The advance engineering methods to plan the behaviour of fused panel

Jevšnik, Simona; Geršak, Jelka; Gubenšek, Ivan

doi:10.1108/09556220510590858

Cited by 9 publications

(14 citation statements)

References 7 publications

(6 reference statements)

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“…The end use of a fused panel drape is dependent on the orientation of the shell fabric and the fusible interlining, as well as on the constructional and mechanical properties of the shell fabric and the fusible interlining separately [3,12,13]. The effect of the layer orientation upon textile systems' tensile and shear behaviour was investigated in our earlier works [14][15][16].…”

Section: Introductionmentioning

confidence: 99%

“…Corresponding author, Kristina.Ancutiene@ktu.lt It is known that the properties of the fiased panel can be predicted on the basis of specified mechanical and physical properties of the shell fabric and fusible interlining [3]. The relationship between certain mechanical properties (tension stiffness, residual extension, bending stiffness, and shear stiffness) of fused composites and those of the outer fabric and fusible interlining were studied by Shishoo et al [4], who found that the mechanical properties of a composite can be predicted on the basis of the corresponding properties of its constituent components.…”

Section: Introductionmentioning

confidence: 99%

“…Tensile and shear properties were defined with an KES-F system, and on their basis recommendations were given for achieving the desirable mechanical reaction of the fused system. The proper selection of the interlining is very important from the standpoint of the quality properties of the produced garments [3].…”

Section: Introductionmentioning

confidence: 99%

See 2 more Smart Citations

Relationship between mechanical properties of bilayer textile systems and their components

Ancutienė¹,

Strazdiene²,

Papreckiene³

2012

Proc. Estonian Acad. Sci.

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The goal of this research was to defme the relationship between the mechanical properties of fused bilayer textile systems and their constituent layers, i.e. fabrics and fusible interlinings. The objects of investigation were four samples of broken twill outer fabric different in thickness (1.01-2.28 mm) and mass per square metre (222-398 gW), and two types of fusible interlinings: nonvowen with longitudinal threads and warp knitted. Fused bilayer textile systems were created by changing the orientation of the fusible interlining by 0°, 45°, and 90° in respect to the outer fabric's warp direction. Mechanical properties (tensile, shear, bending, and surface properties) of fused textile systems and their components were determined using KES-F automated testing devices. The relationships z = z{x,y) between fused textile systems' mechanical parameters (z) and parameters of the outer fabrics (x), as well as parameters of fusible interlinings (y) in 0°, 45°, and 90° orientations were deñned. The obtained theoretical relationships were confirmed experimentally by fmding proper mechanical properties of fusible interlinings (y) on the basis of which bilayer textile systems with mechanical properties (z) falling into the allowable value range of the KES-F quality chart could be composed. Selection of compatible components for fused textile systems with certain mechanical parameters allows avoiding problems in garment manufacturing processes and predicting the appearance and quality of the fmal textile product.

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Section: Introductionmentioning

confidence: 99%

Section: Introductionmentioning

confidence: 99%

See 1 more Smart Citation

Relationship between mechanical properties of bilayer textile systems and their components

Ancutienė¹,

Strazdiene²,

Papreckiene³

2012

Proc. Estonian Acad. Sci.

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“…The results of the work of Sacevicˇiene _ and Masteikaite _ [17] have shown that method using the loop of the pear shape allows testing the larger variety of coated and laminated fabrics but received results also confirm that this method is less sensitive due to insignificant differences between results of different fabrics. The bending rigidity characteristics of multilayered fabrics were different as result of bending them in face and in back sides in most cases [22,23]. In some cases this difference reached till 7 times.…”

Section: Introductionmentioning

confidence: 96%

Compressed loop method for the bending behaviour of coated and laminated fabrics analysis

Masteikaitė

Sacevičienė

Čironienė

2012

Journal of Industrial Textiles

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Fabric stiffness is one of the most important parameters in estimating the wear and comfort properties of multilayered textile materials. The characteristics of bending stiffness may be determined using different test methods. The aim of this work was to apply the compress hanging loop method for the evaluation of stiffness of coated and laminated fabrics. In order to achieve this purpose an extension machine appropriately equipped with a special device for specimen fixing has been used in this work. The initial and ultimate geometrical characteristics of the loop, and also the forces that were necessary to compress the loops to a certain degree were determined in this work. The investigation reveals that the force, which is necessary to compress the loop to a stated degree, is different not only for specimens cut in various directions but also for those specimens that are of different size. Therefore, the deformation properties are dependent on the material structure and testing conditions. The results indicate that coated and laminated fabrics with larger surface weight were more resistant to compression force. Also for these fabrics the larger difference of compressing force values was determined when the polymer film had been in different loop sides. It should be noted that analysis of geometrical compressed loop characteristics showed that for all tested specimens the upper and lower ratios of formed semicircles were not equal. The investigation reveals that the hanging compressed loop method allows extending the range of tested materials, which include rigid and less rigid fabrics.

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“…Shishoo et al [14] introduced regression equations and investigated the relationship of mechanical properties theoretically and experimentally. Jevsˇnik et al [15] analyzed some mechanical properties and parameters of drapability using different methods from two different points of the research area, using the finite element method. Jevsˇnik and Gersˇak [16] analyzed the dependence of the constructional parameters of fabrics on the properties of fused panels.…”

Section: Introductionmentioning

confidence: 99%

Prediction of bending rigidity for laminated fabric with adhesive interlining by a laminate model considering tensile and in-plane compressive moduli

Kim

Inui

Takatera

2012

Textile Research Journal

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The purpose of this study is to predict bending rigidity of laminated fabric with adhesive interlining considered tensile and in-plane compressive moduli. The predicting method considering those moduli was proposed by theoretical derivation based on laminate model. Tensile and in-plane compressive moduli of neutral surface for face fabric and adhesive interlining respectively before laminating and modulus for bending rigidity were considered independently. The calculating equation for in-plane compressive modulus was proposed from the relationship between bending rigidities and tensile properties. The proposed predicting method was verified experimentally. Bending rigidities, tensile properties and thicknesses of adhesive interlinings, face fabrics and laminated fabrics with adhesive interlinings were measured by KES-FB system. The in-plane compressive moduli of adhesive interlinings were calculated by the proposed equation with the results of tensile properties for face fabrics. With the results of tensile and in-plane compressive moduli, the bending rigidities of laminated fabric with adhesive interlinings were calculated. The predicted bending rigidities considered with measured tensile properties and calculated in-plane compressive moduli were precisely closer to experimental results than the ones of the laminated model from our previous study. Therefore, this model gives a new way to predict bending rigidity of laminated fabric with adhesive interlining.

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The advance engineering methods to plan the behaviour of fused panel

Cited by 9 publications

References 7 publications

Relationship between mechanical properties of bilayer textile systems and their components

Relationship between mechanical properties of bilayer textile systems and their components

Compressed loop method for the bending behaviour of coated and laminated fabrics analysis

Prediction of bending rigidity for laminated fabric with adhesive interlining by a laminate model considering tensile and in-plane compressive moduli

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