1985
DOI: 10.1115/1.3169092
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Analysis of Wire Ropes With Internal-Wire-Rope Cores

Abstract: Stresses in the individual wires of complex wire rope are determined for rope constructions having an internal-wire-rope (IWRC). The ropes may be pulled, twisted, and bent over a sheave or drum. The effects of friction are neglected. Specific results for a 6 × 25 filler-wire IWRC rope that is prevented from twisting indicate that the maximum stresses (exclusive of contact stresses) are typically 1.5 to 3 times as large as the nominal rope stress based on rope load and total metallic area.

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Cited by 58 publications
(20 citation statements)
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“…In the past years, different linear analytical models were presented to predict the mechanical behaviors of the spiral strands [1][2][3][4][5][6], but the precision of the models are very limited due to the simplifications used. In these models, some influencing factors are ignored, such as the complex helical configuration, Poisson's ratio effect, symmetric stiffness matrix, torsion, bending, contact, friction and local plastic yielding of wire ropes.…”
Section: Introductionmentioning
confidence: 99%
“…In the past years, different linear analytical models were presented to predict the mechanical behaviors of the spiral strands [1][2][3][4][5][6], but the precision of the models are very limited due to the simplifications used. In these models, some influencing factors are ignored, such as the complex helical configuration, Poisson's ratio effect, symmetric stiffness matrix, torsion, bending, contact, friction and local plastic yielding of wire ropes.…”
Section: Introductionmentioning
confidence: 99%
“…This formulation leads to a set of non-linear equations. A more recent paper by Philips and Costello (1985) presents a solution of the same theory applied to wire rope with internal wire rope cores. Kumar and Cochran (1987) have developed a linearized form of this theory, leading to a closed-form expression for axial stiffness coefficients.…”
Section: Earlier Modelsmentioning
confidence: 94%
“…The elastic constants of the individual sheets along their principal direction of orthotropy may be transformed by -y 2 s' 12 6 6 + s11s22s66 (16) The stiffness coefficients for a spiral strand are then given by where A j = net steel area of layer of wires j with n = number of layers of wires excluding the core wire whose area is A,,,,; l j is equal to 1 for the right-hand lay and -1 for the left-hand lay, and an absolute magnitude …”
Section: (5)mentioning
confidence: 99%