higher the creep; also, the higher the temperature, the higher the creep. In general, the degree of creep is dependent on the type of strain. Creep is greater under tension strain than under equal compression strain. Creep is also increased more under dynamic loading than under static loading because of internal heat generation.

The creep characteristics of two Adiprene polymers, over a ten-month period, are shown on Figure 2. After approximately 3000 hours (18 weeks) creep reaches a plateau and becomes almost constant. The amount of creep is a function of stress level. This involves a stress of 400 psi. Creep will continue at a very low rate after this point, which is the classic behavior of elastomers. The actual creep of the 95 durometer A compound was 0.033 inches after ten months compared with an initial deflection of 0.200 for a sample 0.500 inches thick. After the initial loading, creep is only 6.6%.

The creep rate of rubber materials of all kinds increases at elevated temperatures. Where dimensions are important, operating temperatures must be kept below 150°F (66°C).

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STRESS RELAXATION Stress relaxation is the loss in stress when it is held at a constant strain over a period of time. It is usually expressed in terms of percent stress remaining after an arbitrary length of time at a given temperature. It is an important property where a given level of force or tension must be maintained over a long time, such as in seals of various types. There is no standard method for determining stress relaxation. However, many laboratories have developed relaxation cells. These cells utilize compression set specimen and the test procedure parallels ASTM D-395 Method B. Stress relaxation for Adiprene L-100 is shown in Figure 3 and Figure 4.

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RESILENCE

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RESILENCE

Resilience is defined as the ratio of energy given up in recovery from deformation to the energy required to produce the deformation, usually expressed in percent. Hysteresis is the percent energy loss per cycle of deformation. Hysteresis is the result of internal friction and is the conversion of mechanical energy into heat. Heat build-up is measured as the temperature rise resulting from hysteresis. In general, resilience is determined in one of four ways – from a low speed stress-strain loop, by impact tests, by free vibration or forced vibration methods. Low Speed Stress-Strain is obtained by loading and unloading a specimen in tension, compression or shear using a low rate of strain and large deformation. Since most practical applications involve vibratory stresses of relatively high frequency and low amplitude, the low-speed stress-strain loop is not often used for measuring hysteresis.

The most widely used methods for measuring resilience by impact involve rebound in some form. A very simple test consists of dropping a metal plunger from known height onto a firmly supported rubber specimen and measuring the height of rebound, as with the Bashore Resiliometer (Figure 1). An impact test, however, is not equal to a vibration test since there is no cyclic interchange of potential and kinetic energy. A widely used instrument that measures vibratory resilience is the Yerzley Oscillograph. This instrument is popular because it involves a relatively high speed deformation (many times faster than a stress-strain loop, although considerably slower than with impact resilience tests) through one or more complete vibration cycles and yields precise and reproducible data. However, the frequency is not the same order of magnitude as that of many applications involving vibration.

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Free Vibration Technique can use the Yerzley Oscillograph, which makes use of an unbalanced horizontal lever which strikes a cylindrical specimen of rubber and traces the resultant motion on a chart (Figure 2).

Since the chart is mounted on a revolving drum, the trace has the form of a sine wave as shown in Figure 3.

The apparatus consists of a balanced beam supported on knife edges, with weights which are added to one end to strain the specimen on the opposite side of the knife edges. When the weights are released, a trace of the damping curve is automatically recorded. No significant test values can be obtained on materials which have a moduli greater than 280 psi in compression with 10% deformation. Yerzley tests are, therefore, limited to the softer urethane rubbers (Durometer 90A or below). The Bashore rebound test can be used on rubber of all hardnesses, but does not yield results which are as precise and distinguishing as Yerzley resilience. Impact may cause a rise in temperature resulting from heat generated within the specimen. Resilience is a function of temperature and usually increases when rubber is heated. Forced vibration methods may be used to measure resilience, but they are usually employed to determine heat build-up in the specimen. Three flexometers described in ASTM D-623 are most commonly used for this measurement. These are known as Goodyear, Firestone and St. Joe Flexometers. They are most frequently used to compare various compositions with one whose performance has been determined by actual use. There is a tendency to assume that a composition having high hysteresis will be unsatisfactory for almost any use. This is not necessarily true. In certain vibration damping applications, compounds having relatively low resilience may be desirable because their damping effect limits the maximum amplitude which may develop in service.

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For vibration damping purposes, resilience requirements are determined largely by the frequency and amplitude of vibration. Hysteresis in a low resilience compound would cause excessive heat build-up in the part. In this case, a highly resilient composition should be used. Damping refers to the reduction amplitude in a free vibration system. Damping is a result of hysteresis and the two terms are frequently used interchangeably. Heat generation measured by the temperature rise, or the equilibrium temperature, for a sample under forced vibration at non-resonance is more nearly related to the requirements of actual service than is resilience. The temperature rise at a given amplitude depends upon both the resilience and the compression/deflection of the rubber compound. The resilience determines the proportion of the vibrational energy which is converted into heat, but the actual value of the vibrational energy at a given amplitude is proportional to the dynamic modulus. EFFECT OF AMPLITUDE AND OF FREQUENCY ON VIBRATION PROPERTIES If there is no appreciable rise in temperature of the rubber, the dynamic modulus and dynamic resilience are independent of frequency for the ordinary range of mechanical frequencies. Any rise in temperature of the rubber due to internal heat generation will increase with frequency, tending to lower the dynamic modulus and raise the resilience. The dynamic properties of gum compounds are usually not affected by amplitude; but with filled compounds, the dynamic modulus decreases with the increase in amplitude even if the temperature in the rubber is constant. Any rise in temperature contributes to this effect. Resilience is not affected by the amplitude except indirectly by temperature changes. The resilience of Adiprene and natural rubber of 60 Durometer A hardness over the temperature range of 0 to 250°F (-18°C to 121°C) are compared in Figure 4. The resilience of Adiprene urethane rubber increases as temperature is increased from 0 to 50°F (-8°C to 10°C) and then becomes almost constant. Being almost constant permits more confidence in design where service temperature may vary considerably. Heat build-up in urethane parts, under high frequency flexing, exceeds that of conventional elastomers and is the usual cause of premature failure under dynamic conditions. Because of the low thermal conductivity of urethane elastomers, heat developed by internal friction cannot readily be dissipated. The effect of heat build-up is, therefore, a very important consideration when designing with urethanes. Its adverse effects can be minimized by using thin cross-sections from which heat is more easily dissipated. The high strength and load bearing capacity of urethane elastomers makes possible the use of sections which are thin enough to dissipate heat at the same rate at which it is developed.

