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MATERIAL PROPERTIES GUIDE

TABLE OF CONTENTS

Page

INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .1

MATERIAL PROPERTY DATA TABLE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2

MECHANICAL PROPERTIES Tensile Properties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 Flexural Properties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 Creep Properties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .9 Creep Rupture . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .10 Fatigue Properties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11 Impact Properties . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .11

THERMAL PROPERTIES Heat Deflection Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .12 Continuous Use Temperature . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .12 Heat Aging . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .13

FLAMMABILITY AND COMBUSTION PROPERTIES Flammability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .13 Smoke Emission . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .13 Toxic Gas Emission . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .14

ELECTRICAL PROPERTIES Volume Resistivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .14 Surface Resistivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .14 Relative Permittivity and Dielectric Dissipation Factor . . . . . . . . . . . . . . . .15

TRIBOLOGY Wear . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .16 Friction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .16 Limiting Pressure and Velocity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .17 Environmental Resistance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .18 Gas Permeation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .18 Hydrolysis Resistance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .19 Chemical Resistance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .19 Radiation Resistance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .20

INTRODUCTION

Victrex is the sole manufacturer of VICTREX PEEK polymer, the repeat unit that comprises oxy-1,4-phenyleneoxy-1,4-phenylene-carbonyl-1,4-phenylene, as shown in Figure 1. This linear aromatic polymer is semi-crystalline and is widely regarded as the highest performance thermoplastic material currently available. A summary of key physical properties is as follows:

Figure 1: VICTREX PEEK Repeat Unit

HIGH TEMPERATURE PERFORMANCE

VICTREX PEEK and compounds typically have a glass transition temperature of 143°C (289°F) and a melting temperature of 343°C (649°F). Independent tests have shown that VICTREX PEEK exhibits a heat distortion temperature up to 315°C (599°F) (ISO R75, glass fibre filled) and a Continuous Use Temperature of 260°C (500°F) (UL 746B).

WEAR RESISTANCE

VICTREX PEEK has excellent friction and wear properties which are optimised in the specially formulated tribological grades VICTREX 450FC30 and VICTREX 150FC30. These materials exhibit outstanding wear resistance over wide ranges of pressure, velocity, temperature and counterfacial roughness.

CHEMICAL RESISTANCE

VICTREX PEEK has excellent resistance to a wide range of chemical environments, even at elevated temperatures. The only common environment which dissolves VICTREX PEEK is concentrated sulfuric acid.

FIRE, SMOKE AND TOXICITY

VICTREX PEEK is highly stable and requires no flame-retardant additives to achieve a V-0 rating at 1.45 mm

(0.057 in) thickness. The composition and inherent purity of the material results in extremely low smoke and toxic gas emission in fire situations.

HYDROLYSIS RESISTANCE

VICTREX PEEK and compounds are not attacked by water or pressurised steam. Components that are constructed from these materials retain a high level of mechanical properties when continuously conditioned in water at elevated temperatures and pressures.

ELECTRICAL PROPERTIES

The electrical properties of VICTREX PEEK are maintained over a wide frequency and temperature range.

PURITY

VICTREX PEEK materials are inherently pure with exceptionally low levels of ionic extractables and excellent outgassing characteristics.

VICTREX PEEK PRODUCT RANGE POWDER 150P Low viscosity grade for extrusion compounding. 380P Medium viscosity grade for extrusion compounding. 450P Standard viscosity grade for extrusion compounding.
GRANULES 150G Easy flow grade for injection moulding of thin sections and complex parts (USA only). 450G General purpose grade for injection moulding and extrusion.
GLASS FILLED 150GL30 Easy flow, 30% glass fibre reinforced for injection moulding. 450GL30 General purpose, 30% glass fibre reinforced grade for injection moulding and extrusion.
CARBON FILLED 150CA30 Easy flow, 30% carbon fibre reinforced for injection moulding. 450CA30 Standard viscosity, 30% carbon fibre reinforced grade for injection moulding.
LUBRICATED 150FC30 Easy flow, 30% carbon/PTFE grade for injection moulding. 450FC30 Standard viscosity, 30% carbon/PTFE grade for injection moulding and extrusion.
DEPTH FILTERED 381G Medium viscosity for wire coating, capillary tubing, film and monofilament extrusion. 151G Low viscosity monofilament and multifilament extrusion grade. Also suitable for injection moulding of thin wall and complex parts.

* Results based on VICTREX 450G

3

There are a number of Victrex specialty products that are not listed in the data table. Data sheets for these materials can be obtained from your local Victrex representative.

