Deepwater Flexible Risers and Pipelines. Yong Bai
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Figure 4.1 Linear-longitudinal profile.
4.2 Theoretical Models
4.2.1 Mechanical Model of Pressure Armor Layer
The benchmark analyzed in this chapter focuses on a composite pipe composed of one pressure armor layer and two conversely winded tensile armor layers embedded into two HDPE layers, as in Figure 4.1.
The theoretical model is based on two main hypotheses.
The contribution of the pressure armor due to the axial strength can be neglected in terms of tensile resistance as the winding angle is close to 90°, as discussed by De Sousa [14]. While, it confers most of the radial stiffness, which highly influences the tensile capacity of the pipe.
The contribution of the HDPE layers to the radial stiffness is neglected. This is possible due to the presence of the pressure armor layer, which gives the main contribution in terms of radial stiffness.
Therefore, the computation in radial direction is reduced into two components: pressure armor layer and tensile armor layers. No initial gaps between different layers are assumed. Winding angle and thickness variations, as well as friction are neglected [15].
The tensile response of the pipe is estimated considering tensile force and external pressure at the same time. The external pressure Pext can be applied directly on the external surface of the outermost tensile armor layer due to the weakness of the surrounding HDPE coat. The tensile contribution of HDPE cylinders is included in calculating the total tensile resistance.
Figure 4.2 Contact pressures between layers mechanical model of pressure armor layer.
According to what has been already discussed in the paper by Yue et al. [15], the authors in the present contribution are considering the same assumptions for the present study. Such simplification does not affect the results which are in very good agreement with the numerical model. Pressures can lead to radial contraction of the layers, which can reduce the tension stiffness of the flexible pipe. It is possible to study tensile and pressure armors separately, in order to get the radial displacements of each layer. Let PC be the contact pressure between the pressure armor and the innermost tensile armor layer, while PW represents the contact pressure between the tensile armor layers, as shown in Figure 4.2, where Rm1 and Rm2 are the mean radii of the tensile armor, R1 and R2 are inner and outer radii of the pressure armor, respectively.
When subjected to tensile loading, the resistance of the flexible pipe is influenced by its radial stiffness due to the helical structure of the layers. The first effort of this chapter is to investigate the radial stiffness of the pressure armor in order to obtain relatively accurate results for this axial problem. Due to its complex shape, which shows different properties in longitudinal and transverse directions, an equivalent theoretical model is used to simplify the computation. The use of negligible elastic modulus in the longitudinal direction is a common practice in the study of equivalent helical structures of flexible pipelines with winding angle close to 90° using analytical approaches. Such null modulus is not considered in the FE analysis (which has actual mechanical properties of the materials used). In fact, the pressure armor layer can be seen as an orthotropic cylinder, with Young’s modulus equal to zero along the longitudinal direction, while in the radial direction its equivalent thickness heq and Young’s modulus Eeq are computed as previously done by De Sousa [14]:
(4.1)
(4.2)
for which, Ieq is the equivalent moment of inertia per unit length, A′ is the cross- sectional area of the pressure armor according to API 17B [17], n is the number of tendons per each layer, Lp is the pitch length, and E is the Young’s modulus of the material. Ieq is computed as in Ref. [1]:
(4.3)
where k is depending on both lay angle and moment of inertia of the cross section, and
Then, as discussed by Yue et al. [15], if the orthotropic cylinder is loaded by radial confining pressure PC induced by the adjacent tensile armor layers, it can be simplified into a planar ring under the same pressure. The equivalent Young’s modulus Eeq and thickness heq for pressure armor can be used in the calculation, where the mean radius for the equivalent cylinder is kept the same as its actual one, as can be seen in Figure 4.4.