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Values of resilience for typical compounds of Adiprene are shown in Table I.

Table I

Resilience of Adiprene Adiprene Hardness Yerzley Resilience Bashore Resilience Durometer A 58 72 – 75 70 60 80 70 60 85 65 – 90 65 45 95 – 39 Durometer D

58 – 72 48 75 50

Compared to natural rubber over a hardness range of 55A to 85A (Figure 5), Adiprene shows little change in resilience.

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Adiprene urethane rubbers can be formulated to exhibit high or low resilience. Yerzley Oscillograms of compounds having high and low resilience are shown on Figure 6.

Adiprene provides a greater hardness range with less sacrifice in resilience than many types of elastomers. This is a characteristic because urethanes are non-reinforced while rubber requires the use of fillers to develop optimum properties.

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37

TEAR RESISTANCE

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TEAR RESISTANCE

Tear resistance is a complex result of other basic properties, such as modulus and tensile strength. Many laboratory methods have been devised to measure this property. The tests now being used to measure the tear resistance of elastomers are useful for laboratory comparisons, but correlation between test results and service performance is often quite difficult. The various tests produce different results when used with Adiprene urethane rubbers. The following tear tests for Adiprene have been compared:

ASTM D-470 Instron Split Tear

ASTM D-751-52T (Modified Trapezoid) ASTM D-624 Die C (Graves)

ASTM D-624 Die B (Winkelmann) ASTM D-1938 (Trousers)

ASTM D-470, D-1938 and the Instron split tear tests dependent on tensile strength and give the most realistic evaluation of the tear strength of Adiprene. Specimens used in each test are shown in Figure 1. The D-1938 is similar to the Instron Tear. Tear test results for compounds of Adiprene of varying hardnesses are listed in Table 1.

TABLE 1 A COMPARISON OF TEAR TESTS FOR VULCANIZATES OF ADIPRENE

COMPOUND

Adiprene L-100

Adiprene L-167

Adiprene L-213

Adiprene L-315

ADIPRENE L 100 100 100 100 MBCA 11 20 26.6 26.9 Mix Temperature, °F (°C) 212 (100) 212 (100) 150 (66) 150 (66) Cure Temperature, °F (°C) 212 (100) 212 (100) 212 212 Cure Time, Min. 60 60 60 60 Postcure, Hrs. @ °F (°C) 16/158(70) 16/158(70) 16/212 16/212 VULCANIZATE PROPERTIES Hardness, Durometer A 90 95 — — Hardness, Durometer D 43 53 73 73 Tensile Strength, psi 4500 5000 7500 7500 Tear Strength lb./min. Graves, 20 in./min. 1 in./min.

400 —

500 —

753 389

1000 810

Winkelmann, 20 in./min. 1 in./min.

368 —

517 —

1525 384

1075 1000

ASTM D-470, 20 in./min. 75 150 145 110 Instron, 20 in./min. 1 in./min.

73 —

234 —

— 173

220 165

Trapezoid, 20 in./min. 130 917 ** ** **No test, too stiff to fold.

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Results are computed in terms of force per inch thickness required to tear the specimen. For example, if a load of 40 lbs. is necessary to tear a specimen 0.07 inches in thickness, the tear resistance would be:

inchper.lb572070.040

=

Graves (Die C) and Winkelmann (Die B) tear values increase with increasing hardness. The absolute values obtained with these tests are high, since the test depends to a large extent on tensile factors. For some of the harder compounds, slowing the head speed from 20 inches per minute to one inch per minute permits the sample to relax during the test; this reduces the effect of tensile strength, resulting in lower values for both tests. For example, Adiprene L-213 urethane rubber pulled at 20 inches per minute gives a tear strength which is much greater than that obtained by pulling the same compound at one inch per minute. Adiprene L-315 shows less tendency to relax than Adiprene L-213, and yields Graves and Winkelmann values which are most independent of testing speed over the range studied. ASTM D-470 and Instron test values increase with increasing hardness for Adiprene L-100 and Adiprene L-167, but are lower for Adiprene L-213 and Adiprene L-315 even though these compounds are harder. Absolute values from these two tests are similar and are the lowest of all the tests studied. Both tests are split tear tests, which tend to eliminate tensile factors and give a more realistic evaluation of cut growth resistance. These tests appear to be the best available measure of the tear resistance of Adiprene. The Trapezoid tear test values increase with hardness, with a large increase for Adiprene L-167. In the Trapezoid test, mainly used to test rubber coated fabrics, the entire stress is placed at the initiation of tear, in a direction perpendicular to the direction of tear. This eliminates the “doubling back” and shear effects associated with split tears and tensile effects found in Graves and Winkelmann tests. The Trapezoid test is a useful complement to the other tear tests, but it cannot be used for hard compounds (e.g. Adiprene L-213 and Adiprene L-315) because it is difficult to fold the sample properly.