6

MECHANICAL PROPER TIES Figure 3: Tensile Strength Versus Temperature for VICTREX PEEK Materials
VICTREX PEEK is widely regarded as the highest performance material processable using conventional thermoplastic processing equipment. 300 -148 -48 VICTREX 52 152 252 Temperature / °F 352 452 40000 552

450CA30

250

Tensile Strength / MPaFlexural Strength / psi Tensile Strength / psi

10000

TENSILE PROPERTIES

The tensile properties of VICTREX PEEK exceed those of

most engineering thermoplastics. A comparative tensile

plot of VICTREX PEEK materials is shown in Figure 2,

where stress is defined as the applied force divided by

200

150

100

the original cross-sectional area and the strain as the extension per unit length of the sample.

The initial part of each trace in Figure 2 is approximated to be linear and by definition is equivalent to the tensile modulus. Due to the viscoelastic nature of VICTREX PEEK, a range of values for tensile properties may be obtained by testing at different strain rates or temperatures. Therefore, evaluations of the tensile parameters contained in the data table were conducted in accordance with the ASTM D638 testing standard with strain rates set at either 5 or 50 mm min-1 (0.2 or

2.0 in min-1).

Figure 2: Typical Stress Versus Strain Curves for

VICTREX PEEK Materials

300 40000

250 35000 50 00

Flexural strength has been defined as the maximum stress sustained by the test specimen during bending, and flexural modulus as the ratio of stress to strain difference at pre-defined strain values.

The data plotted in Figures 4 and 5 define the exceptional temperature range over which VICTREX PEEK can be used as a structural material. However, flexural strength measurements made above 200°C (392°F) are subject to error as the yield point of these materials is greater than the 5% strain specified in the test standard. Above this value, a linear stress to strain relationship cannot be assumed for the calculation of flexural properties.

30000

200

Stress / MPa

Stress / psi

Figure 4: Flexural Strength Versus Temperature for

VICTREX PEEK Materials

Temperature / °F

25000

20000

150

15000

100

32 132 232 332 432

350

10000

VICTREX 450CA30

5000 300

0

Flexural Strength / MPa

40000

0

0

250

30000

200

150

VICTREX PEEK is used to form structural components

which experience or continually operate at high tem

peratures. Figure 3 shows a plot of tensile strength ver

20000

100

10000

50

sus temperature for VICTREX PEEK materials and

demonstrates a high retention of mechanical properties

over a wide temperature range.

Temperature / °C

FLEXURAL PROPERTIES

VICTREX PEEK and the high-performance compounds based on VICTREX PEEK exhibit outstanding flexural performance over a wide temperature range. Due to the viscoelasticity of these materials, evaluations were performed using a defined deformation rate three point bending test (standards ISO 178 and ASTM D790) with the results plotted versus temperature in Figures 4 and 5.

Figure 7: Tensile Strain Versus Time for VICTREX 450G at 150°C (302°F)

2.0

Tensile Strain / %

1.5

5 MPa (725 psi)

1.0

4 MPa (580 psi)

0.5

0.0 1.E+1 1.E+2 1.E+3 1.E+4 1.E+5 1.E+6 1.E+7 1.E+8

Time / s

Figure 5: Flexural Modulus Versus Temperature for CREEP PROPERTIES VICTREX PEEK Materials Creep may be defined as the deformation observed in a sample versus time under a constant applied stress.

Temperature / °F -148 -48 52 152 252 352 452 VICTREX PEEK has outstanding creep resistance for an

3500000 engineering thermoplastic material and may sustain

large stresses over a useful service life without signifi-

Flexural Modulus / psi

Flexural Modulus / GPa

cant time induced extension. Figures 6 and 7 display

the creep behavior of VICTREX 450G with respect to

applied stress, time and temperature.

The magnitude of stress, time and temperature

required to induce accurately measurable (> 0.5%)

strains is exceptionally large for an unfilled polymer.

500000

Values of creep modulus may be calculated from such

0 data and used as a measure of resistance to creep deformation. The creep moduli for some of the high performance compounds from the VICTREX PEEK grade range are plotted against time in Figure 8.

Figure 6: Tensile Strain Versus Time for Figure 8: Creep Modulus Versus Time for VICTREX 450G at 23°C (73°F) VICTREX PEEK at 23°C (73°F) and 150°C (302°F)

2.0

25

3500000

50 MPa (7250 psi)

3000000

20

1.5

Tensile Strain / %

2500000

Modulus / psi

2000000

1.0

30 MPa (4350 psi)

1500000

20 MPa (2900 psi)

0.5

1000000

5

500000

10 MPa (1450 psi)

0.0 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08

0

0 1E+1 1E+2 1E+3 1E+4 1E+5 1E+6 1E+7 1E+8

Time / s Time / s

From the data in Figure 8 it is clear that reinforcement significantly enhances the excellent creep resistance of VICTREX PEEK and that the carbon fibre based compounds (CA30) are the highest performance materials tested.

