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Creep factors

Increase of creep factors with time, determined for different adhesive layers in the three thickness classes (nd = not determined because of failure)... [Pg.134]

Loss of stability from increased second-order effects (i.e. changes in the effects of actions or in the forces in members resulting from deformation of the components, members or of the structure as a whole) due to creep may be dealt with by using ultimate limit state loads and the long-term structural stiffness, e.g. with a creep factor applied to the modulus of elasticity. [Pg.280]

The long-term stress, including creep factors and safety factors, that is used in designing structural fabrication. Treating plastic materials to minimize their accumulation of static electricity. [Pg.2211]

EN 761 Glass-reinforced thermosetting plastics (GRP) pipes - determination of the creep factor under dry conditions. [Pg.91]

The 3-month creep factors, obtained from both flexural and compressive creep tests, were 0.5 in compressive and 0.1 in flexural. In addition, in rPET polymer concrete the stable creep domain extends to stress ratios of 0.4 in flexural and 0.3 in compression. As the imposed loads increase beyond these stress ratios, the rPET polymer concrete show a progressive tendency to shift into catastrophic creep. [Pg.88]

One human element had been that the engineer (staff/technical) writing the specifications had not considered the creep factor of pure... [Pg.84]

In general, more highly oriented and therefore higher modulus fibers tend to exhibit lower shrinkage and less creep. Creep is an important factor in the control of tire dimensions during service and in certain aspects of tire appearance (30). [Pg.83]

For straight metal pipe under internal pressure the formula for minimum reqiiired w thickness is applicable for D /t ratios greater than 6. Tme more conservative Barlow and Lame equations may also be used. Equation (10-92) includes a factor Y varying with material and temperature to account for the redistribution of circumferential stress which occurs under steady-state creep at high temperature and permits slightly lesser thickness at this range. [Pg.981]

Metals Successful applications of metals in high-temperature process service depend on an appreciation of certain engineering factors. The important alloys for service up to I,I00°C (2,000°F) are shown in Table 28-35. Among the most important properties are creep, rupture, and short-time strengths (see Figs. 28-23 and 28-24). Creep relates initially applied stress to rate of plastic flow. Stress... [Pg.2464]

Nickel and its alloys form another important class of non-ferrous metals (Table 1.3). The superb creep resistance of the nickel-based superalloys is a key factor in designing the modern gas-turbine aero-engine. But nickel alloys even appear in a model steam engine. The flat plates in the firebox must be stayed together to resist the internal steam pressure (see Fig. 1.3). Some model-builders make these stays from pieces of monel rod because it is much stronger than copper, takes threads much better and is very corrosion resistant. [Pg.7]

Polymers are a little more complicated. The drop in modulus (like the increase in creep rate) is caused by the increased ease with which molecules can slip past each other. In metals, which have a crystal structure, this reflects the increasing number of vacancies and the increased rate at which atoms jump into them. In polymers, which are amorphous, it reflects the increase in free volume which gives an increase in the rate of reptation. Then the shift factor is given, not by eqn. (23.11) but by... [Pg.244]

In compression, of course, the strength is greater. Most ceramics are about fifteen times stronger in compression than in tension, for the reasons given in Chapter 17. For ice the factor is smaller, typically six, probably because the coefficient of friction across the crack faces (which rub together when the ceramic is loaded in compression) is exceptionally low. At stresses below 6 MPa, ice loaded in compression deforms by creep at 6 MPa it crushes, and this is the maximum stress it can carry. [Pg.305]

Creep becomes an important factor with different metals and alloys at different temperatures. For example, lead at room temperature behaves similarly to carbon steel at 1,000°F and to certain of the stainless steels and superalloys at 1,200°F and higher. [Pg.260]

Furnace tubes, piping, and exchanger tubing with metal temperatures above 800°F now tend to be an austenitic stainless steel, e.g., Type 304, 321, and 347, although the chromium-molybdenum steels are still used extensively. The stainless steels are favored beeause not only are their creep and stress-rupture properties superior at temperatures over 900°F, but more importantly because of their vastly superior resistance to high-temperature sulfide corrosion and oxidation. Where corrosion is not a significant factor, e.g., steam generation, the low alloys, and in some applications, carbon steel may be used. [Pg.261]