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Tear strength of Adiprene L-100 and Adiprene L-167 urethane rubber can be enhanced by use of MBCA levels at 100 to 110% of theory. This improvement is illustrated in Figures 2 and 3.

The increase in tear strength is attributed to making the polymer chain more linear with less crosslinking. An excellent discussion on tear strength may be found in Rubber Chem. And Tech., Volume 33, Pages 1438-1481 (1960). This is a translation of a series of articles by Kainradl and Handler which appeared in Kautchuk and Gummi, September, October and November, 1959.

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ABRASION RESISTANCE

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ABRASION RESISTANCE There are two types of abrasion – sliding and impingement. Sliding is the passing of an adjacent surface across the rubber surface. Impingement is wearing of the rubber exemplified by sand particles hitting the surface. Most wear in actual service occurs as a combination of both sliding and impingement. When sliding, localized friction forces can impose high energy levels on the rubber. Abrasion and wear takes place when the rubber cannot withstand these forces. Impingement by particles occurs in applications such as chutes, rebound plates and sandblast hoses. Elastomers can yield easily and distribute stresses imposed by particle impingement. A sandblast test shows that with a 90°C impingement angle, soft resilient rubber is more abrasion resistant than steel or cast iron. However, not just any elastomer can be used. Under this same condition, a tough tire tread will wear out more rapidly than a soft elastomer. The angle of particle impingement has a significant effect on which material should be used. Laboratory abrasion tests are difficult to correlate with end-use applications. Measurement of properties can be helpful in selection of materials, but do not compare to rates in actual service which can be thousands of times greater with regard to velocities and temperatures. There are at least 25 laboratory abrasion test devices, an indication that this type of test is difficult to correlate with service performance. The most widely recognized test device in the rubber industry is the National Bureau of Standards Abrader, a sliding type abrader. The NBS Abrader uses a constant velocity, under a fixed load using a specified abrasive grit. See Figure 2 for diagrammatic sketch.

It does not tell how a compound performs under widely varying conditions, nor does it tell anything about cut resistance, chunking, or flat spotting.

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The abrasion resistance of vulcanizates of Adiprene L urethane rubber, as measured on two laboratory tests, the National Bureau of Standards test and the Tabor Abrader, are shown on Table I.

TABLE I ABRASION RESISTANCE

Adiprene Hardness NBS Abrasion Index Tabor Abrasion

Durometer A Durometer D ASTM D-394, Method B Resistance, Wt. Loss* ASTM D-1044

80 110 — 85 200 — 90 175 79 95 48 300 118

73 (Adiprene L-213) 500 373 73 (Adiprene L-315) 400 —

*mg/100 rev.; H-18 wheels, 1000 gm. wts.; 5000 rev. Note that these two tests give different values. The differences in performances of vulcanizates of Adiprene can be explained however. The National Bureau of Standards test simulates a very harsh service. In this case, the hardest vulcanizates hold up best. The Tabor test is much less severe. Softer compounds perform better than the harder ones because they are more resilient and “give” under load. The resistance to sliding abrasion increases with increasing hardness for the NBS test. The unusually high NBS Index for the 75A durometer vulcanizate is probably due to lubrication of the abrasive wheel by the plasticizer (Flexol DOP) used in the compound. As the hardness of the Adiprene L urethane rubber increases, NBS values increases for non-plasticized compounds. Only Adiprene L-213 does not show the expected improvement. In spite of the difficulties in obtaining meaningful laboratory abrasion test values, Adiprene L is considered to have excellent sliding abrasion resistance and has performed well in many applications where wear is a problem. Adiprene L has outworn convention rubber and plastics often by a factor of as much as 8 to 1.

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FLEXING

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FLEXING When subjected to flexing, rubber products frequently fail due to the development and propagation of cracks. The cracks reduce other properties, which in turn reduce the service life of the rubber. Cracks can grow through mechanical means or by oxidative and ozone attack. ASTM D-430, Method B, is a test designed to produce cracking by bending. The time or number of flexes to crack initiation are used as the measure of performance. It employs a DeMattia flexing machine which flexes a 6” x 1” x ¼” specimen having a 0.094” round grove molded transversely in the center of the strip. This machine operates at 300 cycles per minute. See Figure 1.

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An adaptation of the bend flex method of ASTM D-430 is ASTM D-813 which requires the deliberate cutting of the bottom of the grooved specimen to initiate crack. The number of flexing cycles needed to attain a specified crack length is then observed. ASTM D-1052 (Ross Flexer) is another method of determining the resistance of elastomers to cut growth from repeated bending. The equipment is illustrated in Figure 2. The flexed area of the test specimen bends freely over a rod 3/8” in diameter, through an angle of 90°. One end of the test specimen is gripped by a holder. The other end is placed between two rollers which permit free bending movement of the test

specimen during each cycle. This machine runs at 100 cycles per minute.

To obtain the ultimate in flex life with urethanes, careful attention to stoichiometry and polymer hardness must be considered. Urethanes may be specially compounded by adjustment of curing agent level to 100-110% theory (See Figures 3,4 and 5) to provide best flex resistance.