If analogous plots to Figures 6 and 7 are constructed for VICTREX 450CA30 (Figures 9 and 10), the time dependent strain behaviour over experimentally practicable lifetimes may be evaluated. From the data shown in Figure 9 it is clear that there is little measurable creep at ambient temperatures even for the highest values of stress [80 MPa (11,600 psi)] applied to the VICTREX

450CA30 samples.

At elevated temperatures (Figure 10), under the same applied stresses, small but measurable time dependent strains are observed. Although the creep resistance of natural VICTREX PEEK is outstanding for an unfilled material, VICTREX 450CA30 can be used to make structural components which will withstand continual loading over a wide temperature range.

Figure 9: Tensile Strain Versus Time for VICTREX 450CA30 at 23°C (73°F)

CREEP RUPTURE

The performance of thermoplastic materials under a constant applied stress may also be considered in terms of creep rupture. Creep rupture indicates the maximum loading a material will sustain for a given period before it fails, where failure is defined as brittle or necking deformation. Figure 11 shows tensile creep rupture data versus time for natural and reinforced VICTREX PEEK materials.

Strain / %

1
0.8
0.6
0.4 60 MPa (8700 psi) 80 MPa (11,600 psi)

Figure 12: Creep Rupture for VICTREX PEEK Materials at 150°C (302°F)

1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07 1.E+08 Time / s

Figure 11 shows that there is little difference between the grades at ambient temperatures over the time-scale tested. Therefore, experiments were performed at elevated temperatures (Figure 12).

40 MPa (5800 psi)

0.2

20 MPa (2900 psi)

0 1E+1 1E+2 1E+3 1E+4 1E+5 1E+6 1E+7

Time / s

Figure 10: Tensile Strain Versus Time for VICTREX 450CA30 at 150°C (302°F)

1

0.8

Tensile Strain / %

0.6

0.4

0.2

50 MPa (7250 psi) 40 MPa (5800 psi) 30 MPa (4350 psi) 20 MPa (2900 psi)

0
1E+1 1E+2 1E+3 1E+4 1E+5 1E+6 1E+7
Time / s

1E+0 1E+1 1E+2 1E+3 1E+4 1E+5 1E+6 1E+7 Time / s

Figure 12 shows the effect of fibre reinforcement and orientation for VICTREX PEEK materials. The angles indicate the direction of testing with respect to melt flow. VICTREX 450CA30 exhibits superior creep rupture performance over the other materials tested and to most high performance thermoplastics. Therefore, VICTREX 450CA30 materials are often used to form components which experience permanent loading at high temperatures.

FATIGUE PROPERTIES Figure 14: Charpy Impact Strength Versus Temperature for Fatigue may be defined as the reduction in mechanical VICTREX PEEK Materials properties during continued cyclic loading. In these

1.E+00 1.E+01 1.E+02 1.E+03 1.E+04 1.E+05 1.E+06 1.E+07

No. of Cycles to Failure and 16 (ASTM D256). Figure 13 clearly shows that the excellent fatigue resis-

tance of VICTREX 450G is enhanced by both glass and

for Various High Performance Materials

carbon fibre reinforcement. Independent studies have shown that these compounds feature the optimum 1200

level of reinforcement for improved fatigue and

mechanical performance.

IMPACT PROPERTIES

Impact testing may be classified according to the ener

gy imparted to the impactor prior to contact with the

Izod Impact Strength / J m-1

1000

800

600

material. Low energy studies are performed using a

pendulum geometry, whereas higher energy failures

are evaluated using falling weight apparatus. The impact properties of a material are strongly dependent on test geometry (notch radius and position), temperature, impact speed and the condition of the sample (surface defects). Therefore, in an attempt to unify these variables, measurements are often made in accordance with one of the testing standards.

400

200

0

VICTREX VICTREX VICTREX PAI + 30% PPS + 40% Polyimide 450G 450GL30 450CA30 Glass Glass

The bar chart shown in Figure 15 allows comparisons to be made between VICTREX PEEK materials and other high performance compounds. Natural VICTREX 450G has the highest unnotched impact strength and remains unbroken under the Izod test conditions.

THERMAL PROPERTIES

Various High Performance Materials

VICTREX PEEK has a glass transition temperature of

120

143°C (289°F) and, because it is a semi-crystalline ther

100

80

60

40

20

PAI + 30% VICTREX VICTREX VICTREX Polyimide PPS + 40% Glass 450GL30 450CA30 450G Glass

moplastic, retains a high degree of mechanical properties close to its melting temperature of 343°C (649°F).

