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Displacement, axial

The structure of PBT fibres, has not been completely resolved although efforts are continuing using diffraction analysis, For example Adams et al. 95) have interpreted the x-ray diffraction patterns of oriented PBT fibres in terms of a nematic arrangement of molecules which are treated as periodic cylinders packed in an hexagonal array. The cylinders are oriented parallel to each other but are arbitrarily displaced axially. Unfortunately although the model explains many features of the diffraction pattern it predicts a fibre density which is well below the observed experimental value. [Pg.88]

This would tend to indicate that the shaft and drums are being displaced axially during the clutching or winding operations ... [Pg.18]

A positive value of n implies a focusing effect. The value of n varies with the radius r (it is zero at the center of the magnet) and it can be used to calculate the motion of particles in the radial and axial directions at a particular radius. Ignoring the detailed discussion, particles displaced axially or radially from their equilibrium orbit will sense a force which is proportional to the displacement (like a simple harmonic oscillator) and will perform stable axial and radial oscillations, which are known as betatron oscillations. These oscillations are stable when n lies between 0 and 1. Any ion leaving the ion source in a direction not in the median plane and not on the equilibrium orbit will make axial and radial betatron oscillation. [Pg.2358]

Fig. 7.5 Lateral strength-lateral displacement (axial stress = 0.5 MPa)... Fig. 7.5 Lateral strength-lateral displacement (axial stress = 0.5 MPa)...
Plastic deformation of fibrous structure slightly deforms the microfibrils by shear displacement of chains in the folded chain crystal blocks thus reducing the sharpness of the meridional maximum of It displaces axially the fibrils and... [Pg.216]

The compression test has been performed on an (7, 7) armchair nanotube having 24 repeat units. Total number of atoms in the configuration was 672. The diameter of CNT was 1 nm while its length was 6 nm giving the aspect ratio (1/d) 6. The atoms of top four rings were displaced axially by -0.0005 A in every deformation stqi. After each deformation step the CNT is allowed to equilibrate for 100... [Pg.1181]

An alternative type of downhole mud motor is the mud turbine, (multistage axial flow turbine) which directly drives the bit. The tool consists of an upper section containing the turbine blades and lower section with bearings. As mud is pumped through the upper section the blades are turned. Turbines are designed to rotate at higher speed than the displacement motor. The higher rotation speed requires diamond or composite bits. [Pg.48]

Tables I and 2 show the experimental results obtained for axial and transversal displacements respectively, where % is the displacement and Xv. is the displacement measured using our experimental. setup. Tables I and 2 show the experimental results obtained for axial and transversal displacements respectively, where % is the displacement and Xv. is the displacement measured using our experimental. setup.
CompoundShrinka.g e. In its simplest form (Fig. 8a) compound shrinkage consists of machining the inner radius of an outer component I, (Qp so that it is smaller than the outer radius of an inner component II, The difference between the two is known as the radial interference 5. To assemble the cylinders, outer component I is heated and/or inner component II cooled so that the outer component can be sHpped over the inner as shown in Figure 8b. When the temperature of the assembly returns to ambient, a compressive stress (pressure) is generated across the interface which simultaneously compresses the inner and expands the outer component and, in so doing, displaces radius (r/j by Uj and radius ( jj by U, Unfortunately, it is difficult to carry out this operation without setting up stresses in the axial direction (32). [Pg.82]

The radial interference, 5, necessary to achieve pressure P may be calculated from the radial displacements Uj and Ujj generated during assembly, assuming that the shrinkage is carried out without generating an axial stress in either component. [Pg.83]

Whereas the total dynamic head developed by a centrifugal, mixed-flow, or axial-flow pump is uniquely determined for any given flow by the speed at whicdi it rotates, positive-displacement pumps and those which approach positive displacement will ideally produce whatever head is impressed upon them by the system restrictions to flow. Actually with slippage neglecTed, the maximum head attainable is determined by the power available in the drive and the strength of the pump parts. An automatic relief valve set to open at a safe pressure... [Pg.909]

To be able to decide which type of compressor would best fit the job, we should first divide the compressors into three main categories positive displacement, centrifugaf and axial flow In general terms, positive displacement compressors are used for high pressure and low flow characteristics centrifugal compressors are used for medium to high pressure dehvery and medium flow and axial flow compressors are low pressure and high flow... [Pg.923]

Many users consider rotaiy compressors, such as the Rootes -type blower, as turbomachines because their behavior in terms of the rotor dynamics is very close to centrifugal and axial flow machineiy. Unhke the reciprocating machines, the rotary machines do not have a veiy high vibration problem but, like the reciprocating machines, they are positive displacement machines. [Pg.928]

The primary cause of efficiency losses in an axial-flow turbine is the buildup of boundary layer on the blade and end walls. The losses associated with a boundary layer are viscous losses, mixing losses, and trailing edge losses. To calculate these losses, the growth of the boundary layer on a blade must be known so that the displacement thickness and momentum thickness can be computed. A typical distribution of the displacement and momentum thickness is shown in Figure 9-26. The profile loss from this type of bound-ary-layer build-up is due to a loss of stagnation pressure, which in turn is... [Pg.363]


See other pages where Displacement, axial is mentioned: [Pg.1014]    [Pg.168]    [Pg.140]    [Pg.452]    [Pg.452]    [Pg.533]    [Pg.278]    [Pg.171]    [Pg.355]    [Pg.94]    [Pg.171]    [Pg.593]    [Pg.614]    [Pg.1014]    [Pg.168]    [Pg.140]    [Pg.452]    [Pg.452]    [Pg.533]    [Pg.278]    [Pg.171]    [Pg.355]    [Pg.94]    [Pg.171]    [Pg.593]    [Pg.614]    [Pg.336]    [Pg.604]    [Pg.85]    [Pg.77]    [Pg.270]    [Pg.441]    [Pg.442]    [Pg.418]    [Pg.76]    [Pg.65]    [Pg.65]    [Pg.192]    [Pg.401]    [Pg.330]    [Pg.331]    [Pg.268]    [Pg.113]    [Pg.475]    [Pg.1143]    [Pg.26]    [Pg.127]    [Pg.155]   
See also in sourсe #XX -- [ Pg.4 ]




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Axial load-displacement responses

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