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Softer vulcanizates like Adiprene L-42 urethane rubber with MBCA curing agent have excellent flex life. In the Ross notched test, no cut growth occurred during 420,000 flexes (70 hrs.) at a rate of 100 cycles/minute. The more vigorous DeMattia test, run at 300 cycles/minute, caused failure in 24 hours using notched specimens; but unnotched samples ran for 100 hours (1,800,000 flexes) with only slight cracking occurring. Design of the part to reduce localized concentration of the stress or heat build-up will improve flex life. When an elastomeric part is flexed, very high stresses are developed in thick cross sections. Under repeated flexing, any cut in the surface of the part will grow larger because of the high local stresses concentrated at the cut. As with any elastomer, the rate of cut growth under flexing may be reduced (Figure 6) by decreasing the thickness of the part.

Unlike other elastomers, Adiprene L can be utilized practically in very thin sections because of its exceptional strength and toughness.

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INTERNAL HEAT BUILD-UP As mentioned in the section on resilience, heat build-up in urethane parts, resulting from internal friction under high frequency flexing, exceeds that of many conventional elastomers and is the usual cause of premature failure of urethane parts operating under flexing or high speed rotary motion under load. Because of the low thermal conductivity of urethane elastomers, heat developed by internal friction cannot be readily dissipated. Heat build-up is, therefore, a very important consideration when designing with urethanes. Its adverse effects can be minimized by using thin cross sections from which heat is more easily dissipated. The high strength and load bearing capacity of urethane elastomers makes possible the use of sections which are thin enough to dissipate heat at the same rate at which it is developed so the piece is not harmed. An example in which thinner sections actually increased the service life of a urethane elastomer part is offered by experience with industrial truck wheels made of Adiprene L urethane rubber. Early test wheels were made to the same dimensions normally used with conventional elastomers. In service, abrasion resistance was excellent but many premature failures occurred as a result of internal fracture and reduction in adhesive bond strength at the hub. Both types of failure were traced to excessive heat build-up under very high loads. The problem was solved by increasing the hub size and reducing the thickness of elastomer in the tire. This change provided a thinner tire section which dissipated internal heat more effectively. It also increased the shape factor of the area over which the load was distributed, thus decreasing the deflection for a given load. With the new design, urethane fork truck wheels are giving outstanding performance.

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48

INTERRELATION OF PHYSICAL

PROPERTIES

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INTERRELATION OF PHYSICAL PROPERTIES MBCA curing agent is an excellent general purpose curing agent for polymers of Adiprene L urethane rubber. It provides a good balance of pot life, cure rate and vulcanizate properties. The following MBCA concentrations are suggested for general purpose use.

TABLE I MBCA CONCENTRATION BASED ON MID-RANGE NCO

ADIPRENE POLYMER

PARTS/HUNDRED

% THEORY L-42 8.8 100 L-83 10.3 100

L-100 12.5 95 L-167 19.5 95 L-200 23.2 95 L-213 26.6 90 L-315 — 90

Particular properties can be optimized for specific applications by varying MBCA concentration. However, optimizing one property usually reduces another so that when formulating a compound, a compromise must be established. The effect of MBCA concentrations on the physical properties of the Adiprene polymers are shown on Figures 1 thru 6. The range of MBCA concentrates for several Adiprene polymers to optimize specific physical properties are shown on Table II.

TABLE II MBCA CONCENTRATION

% Theory Based on Isocyanate Content of Polymers

ADIPRENE

Tensile Strength

Compression Set

Tear Resistance

Flex Resistance

Abrasion Resistance

ASTM D-412 D-395 D-470 D-1025 D-394 L-42 85-100 80-90 100 100-110 100-110 L-100 85-100 85 90-110 100-110 100-110 L-167 90-100 90-95 100-110 105-110 90-105 L-200 95-100 95-100 — — 100 L-213 90-100 80-90 — — 90-05 L-315 90-95 80-90 90-100 — 90-95

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The amount of MBCA curing agent suggested for general purpose use (see Table I) allows processing safety. Some properties can be optimized at 110% theory (Figures 1 thru 6), but it must be recognized that processing safety may be jeopardized. Should the amount of MBCA exceed 110%, many of the physical properties are drastically reduced and a poor vulcanizate results. Adiprene polymers can be blended and physical properties generally are proportional to the amount of each polymer used. This is shown in Table III and Figure 7.

TABLE III Blends of ADIPRENE L-42 and ADIPRENE L-100

Adiprene L-42 100 60 50 40 — Adiprene L-100 — 40 50 60 100 MBCA 8.8 10.3 10.7 11.0 12.5

All compounds mixed at 212°F and cured 1 hour at 212°F. Postcured 16 hours at 158°F.

100% Modulus, psi 400 625 750 800 1100 300% Modulus, psi 625 1000 1250 1275 2100 Tensile Strength, psi 3000 3600 4000 4800 4500 Elongation @ break, % 800 730 675 640 450 Durometer A Hardness 80 82 83 84 90 ASTM D-470 Tear, lb./in. 70 85 90 95 75 Compression Set, Method B 22 Hrs. @ 158°F, %

45

38

34

33

27

NBS Abrasion Index, % 110 130 133 135 175 Properties for a 40% blend of Adiprene L-42 urethane rubber with 60% Adiprene L-100 at different MBCA levels are shown in Table IV and Figure 8.