Pressure Vessels. Refineries have many pressure vessels, e.g., hydrocracker reactors, cokers, and catalytic cracking regenerators, that operate within the creep range, i.e., above 650°F. However, the phenomenon of creep does not become an important factor until temperatures are over 800°F. Below this temperature, the design stresses are usually based on the short-time, elevated temperature, tensile test. [Pg.261]

The creep strength of steels is a factor limiting the maximum temperatures for such high-pressure equipment as shells and stirrers of high temperature reactors. Table 3.10 presents creep data for temperatures ranging from 400 to 600°C. The stress for 1% creep in 100,000 hours (which is a design criterion) is accepted to be not less than two-thirds of the creep stresses. [Pg.65]

It was shown earlier that the variation of creep or relaxation moduli with time are as illustrated in Fig. 2.9. If we now introduce temperature as a variable then a series of such curves will be obtained as shown in Fig. 2.58. In general the relaxed and unrelaxed modulus terms are independent of temperature. The remainder of the moduli curves are essentially parallel and so this led to the thought that a shift factor, aj, could be applied to move from one curve to another. [Pg.116]

If a plastic moulding fails in the performance of its normal function it is usually caused by one of two factors - excessive deformation or fracture. In the previous sections it was pointed out that, for plastics, more often than not it will be excessive creep deformation which is the limiting factor. However, fracture. [Pg.119]

Other factors which promote brittleness are geometrical discontinuities (stress concentrations) and aggressive environments which are likely to cause ESC (see Section 1.4.2). The absorption of fluids into plastics (e.g. water into nylon) can also affect their creep rupture characteristics, so advice should be sought where it is envisaged that this may occur. [Pg.135]

Example 2.21 A rod of plastic is subjected to a steady axial pull of 50 N and superimposed on this is an alternating axial load of 100 N. If the fatigue limit for the material is 13 MN/m and the creep rupture strength at the equivalent time is 40 MN/m, estimate a suitable diameter for the rod. Thermal effects may be ignored and a fatigue strength reduction factor of 1.5 with a safety factor of 2.5 should be used. [Pg.144]

A 200 mm diameter plastic pipe is to be subjected to an internal pressure of 0.5 MN/m for 3 years. If the creep rupture behaviour of the material is as shown in Fig. 3.10, calculate a suitable wall thickness for Ae pipe. You should use a safety factor of 1.5. [Pg.165]

A uPVC rod of diameter 12 mm is subjected to an eccentric axial force at a distance of 3 ttun from the centre of the cross-section. If the force varies sinusoidally from — F to f at a frequency of 10 Hz, calculate the value of F so that fatigue failure will not occur in 10 cycles. Assume a safety factor of 2.5 and use the creep rupture and fatigue characteristics described in the previous question. Thermal softening effects may be ignored at the stress levels involved. [Pg.167]

The resistance of rhodium-platinum alloys to corrosion is about the same as or slightly better than that of pure platinum, but they are much more stable at high temperatures. They have excellent resistance to creep above 1 000°C, a factor which largely determines their extensive use in the glass industry, where continuous temperatures sometimes exceeding 1 500°C are encountered. Rhodium additions to platinum reduce appreciably the volatilisation of pure platinum at high temperatures. [Pg.925]


See other pages where Creep factors is mentioned: [Pg.455]    [Pg.132]    [Pg.132]    [Pg.455]    [Pg.132]    [Pg.132]    [Pg.367]    [Pg.85]    [Pg.151]    [Pg.465]    [Pg.315]    [Pg.59]    [Pg.588]    [Pg.643]    [Pg.2518]    [Pg.281]    [Pg.260]    [Pg.260]    [Pg.269]    [Pg.468]    [Pg.200]    [Pg.470]    [Pg.873]    [Pg.24]    [Pg.165]    [Pg.167]    [Pg.167]    [Pg.899]    [Pg.1296]   
See also in sourсe #XX -- [ Pg.321 , Pg.322 ]




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