HEAT DEFLECTION TEMPERATURES

The short term thermal performance of a material may be characterised by determining the Heat Deflection Temperature (HDT, ISO 75). This involves measuring the temperature at which a defined deformation is observed in a sample under constant applied stress. A comparative chart of high performance materials using ISO 75 HDT values (Figure 18) for a defined applied stress of 1.8 MPa (264 psi) shows that VICTREX PEEK compounds are superior to the other materials tested.

Izod Impact Strength / J m -1

Figure 16 shows the effects on the impact strength of notching various materials. The geometry of the notch has been shown to be critical to the measured impact strength. Therefore, in component design, moulded

notches or acute angles should be avoided. High Performance Materials

600 500 400 300 200

Temperature / °F

80 70 60 50 40 30 20 10 0

Failure Energy / J

-100 -50 0 50 100 150 200 250 300

Temperature / °C

Figure 17 shows the energy to failure of VICTREX PEEK and compounds versus temperature to failure.

Use Temperature (CUT) otherwise known as the Relative Thermal Index (RTI) as defined by Underwriters Laboratories (UL 746B). This test determines the temperature at which 50% of material properties are retained after a conditioning period of 100,000 hours. The UL RTI rating for natural VICTREX PEEK is charted against other engineering materials in Figure 19 (page 13).

Figure 19: Relative Thermal Index (RTI) for a Range of chemical structure of the VICTREX PEEK is highly stable-High Performance Materials and requires no flame retardant additives to achieve low flammability and ignitability values. The composi

300

tion and inherent purity of VICTREX PEEK results in 500 excellent smoke and toxicity performance.

250

FLAMMABILITY

400

200

Temperature / °C

Temperature / °F

The flammability of a material may be defined as the

300

ability to sustain a flame upon ignition from a high

150

energy source in a mixture of oxygen and nitrogen. The

200

100

recognized standard for the measurement of flamma

100

50

0

0

VICTREX VICTREX VICTREX PPA + PAI + 30% PPS + PES PSU 450G 450GL30 450CA30 33% Glass Glass 40% Glass

HEAT AGING

As part of the Underwriters Laboratories evaluation of the physical performance of polymeric materials with respect to temperature, heat aging experiments are performed. These involve conditioning specimens for a pre-defined time at a constant temperature and subsequently measuring their tensile properties. The retention of these properties is calculated with respect to a control and is used as a measure of the thermal aging performance. The outstanding percentage retention of tensile strength and elongation to break for natural VICTREX PEEK is plotted versus conditioning time in Figure 20.

bility is the Underwriters Laboratories test UL94. This involves the ignition of a vertical specimen of defined geometry and measures the time for the material to self-extinguish. The average time from a repeated ignition sequence is used to classify the material. Natural VICTREX 450G has been rated as V-0 [1.5 mm (0.059 in) thickness] which is the best possible rating for flame retardancy.

SMOKE EMISSION

The current standard for the measurement of smoke produced by the combustion of plastic materials is ASTM E662. This uses the National Bureau of Standards (NBS) smoke chamber to measure the obscuration of visible light by smoke generated from the combustion of a standard geometry sample in units of specific optical density. The test may be carried out with either continuous ignition (flaming) or interrupted ignition (nonflaming). A comparative bar chart of the specific optical density for a range of engineering plastics is shown in Figure 21.

Figure 21: Specific Optical Density for a Range of

Engineering Thermoplastics Measured in Flaming Mode for 3.2 mm (0.126 in) Thick Samples

1000

900 800 700 600 500 400

Specific Optical Density / Ds

300 200 100

Exposure Time / h

FLAMMABILITY AND COMBUSTION PROPERTIES

In a fire, the thermal and chemical environment is changing constantly. Therefore, it is difficult to simulate the conditions experienced by a material in a fire situation. The four commonly accepted variables are flammability, ignitability, smoke and toxic gas emission. The

0

VICTREX PEI Phenolic PTFE PC PSU PS PVC Polyester ABS 450G

The data in Figure 21 show that natural VICTREX PEEK has the lowest value of specific optical density of all the materials tested.