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TABLE IV

40:60 BLENDS OF ADIPRENE L-42 AND ADIPRENE L-100 EFFECT OF MBCA LEVEL

Adiprene L-42 40 40 40 40 40 Adiprene L-100 60 60 60 60 60 MBCA - phr 10.2 10.7 11.3 11.9 12.4 MBCA - % Theory 90 95 100 105 110

All compounds mixed at 212°F and cured 1 hour at 212°F. Postcured 16 hours at 158°F.

100% Modulus, psi 875 850 775 700 600 300% Modulus, psi 1400 1425 1250 1000 775 Tensile Strength, psi 4100 4000 4500 2600 1500 Elongation @ break, % 530 550 610 780 960 Durometer A Hardness 85 84 83 81 80 ASTM D-470 Tear, lb./in. 55 67 94 97 90 Compression Set, Method B 22 Hrs. @ 158°F, %

35

32

37

55

70

NBS Abrasion Index, % 109 117 143 164 90

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SHEAR

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SHEAR Mounting and suspension assemblies generally require the loading of elastomers in shear. Elastomers deflect more under a given load in shear than in compression. Since shear is essentially a combination of tensile and compression forces acting at right angles to each other, the stress-strain curve for an elastomer in shear is similar to the tensile and compressive stress-strain curves. Shear is the ratio of linear deformation (d) to elastomer thickness (t) as illustrated in Figure 1.

Figure 2 shows typical shear stress-strain curves for ADIPRENE urethane rubber ranging in hardness from 55A to 75D durometer.

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Because of its high load bearing capacity in tension and compression, Adiprene has a high load bearing capacity in shear. Improvements in bonding Adiprene to metal will permit greater stress that those shown in Figure 2, Presently, 300 pli adhesion can be achieved compared to those values shown which are based on 100 pli. Past practice has limited shear strain (t) to 0.5; that is, the thickness of the rubber is twice the horizontal deflection. No specific reasons can be cited for this limitation. Some static applications of shear loading have been deformed to strains of 1.0 or more. However, under high strain, bond failures can occur imposing high stresses on the part. Useful hardnesses of urethanes are limited from 65A to 90A durometer. Below 65A conventional rubber can be used, and above 90A stresses are very unpredictable. It is common practice to enclose a shear mounting and move the loading surfaces closer together to provide a compressive load on the elastomers. Compression of 5% of the free thickness is commonly used. The effect of shear loading for a double shear pad is shown in Figure 3.

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With load, the rubber tends to leave the supporting walls at the top. As the angle decreases, diagonal A decreases in length thus creating compression at X. But diagonal B increases in length causes tension at Y. Therefore, by moving the loading surface closer together, the tensile stresses are reduced. To achieve stability, the ratio of width and length to thickness should be at least four. Lower ratios probably can be used with Adiprene urethane rubber and still be stable. It a shear pad were so designed that the height of the rubber equaled its thickness, the rubber would tend to bend as a cantilever beam rather than as a shear mounting.

If larger deflections are required than can be accommodated by one thickness, it may be necessary to make several sandwiches in shear as shown in Figure 4. However, the total width of the part between supports cannot be made too wide. Even though the elastomer is broken up into several sandwiches between supports, instability results in deflections greater than calculated from plain shear.

Shear bonds are affected by the thickness of the sandwich. The greater the thickness, the higher the tensile component in shear which results in less bond strength as shown in Figure 5.

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63

PHYSICAL CONSTANTS

OF ADIPRENE

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PHYSICAL CONSTANTS OF ADIPRENE

SPECIFIC GRAVITY Values for specific gravity, thermal conductivity, linear coefficient of thermal expansion and linear shrinkage are shown in Table I.

TABLE I PHYSICAL CONSTANTS

Linear Coefficient of Thermal Expansion in./in/+32°F

Specific Gravity

Thermal Conduct BTU/(hr.)

(Sq.ft.)(°F/in.)

-32° to +32°F

32°F to 75°F

75°F to 212°F

212°F to 302°F

Linear

Shrinkage%

L-100 1.10 0.917 1.43x10-4 1.01x10-4 0.95x10-4 0.90x10-4 1.0 L-167 1.13 0.862 1.27x10-4 0.89x10-4 0.89x10-4 0.69x10-4 1.7 L-213 1.19 0.754 0.79x10-4 0.81x10-4 0.75x10-4 1.08x10-4 1.7

Results for specific gravity are based on water which is 1.0 and give a quantity numerically equal to the density in grams per cubic centimeter. The specific gravity of vulcanizates of Adiprene urethane rubber varies depending on the polymer density and amount of MBCA used; for example, the specific gravity of Adiprene L-167 varies from 1.12 to 1.14 as the MBCA curing agent level changes from 15 parts to 21 parts. THERMAL CONDUCTIVITY Thermal conductivity is defined as the amount of heat per unit time passing across unit area and through unit thickness of material for unit temperature differences in the direction of the thickness. The units for thermal conductivity (K factor) are BTU per hour per square foot for temperature gradient of one degree Fahrenheit per inch thickness. LINEAR COEFFICIENT OF THERMAL EXPANSION The coefficient of thermal expansion is the ratio of the change in length per degree to the length at 32°F. The coefficient of thermal expansion varies with temperature. The expansion of all rubbers are of the same magnitude, approximately 10 times that of structural steel. If the part dimensions are critical, as in )-rings and seal, thermal expansion of rubber should be calculated. LINEAR SHRINKAGE Linear shrinkage is the approximate percent change in the dimensions of a part which occurs when the part cools to room temperature. The figures for linear shrinkage shown in Table I are for conventional mixing and curing conditions. Shrinkage is normal for most rubbers and should be accounted for in mold design.

