Fabric for air bag
A technology for fabrics and airbags, applied in the directions of fabrics, textiles, textiles, and papermaking, etc., can solve the problems of not involving the slippage resistance of the fabric, the slippage of the stitched part is large, and the incomprehension is not possible.
- Summary
- Abstract
- Description
- Claims
- Application Information
AI Technical Summary
Problems solved by technology
Method used
Image
Examples
Embodiment 1
[0040] The nylon 66 raw yarn with a total fineness of 470 dtex, a number of 72 threads, and a circular cross section is used, the breaking strength is 39.5N, and the breaking elongation is 23.5%. After the sample warping machine is warped, a plain weave fabric is woven with a water jet loom, and dried at 80°C to obtain a fabric with a warp yarn density of 53 yarns / inch and a weft yarn density of 53 yarns / inch. The properties of the base fabric were evaluated and shown in Table 1.
Embodiment 2
[0042] The nylon 66 raw yarn with a total fineness of 470 dtex, a number of 136 threads, and a circular cross-section is used. The breaking strength is 40.5N and the breaking elongation is 23.0%. After the sample warping machine is warped, a plain weave fabric with a density of 53 threads / inch is woven with a water jet loom, and the woven safety zone airbag fabric is heat-set and processed. The results of the processed airbag fabric are shown in Table 1.
Embodiment 3
[0044] The nylon 66 raw yarn with a total fineness of 350 dtex, 72 yarns and a circular cross-section is used, the breaking strength is 29.6N, and the breaking elongation is 23.5%. After being warped by a warping machine, a plain weave fabric is woven with a water jet loom, and dried at a temperature of 80°C to obtain a fabric with a warp yarn density of 59 yarns / inch and a weft yarn density of 59 yarns / inch. The properties of the base fabric were evaluated and shown in Table 1.
PUM
| Property | Measurement | Unit |
|---|---|---|
| elongation at break | aaaaa | aaaaa |
| elongation at break | aaaaa | aaaaa |
Abstract
Description
Claims
Application Information
Login to View More 