TOXIC GAS EMISSION Figure 22: Volume Resistivity Versus Electrification The emission of toxic gases during combustion of a Time for VICTREX 450G polymer cannot be considered purely as a function of

1E+17

the material. The component geometry, heat release,

conditions of the fire, and the synergistic effects of any

toxic gases affect the potential hazard of the material

in an actual fire situation. VICTREX PEEK, like many

organic materials, produces mainly carbon dioxide and

carbon monoxide upon pyrolysis. The extremely low concentrations of toxic gases emitted have been evalu

ated using the Aircraft Standards (BSS 7239, ATS1000/ABD0031). This procedure involves the com-

Volume Resistivity / cm

1E+16

1E+15

1E+14

1E+13

1E+12

plete combustion of a 100 g (0.22 lb) sample in a 1 m3 (35.3 ft3) volume and subsequent analysis of the

1E+11

toxic gases evolved. The toxicity index is defined as the summation of the concentration of gases present normalized against the fatal human dose for a 30 minute exposure. VICTREX 450G gives a 0.22 toxicity index with no acid gases detected.

ELECTRICAL PROPERTIES

VICTREX PEEK is often used as an electrical insulator with outstanding thermal, physical and environmental resistance.

VOLUME RESISTIVITY

Volume resistance and resistivity values are used as aids

in choosing insulating materials for specific applica

tions. The volume resistance of a material is defined as

the ratio of the direct voltage field strength applied

between electrodes placed on opposite faces of a speci

men and the steady-state current between those elec

trodes. Resistivity may be defined as the volume resis

tance normalized to a cubical unit volume.

volume resistivity of VICTREX 450G is plotted versus temperature in Figure 23. This shows that high values for the volume resistance of natural VICTREX PEEK are retained over a wide temperature range.

Temperature / °F 32 82 132 182 232 282 332 382 432 482 1E+18

1E+17

Volume Resistivity / cm

1E+16

1E+15

1E+14

1E+13

1E+12

1E+11

As with all insulating materials, the change in resistivity with temperature, humidity, component geometry and time may be significant and must be evaluated when designing for operating conditions. When a direct voltage is applied between electrodes in contact with a specimen, the current through the specimen decreases asymptotically towards a steady-state value. The change in current versus time may be due to dielectric polarization and the sweep of mobile-ions to the electrodes. These effects are plotted in terms of volume resistivity versus electrification time in Figure 22.

The larger the volume resistivity of a material, the longer the time required to reach the steady-state current. Natural VICTREX 450G has an IEC 93 value of

6.5 x 1016 Ω cm at ambient temperatures, measured using a steady-state current value for 1000 s applied voltage. Using the same experimental technique, the

1E+10 0 50 100 150 200 250

Temperature / °C

SURFACE RESISTIVITY

The surface resistance of a material is defined as the ratio of the voltage applied between two electrodes forming a square geometry on the surface of a specimen and the current which flows between them. The value of surface resistivity for a material is independent of the area over which it is measured. The units of surface resistivity are the Ohm (Ω), although it is common practice to quote values in units of ohm per square. A comparative bar chart of surface resistivities for some high performance engineering polymers at ambient temperatures is shown in Figure 24. This shows that natural VICTREX 450G has a surface resistivity typical of high performance materials.

Figure 24: Surface Resistivities for Various Engineering From the data reported in Figure 25, natural VICTREX Polymers Tested at 25°C (77°F) with 50% Humidity PEEK has a typical loss-tangent profile compared with other high performance materials over the temperature

2.5E+16

range tested.

Surface Resistivity /

2E+16

1.5E+16

1E+16

5E+15

VICTREX 450G Polyimide PTFE PET

RELATIVE PERMITTIVITY AND DIELECTRIC

DISSIPATION FACTOR

23°C (73°C)

VICTREX PEEK can be used to form components which

support and insulate electronic devices. Often these components experience alternating potential-field

strengths at various frequencies over wide temperature

and environmental changes. The material response to these changes may be evaluated using IEC 250. This

120°C (248°F) 160°C (320°F)

Loss Tangent

200°C (390°F)

1E-1

250°C (482°F)

1E-2

standard test evaluates the relative permittivity of a material and relates sinusoidal potential-field changes to a complex permittivity and a dielectric dissipation factor (tan δ). The permittivity of a material (εr) is defined as the ratio of the capacitance of a capacitor in which the space between and around is filled with that material (Cx) and the capacitance of the same electrode system in a vacuum (Cvac).

εr = Cx / Cvac The relative permittivity in an alternating current forms the complex relationship,

εr* = εr' -jεr'' where εr' is the storage permittivity, j is a complex number and εr'' is the imaginary loss permittivity. When such The comparative plot shown in Figure 26 displays the excellent electrical performance of natural VICTREX PEEK over nine decades of applied frequency. Although many of the electrical properties of the material are described as typical of thermoplastic materials, VICTREX PEEK retains these excellent insulating properties over a wide range of temperature and frequency.