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ADHESION

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ADHESION During fabrication of composite parts, Adiprene urethane rubber can readily be adhered to many metals, elastomers and plastics with bond strength which often exceed even the tear strength of Adiprene itself. It is difficult to bond cured Adiprene to another rmaterial, but special techniques have been developed to satisfy most requirements. Surfaces should be completely free of oil, grease and oxide film. Grit blasting to roughen the surface and degreasing is recommended, followed by a coating of an adhesion primer to protect the surface from oxidation and moisture during storage. A fresh coat of primer should be applied before casting the Adiprene. Good bonds between Adiprene and other elastomers can be obtained by first removing traces of oil, greases and mold release agent from the elastomer and then roughening the surface with sandpaper, sandblasting or other abrasives. An adhesive primer is then applied to the surface by brushing, spraying or roll coating and Adiprene cast against it or adhered with pressure if the Adiprene has been cured. Many adhesives and primers are used with Adiprene. Some of these primers are shown in Table I along with typical peel adhesion values. Tests were made in accordance with ASTM D-429, Method B.

TABLE I PRIMERS FOR BONDING ADIPRENE TO STEEL AND ALUMINUM

90° Peel Adhesion* - lb./in.

Adhesion Primer

Cover Coat

Adiprene L-100 Steel

Adiprene L-167 Aluminum Steel

Thixon 405 Thixon 405 330** 215 300** Thixon 409 Thixon 409 330** 185 310** Chemlok 218 (2) Chemlok 218 270 265 290

Pull – 2”/min. Samples aged 2 weeks at RT before testing BONDING PROCEDURE

1. Grit blast metal. 2. Degrease metal with xylene and MEK. 3. Air dry primers 30 minutes between coats. 4. Bake primers 1 hour at 212°F. 5. Cast Adiprene L with MBCA over the metal which has been preheated to 212°F. 6. Cure cycle: 2 hours/212°F.

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*ASTM D-429 – Method B ** Stock Failure

1. Dayton Chemical Products Laboratories, West Alexandria, Ohio 2. Hughson Chemical Company, Div. Of Lord Corp., Erie, Pennsylvania

Table II describes the use of a primer where prebaking of the metal is not required.

TABLE II ADHESION WITH AND WITHOUT PREBAKE OF PRIMER

90° Peel Adhesion* - lb./in. Primer – Chemlok 218

Steel Aluminum (2024T4)

½ Hr. Bake @ 212°F

No Bake

½ Hr. Bake @ 212°F

No Bake

L-100 with MBCA

250 270 229 265

L-167 with MBCA

300** 330** 290** 330**

BONDING PROCEDURE

1. Clean metal by grit blasing. 2. Degrease metal with xylene, followed by MEK. 3. Apply 2 coats of primer. 4. Air dry primer for 30 minutes between coats. 5. Where primer is not baked, Adiprene L with MBCA at 212°F. 6. When primer is based for ½ hour at 212°F, Adiprene L with MBCA at 212°F is cast on

primed metal preheated to 212°F. *ASTM D-429 – Method B ** Stock Failure The following outlines the general requirements for bonding Adiprene urethane rubber to metal:

1. Sand or grit blast metal surface to remove dirt, oxide, etc. Aim for a matte surface rather than one distinctly rough.

2. Degrease, using any standard degreasing procedure which leaves a dry surface. Avoid using very fast evaporating solvents such as acetone, gasoline, hexane, methylene chloride as they may cause moisture condensation of the metal surface which will interfere with formation of a good bond. Trichloroethylene, perchloroethylene, toluene, methyl ethyl ketone as good degreasing solvents. It is best to prepare the surface just before application of the adhesive primer.

3. Apply one coat of primer at once to prevent rusting and contamination of clean surface.

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4. Maintain both primer and metal at room temperature. Primers applied at temperatures below 70°F (21°C) may not produce good bonds.

5. Apply second coat of primer at any time, but the part should be allowed to air for at least

30 minutes before it is placed in the preheat oven. This is necessary to prevent blistering from solvent evaporation.

6. Heat metal to processing temperature, pour and cure Adiprene. 7. During all phases of metal preparation, protect the surface of metal and primer from

contamination with mold release spray or oil spray from operating machinery. Do not handle surfaces to be bonded with bare hands, use only with clean gloves. Handle inserts and cores only on portions which are not bonded to Adiprene urethane rubber.

8. Adhesives can be applied by any technique which insures a continuous adhesive film

deposited on a clean surface. The five major methods include: dipping, spraying, brushing, roll coating, tumbling.

In addition to casting Adiprene to various substrates, it is possible to bond cure Adiprene to:

1. Cured Adiprene 2. Metal at Room Temperature 3. Epoxy and Fiberglass 4. Cured Natural Rubber 5. Uncured Elastomer Compounds 6. Uncured SBR Compounds 7. Uncured Neoprene

While it is possible to achieve bonds of 300 pli to metal, the bonds listed may not achieve these high values with some materials. Since new primers for specific bonding requirements are continually under development, it is suggested that primer manufacturers be asked for their recommendation. See footnotes in Table I.

