Nonwoven fabric and fiber product
a nonwoven fabric and fiber technology, applied in the field of spun bonding nonwoven fabrics, can solve the problems of easy end breakage, unstable spinnability and moldability, etc., and achieve the effect of improving the flexibility of nonwoven fabrics and the stability of spinning fibers
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example 1
(Preparation of Core Component)
[0123]80% by mass of a propylene-based resin (B) (PP3155, manufactured by ExxonMobil Chemical) having a melt flow rate (MFR), as measured under conditions at a temperature of 230° C. and a load of 2.16 kg in conformity with ASTM D1238, of 36 g / 10 min was compounded with 20% by mass of a propylene-based resin (A) (L-MODU (a registered trademark) S901, manufactured by Idemitsu Kosan Co., Ltd.) having a melt flow rate (MFR), as measured under conditions at a temperature of 230° C. and a load of 2.16 kg in conformity with JIS K7210, of 50 g / 10 min and a melting point of 70° C., thereby preparing a core component.
(Preparation of Sheath Component)
[0124]Only an ethylene-based resin (ASPUN 6834, manufactured by The Dow Chemical Company) having a melt flow rate (MFR), as measured under conditions at a temperature of 190° C. and a load of 2.16 kg in conformity with ISO 1133, of 17 g / 10 min and a melting point of 130° C. was used, thereby preparing a sheath compo...
example 2
[0133]A nonwoven fabric was molded in the same manner as that in Example 1, except that in Example 1, a material obtained by mixing 50% by mass of the propylene-based resin (B) and 50% by mass of the propylene-based resin (A) was used as the core component, and the cabin pressure was changed to 7,500 Pa, and then evaluated in the same way. The results are shown in Tables 1 and 2.
example 3
[0136]A nonwoven fabric was molded in the same manner as that in Example 1, except that in Example 1, the core component and the sheath component were discharged in a mass ratio of 50 / 50 and spun, and the cabin pressure was changed to 6,000 Pa, and then evaluated in the same way. The results are shown in Tables 1 and 2.
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