Figure 25: Loss Tangent of VICTREX 450G at Temperatures Between 23°C (73°F) and 250°C (482°F) at Frequencies Between 50 Hz and 100 MHz

1E+0

1E-3

1E-4 1E+1 1E+2 1E+3 1E+4 1E+5 1E+6 1E+7 1E+8 Frequency / Hz

Figure 26: Relative Permittivity of VICTREX 450G at Temperatures Between 23°C (73°F) and 250°C (482°F) at Frequencies Between 50 Hz and 100 MHz

5.5

23°C (73°C) 120°C (248°F)

5.0

160°C (320°F)

a potential difference is applied to a viscoelastic materi

al the finite response time induced by the material

means that there is a phase-lag (δ) in the measured capacitance. This phase-lag may be described by the

relationship,

Cx = Co (sin ωt + δ)

Dielectric Constant

200°C (390°F) 250°C (482°F)

4.5

4.0

3.5

where Co is the maximum capacitance measured. Therefore, an expression for the viscoelastic phase lag (tan δ) can be derived from consideration of the storage and loss permittivities.

tan δ = εr'

'' / εr Low values of tan δ are desirable for component operating conditions as this implies that the material will continuously insulate without excessive losses. The value of tan δ over wide temperature and frequency ranges is shown in Figures 25 and 26 respectively.

3.0
1.0E+01 1.0E+02 1.0E+03 1.0E+04 1.0E+05 1.0E+06 1.0E+07 1.0E+08
Frequency / Hz

Figure 27: Wear Factor at 200°C (390°F), with 3 m s-1

TRIBOLOGY

(600 ft min-1) and 20 kg (44 lb) Load for some of the Highest Tribological Performance Materials

Tribology may be defined as the interaction of contacting surfaces under an applied load in relative motion. 1 If the surface of a material is viewed on a microscopic

Wear Factor 10-6 / MPa h m min-1

scale, a seemingly smooth finish is, in fact, a series of

0.8

asperities. Therefore, if two materials are then placed in contact and moved relative to one another, the

asperities of both surfaces collide. The removal of asperities may be considered as wear, and resistance to

0.6

the motion as a frictional force. VICTREX PEEK, and

0.4

compounds based on VICTREX PEEK, are used to form tribological components due to their outstanding resis

0.2

tance to wear under high pressure (p) and high velocity

(v) conditions. The friction and wear behaviour of a material may be evaluated using one of several test geometries. The data given in this publication were generated in unlubricated conditions using an AMSLER pad on ring test rig. The rotating disc used in this apparatus was 60 mm (2.36 in) in diameter with a 6 mm

(0.236 in) depth and was ground to a 0.4 µm Ra surface finish.

WEAR

The useful life of components which function in tribologically demanding environments is governed by the wear. The performance of a material may be quantified by evaluating either the specific wear rate (υsp),

V

υsp = ____

F .D where V represents the volumetric loss of the sample,

F the force applied and D the total sliding distance, or the specific wear factor (k),

k = dh . 1

dt p .v where dh/dt represents the rate of height loss measured in the sample. The lower the wear rate or wear factor, the more resistant a material is to tribological

0 Graphite Porous Bronze VICTREX 450FC30 Polyimide + 15% Graphite

and F may vary for VICTREX PEEK components which experience ‘real-life’ tribological contacts. This variable force may be considered in terms of two elements: a deformation term involving the dissipation of energy in a local area of asperity contact, and an adhesion term originating from the contact of the slider and the counterface.

VICTREX 450FC30, a special tribological grade, contains optimum levels of PTFE and graphite to reduce and maintain the coefficient of friction at a low value. In addition, the carbon fiber reinforcement enhances the mechanical and thermal performance of the material. A comparative bar chart of high tribological performance materials is shown in Figure 28.

Figure 28: Coefficient of Friction for a Range of Materials at 200°C (390°F), with v = 3 m s-1 (600 ft min-1) and 20 kg (44 lb) Load

0.5

interactions. Figure 27 shows a comparative wear factor

0.4

Coefficient of Friction / µ

bar chart of some of the materials commonly used in

demanding tribological situations. These data show

that VICTREX 450FC30 has an extremely low wear factor for a thermoplastic material.

FRICTION

The friction of a sliding tribological contact may be defined as the tangential force (F) required to move a

0.3

0.2

0.1

slider over a counterface, 0 F= µ N

where N represents the normal force and µ is the coefficient of friction. Values of µ quoted for polymers vary with the thermal characteristics of the material and experimental conditions. Therefore, the value of µ The measured variation in the value of the coefficient of friction with temperature for VICTREX 450FC30 is shown in Figure 29.