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ELECTRICAL PROPERTIES

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ELECTRICAL PROPERTIES The electrical properties of elastomers most commonly measured are as follows:

1. Resistivity 2. Dielectric Strength 3. Dielectric Constant 4. Power Factor

Materials suitable for electrical insulators have high dielectric strength and resistivity and low dielectric constant and power factor. Such a combination is rarely obtained since companion physical and chemical properties are also required. There is no single best overall material, but Adiprene urethane rubber offers a favorable combination of properties. DIRECT CURRENT RESISTIVITY Direct current resistivity, or volume resistivity, is similar to insulation resistance in that both indicate the magnitude of electrical current expected to pass through th esample located between two electrodes. This test may be used to check the suitability of an elastomeric composition for electrical insulation. Resistivity or specific resistance to electric current is usually considered to be a DC property and is measured as such. It can be defined as the resistance between opposite faces of a unit cube where precautions have been taken to allow no current flow along the other four faces of the cube. CONDUCTIVITY Elastomer compositions are considered electrically conductive when they possess a direct current resistivity of less than 105 to 107 ohm-cm. Conductive compounds find their principal applications where the dissipation of static electricity is desired. DIELECTRIC STRENGTH The dielectric strength of an elastomer is the voltage required to puncture a sample of known thickness and is expressed as volts per mil of thickness. The rate of voltage application, the geometry of the electrodes, and the shape of the test specimen influence the results obtained. DIELECTRIC CONSTANT AND POWER FACTOR The dielectric constant, or specific inductive capacity (SIC), is a measure of an insulator’s ability to store electrical energy. The dielectric constant is the ratio of the electrical capacity of a condenser using the elastomer under test as the dielectric, to the capacity of a similar condenser using air as the dielectric. One of the factors which influences the dielectric constant is frequency, and tests may be run from a low of 25 cycles per second to many megacycles per second. The power factor of an electrical insulation material indicates its tendency to generate heat in service. If a capacitor using an elastomer as the dielectric is charged by a direct current and them immediately discharged, there is an energy loss in the form of heat. If this capacitor is repeatedly charged and discharge by an alternating current, the electrical loss results in heating. The ratio of this loss to the energy required to charge the capacitor is known as power factor. It is expressed as a decimal fraction or a percent of the charging energy.

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Adiprene urethane rubber has been used in potting and insulation compositions at frequencies up to 100 kilohertz at temperatures at 212°F(100°C). Its natural translucency permits easy inspection of the encapsulated assemblies and the flexibility and strength of Adiprene helps protect the assemblies from damage. The electrical properties of vulcanizates of Adiprene measured at different temperatures and frequencies are shown in Table I.

TABLE I ELECTRICAL PROPERTIES

Physical Properties

Adiprene L-100 MBCA

Adiprene L-167 MBCA

Durometer Hardness 90A 50D Electrical Properties 0.1 khz 100 khz 0.1 khz 100 khz Power Fact, %, 75°F (ASTM D-150) 158°F 212°F

4.70 9.45

12.60

5.92 4.15 3.90

7.25 6.65 8.75

4.35 4.75 4.00

Dielectric Constant (SIC) (ASTM D-150) 75°F 158°F 212°F

9.37

11.05 11.48

7.78 9.62 9.87

9.25

11.65 12.19

7.58 9.74 9.98

DC Volume Resistivity, ohm-cm (ASTM D-257)

75°F 4.8 x 10 11 3.7 x 10 12

158°F 3.8 x 10 10 2.0 x 10 11

212°F 2.3 x 10 10 1.1 x 10 11

Dielectric Strength, Volts/mil (ASTM D-149) 75°F

450-500

650-700 1 Herts (HZ) = 1 cycle/sec. 1 khz = 1000 cycles/sec. kc5 kilocycle = 1000 cycles/sec. The basic polymers may be modified with epoxy resins for improved electrical properties. This is shown in Table II.

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TABLE II ELECTRICAL PROPERTIES OF ADIPRENE L-100 WITH EPOXY RESIN VULCANIZATES

Compound

Adiprene L-100 50 Epoxy Resin* 50 MBCA 25 Cure: 6 hours at 285°F

Effect of Temperature

DC Volume Resistivity,

ohm-cm Dielectric

Strength Volts/milDielectric Constant At 1 khz

Power FactorAt 1 khz, %

Tested at 75°F 5 x 1015 932 3.5 1.1 167°F 3 x 1013 - 5.5 5.1 212°F 1 x 1012 - 6.5 5.6 250°F 3 x 1011 - 6.8 3.3 Effect of Aging (Tested at 75°F)

Original 5 x 1015 932 3.5 1.1 Heat Aged, 7 days at 250°F

5 x 1015

818

1.9

0.6

Aged in Water, 7 days at 158°F

1 x 1014

551

5.8

2.8

Aged in ASTM Oil No. 1 - 7 days at 158°F

5 x 1015

784

4.5

1.6 *Expoxide equivalent about 200

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FRICTIONAL CHARACTERISTICS

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FRICTIONAL CHARACTERISTICS Friction of Adiprene polymers against non-lubricated surfaces decreases with increasing hardness

as shown in Figure 1. Since harder polymers have the lowest coefficient of friction, these materials have been used where sliding resistance is important. Of all Adiprene urethane rubbers, Adiprene L-315 has the lowest, unlubricated coefficient of friction. This characteristic, coupled with its superior abrasion resistance and load-carrying ability, is an important reason why Adiprene L-315 is used for bearings and bushings. Since the hardness of compounds of Adiprene L-315 approaches some plastics, comparison of Adiprene L-315 with various plastics is shown in Table I.