Temperature / °F

Figure 29: Variation of the Coefficient of Friction with Temperature for VICTREX 450FC30, v = 0.17 m s-1 (34 ft min-1) and 19 kg (41 lb) Load

0.9 1 122 Coefficieµ 0.5 0.6 0.7 0.8 172 222 272 322 372 422 472
50 nt of Friction / 0 0.1 0.2 0.3 0.4 100 150 200 250

Temperature / °C

LIMITING PRESSURE AND VELOCITY

Materials used for tribologically sensitive applications are classified by defining the limiting product of pressure x velocity (Lpv). Limiting behaviour is taken as the pv condition under which the material exhibits excessive wear, interfacial melting or crack growth from ploughing. Materials in critical tribological interactions may undergo either a pressure or a velocity induced failure. A pressure induced failure occurs when the loading of a sample increases to the point at which the sample undergoes fatigue crack growth from an asperity removal. A velocity induced failure occurs at the point when the relative motion between surfaces is such that thermal work at the material interface is sufficient to catastrophically increase the wear rate. Comparative Lpv charts of materials commonly used to form bearings are shown in Figures 30 and 31. The experimental conditions were chosen to reflect realistic bearing conditions for in-engine applications.

VICTREX PA 6/6 + Graphite Polyimide + 15% Graphite Porous

450FC30 + Glass Graphite Bronze

(68°F), with v = 3 m s-1 (600 ft min-1)

Under these specific conditions, VICTREX PEEK is shown to be among the highest performance materials.

Glass Graphite PTFE Bronze

However, bearings for many applications are produced in large numbers where production speed and costs are critical. VICTREX PEEK is the only high performance tribological material which can be injection moulded to form finished components without further thermal treatment. Although Lpv values are a useful guide to comparative tribological performance, there are no absolute values because identical experimental conditions cannot be reproduced. Comparative data for high performance tribological materials at ambient and elevated temperatures are shown in Table 2.

Table 2: Comparative Tribological Data, with v = 183 m min-1 (600 ft min-1)

Material 20°C (68°F) 200°C (390°F)
Load kg (lbs) Lpv MPa m min-1 µ(a) Wear rate(b) µm min-1 (in min-1) Load kg (lbs) Lpv MPa m min-1 µ(a) Wear rate(b) µm min-1 (in min-1)
VICTREX 450FC30 40 (88) 794 0.17 3.2 (.000125) 40 (88) 622 0.14 132 (0.0052)
VICTREX 450G 8 (17.6) 145 0.58 7.5 (.000295) 8 (17.6) 147 0.51 150 (0.0059)
VICTREX 450CA30 22 (48.4) 376 0.28 3.8 (.000148) 13 (28.6) 445 0.25 -
PA 6/6 + Graphite, Glass Fiber 10 (22) 71 0.76 - - - - -
Polyimide, Graphite 30 (66) 895 0.24 0.84 (.000033) 20 (44) 670 0.21 125 (0.0049)
POM 5 (11) 71 0.34 - - - - -
Carbon Filled PTFE 25 (55) 447 0.25 4.2 (.000164) - - - -
White Metal(c) 15 (33) 265 0.16 - - - - -
Oil Impregnated Bronze(c) 25 (55) 804 0.09 3.5 (.000138) - - - -
Graphite Porous Bronze(c) - - - - 20 (44) 403 0.25 75 (0.003)

(a) Average of the coefficient of friction at Lpv and 50% Lpv. (b) Wear rate at 50% Lpv. (c) One time lubrication with a mineral oil.

ENVIRONMENTAL RESISTANCE

VICTREX PEEK can be used to form components which function in aggressive environments or need to withstand frequent sterilisation processes. The useful service life of such devices depends on retention of the physical properties.

GAS PERMEATION

The permeability of crystalline and amorphous VICTREX PEEK-based film is shown in Table 3 for a variety of common gasses. It provides better barrier properties than many other commonly used polymeric films.

Crystalline and amorphous VICTREX PEEK-based film.

Table 4: A Comparison of the Mechanical Properties of VICTREX PEEK Materials after Conditioning in Steam at 200°C (392°F) and 1.4 MPa (200 psi)

Property Standard Control Time/hours
75 350 1000 2000 2500
Tensile Strength/MPa (psi) VICTREX 150G/151G VICTREX 450G VICTREX 450GL30 ISO 527 50 mm min-1 (2 in min-1) 50 mm min-1 (2 in min-1) 5 mm min-1 (0.2 in min-1) 85 (12,325) 92 (13,340) 134 (19,430) 86 (12,470) 99 (14,355) 98 (14,210) 78 (11,310) 97 (14,065) 93 (13,485) 84 (12,180) 97 (14,065) 90 (13,050) 86 (12,470) 97 (14,065) 92 (13,340) -97 (14,065) 89 (12,905)
Flexural Strength/MPa (psi) VICTREX 150G/151G VICTREX 450G VICTREX 450GL30 ISO 178 156 (22,620) 142 (20,590) 216 (31,320) 175 (25,375) 162 (23,490) 177 (25,665) 153 (22,185) 165 (23,925) 164 (23,780) 130 (18,850) 159 (23,055) 167 (24,215) 155 (22,475) 169 (24,505) 167 (24,215) 130 (18,850) 156 (22,620) 166 (24,070)
Flexural Modulus/GPa (psi) VICTREX 150G/151G VICTREX 450G VICTREX 450GL30 ISO 178 3.8 (551,000) 3.7 (536,500) 9.8 (1,421,000) 3.8 (551,000) 4 (580,000) 9.1 (1,319,500) 3.1 (449,500) 4 (580,000) 8.3 (1,203,500) 3.1 (449,500) 3.8 (551,000) 9 (1,305,000) 4 (580,000) 4 (580,000) 8.9 (1,290,500) 3.7 (536,500) 3.6 (522,000) 8.7 (1,261,500)
Elongation at Break/% VICTREX 150G/151G VICTREX 450G VICTREX 450GL30 ISO 527 50 mm min-1 (2 in min-1) 50 mm min-1 (2 in min-1) 5 mm min-1 (0.2 in min-1) 4 40 3 4 15 3 3 15 3 3 12 3 4 7 3 2 9 3

HYDROLYSIS RESISTANCE

VICTREX PEEK and compounds are not chemically attacked by water or pressurised steam. These materials retain a high level of mechanical properties when continuously conditioned at elevated temperatures and pressures in steam or water. The compatibility of these materials with steam was evaluated by conditioning injection moulded tensile and flexural bars at 200°C (392°F) and 1.4 MPa (200 psi) for the times indicated in Table 4. The data demonstrates the ability of components made from VICTREX PEEK to continuously operate in, or be frequently sterilised by, steam. The initial increase in the mechanical properties is due to the relaxation of moulded-in stresses and further developments in crystallinity due to thermal treatment.

CHEMICAL RESISTANCE

VICTREX PEEK is widely regarded to have superb chemical resistance and is regularly used to form components which function in aggressive environments or need to withstand frequent sterilisation processes. For specific information about the suitability of VICTREX PEEK for a particular chemical environment please contact a Victrex representative at your local office (details on the back cover of this guide). Alternatively, a chemical resistance list is available for download from our website.

RADIATION RESISTANCE

Thermoplastic materials exposed to electromagnetic or particle based ionizing radiation can become brittle. Due to the energetically stable chemical structure of VICTREX PEEK, components can successfully operate in, or are frequently sterilised by, high doses of ionizing radiation. A comparative bar chart of thermoplastic materials is shown in Figure 32, where the recorded dose is at the point at which a slight reduction in flexural properties is observed.

Figure 32: The Oxidative Gamma Radiation Dose at which a Slight Deterioration of Flexural Properties Occurs

Gamma Dose / Rads

1E+10 1E+9 1E+8 1E+7 1E+6 1E+5 1E+4 1E+3

VICTREX PS Epoxy Silicone Polyimide PSU PC Phenolic FEP POM PTFE 450G

The data in Figure 32 show that the VICTREX PEEK has a greater resistance to radiation damage than the other materials tested.

OUTGASSING CHARACTERISTICS OF VICTREX PEEK GRADES

VICTREX PEEK GRADE %TML %CVCM %WVR
VICTREX 450G 0.26 0.00 0.12
VICTREX 450GL30 0.20 0.00 0.08
VICTREX 450CA30 0.33 0.00 0.12
  • Total Mass Loss (TML) – the total mass of material that is outgassed from the test sample when maintained at a specific temperature for a specific time.
  • Collected Volatile Condensable Material (CVCM) – is the quantity of outgassed matter from the test sample which is condensed and collected at a given temperature and time.
  • Water Vapor Regained (WVR) – is the mass of water regained by the test sample after conditioning at 50% RH and 23°C (74°F) for 24 hours.

Data was generated in accordance with ASTM E-595-84. VICTREX PEEK was heated to 125°C (257°F) for 254 h under a vacuum of 5x10-5 Torr. All values are expressed as a percentage of the weight of the test sample. Acceptable limit for TML is 1.0% maximum and for CVCM is 0.1% maximum.

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