TABLE I COMPARISON OF ADIPRENE L-315 WITH PLASTICS

Adiprene

L-315 Nylon 66

2.5% Water

Acetal Cast Phenolic

Unfilled Specific Gravity 1.20 1.14 1.42 1.30 Hardness, Rockwell R90 R108 R120 M110 Tensile Strength, psi 9,000 11,200 10,000 7,000 Elongation at Break, % 210 200 15 — Modulus of Elasticity In Tension, 103 psi

52

260

410

700

Flexural Modulus (Instron) 103 psi

81

175

410

Compressive Modulus 103 psi

68.75

Impact Resistance, ft.lb./in. Notched Izod, 75°F

15

2.0

1.4

0.3

Heat Deflection Temp., % At 66 psi At 264 psi

365 135

300 150

338 255

260 —

Taber Abrasion, CS-17, 1000 g, mg loss/1000 rev.

5

7

20

Water Absorption, 24 Hrs. At 75°F, %

1.2

0.4

0.25

0.4

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EFFECT OF ADDITIVES ON FRICTIONAL PROPERTIES Additives may be used to alter the frictional properties of Adiprene polymers. With Adiprene L-315 urethane rubber, powdered Teflon TFE fluorocarbon resin and Teflon TFE fluorocarbon fiber flock significantly reduce the coefficient of friction of this elastomer. The frictional change due to these additives is shown in Figure 2. Adiprene L-315 without additives is used as a control.

The additives mentioned above will affect other physical properties of Adiprene L-315. Property changes are presented in Table II.

TABLE II ADIPRENE L-315

EFFECT OF LUBRICANT ADDITIVES ON PHYSICAL PROPERTIES

Plain L-315

+ Teflon Powder 10 Parts

+ Teflon Fiber Flock 10 Parts

100% Modulus, psi 4650 4100 4100 Tensile Strength, psi 9000 5000 5200 Elongation @Break, % 210 115 125 Durometer D Hardness 73 72 72 ASTM D-470 Tear, lbs./in. 110 105 95 National Bureau of Stds. Abrasion Index, %

400

500

890

Compression Set, Method A 1350 psi, 22 Hrs. @158°F

10

8

4

Materials Used:

1. TEFLON® Powder – “Rilube #63, Modern Industrial Plastics, Dayton, Ohio 2. TEFLON® Fiber TFE TEFLON® fiber flock, 1/64”, DuPont, Textile Fibers Department

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All of the additives at a 10 part level (7.4% by weight of total compound) will reduce modulus, tensile and elongation. Additives which reduce the friction coefficient also improve abrasion resistance. The improvement in abrasion obtained with TEFLON® fluorocarbon fiber addition is significant and was also observed during long term friction tests. The 10 parts of additive is not necessarily the optimum. However, 10 parts offer significant frictional improvement over 5 parts and is not significantly inferior to 15 parts. The optimum level of additive, considering a balance of physical and frictional properties, probably falls between 5 and 10 parts. EFFECT OF ADDITIVES ON BEARING PERFORMANCE Teflon improves the performance of Adiprene L-315 in bearing applications. Pressure-Velocity (PV) limit data for bearings based on Adiprene L-315 urethane rubber, Nylon 66 and DELRIN®

Acetal resins are shown in Figure 3. These curves represent the performance limits of the bearings. Bearings can operate at any combination of pressure and velocity below the respective curves without catastrophic failure. The PV limits predict nothing about the length of service however. Although Adiprene L-315 may be expected to outwear most thermoplastics, its performance will be influenced strongly by temperature and other environmental conditions. The best determination of bearing durability is a service test.

76

Frictional data listed in this chapter were obtained with an apparatus which utilizes a thrust washer principle and the apparatus is shown schematically in Figure 4. It consists of a table mounted drill press, variable speed drive and simple machined parts to accommodate test samples. Friction force and wear can be measured with this device. The use of standard components and small, easily fabricated test samples make this an inexpensive testing apparatus. The sample is a disc with a diameter of 1-1/3”; on one side is a rim of 1/16” width; this rim constitutes the area of contact.

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IMPACT RESISTANCE

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IMPACT RESISTANCE

The impact or shock resistant of an elastomer is determined by striking a sample with a swinging pendulum (hammer). The sample is placed at the lowest point of the arc traveled by the pendulum head. Measuring the distance in the distance of the upswing of the pendulum after the impact, compared to the same upswing with nothing in its path, determines the energy in breaking the sample which is the measure of impact strength. In the Izod impact method, (ASTM D-256) the test piece is gripped upright and struck with the pendulum 7/8” above the edge of the gripping point. The sample has a standardized notch at the edge of the vise on the side toward the hammer. The Izod Impact Tester and Izod Bar are shown in Figures 1 and 2.

Most vulcanizates of Adiprene urethane rubber flex and bend in this type of test. Adiprene L-315 is a material which approaches structural plastics in hardness. Yet even at this hardness, Adiprene L-315 has significantly better impact resistance than plastics. Values for this 75D material are compared in Table I with those of several plastics. In order to approach these high values for Adiprene L-315, plastic materials require reinforcement with glass fibers.

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TABLE I IMPACT RESISTANCE, IZOD, FT./IN.

(ASTM D-256)

Nylon

Acetal

Acrylic

Adiprene L-213

Adiprene L-315

Hardness (Rockwell or Durometer)

Rockwell R108

Rockwell R120

Rockwell M103

Durometer 73D (Rockwell R90)

Notched, 75°F 2.0 1.4 0.3 4.0 15.0 Notched, -40°F 0.5 1.2 0.3 - 1.1


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