耐低温无石棉绝热层研制
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河南理工大学机械与动力工程学院

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陈蓉,1968 年出生,工程师,主要从事固体火箭发动机内绝热层材料的研究。

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Preparation of Low Temperature-Resistant and Non-Asbestos Insulation
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    摘要:

    通过添加含卤-锑的阻燃剂、芳纶纤维和增塑剂,研制了一种耐低温无石棉的丁腈绝热层配方 (TI506)。研究了芳纶纤维和增塑剂对绝热层静态烧蚀性能和Tg 的影响,对绝热层材料力学性能、比热容、热 导率等性能进行了测试。结果表明:芳纶纤维浆粕用量为10 ~15 份、芳纶短纤维用量为4 ~6 份时,绝热层烧 蚀性能最佳,线烧蚀率达到45 μm/ s,所选增塑剂DOS 用量为10 份、DBP 或ATBC 用量为20 份时,Tg 可达- 40℃,芳纶纤维制备的丁腈绝热层力学性能及烧蚀性能优良,并满足固体火箭发动机耐-40 ~60℃的环境。

    Abstract:

    A low temperature-resistant and non-asbestos NBR insulation formula named TI506 was preparation by using fire retardant agent containing halogen-Sb,aramid fiber and plasticizer. The effect of content of aramid fiber on erosion perfomance of the insulation was investigated. The effect of content of plasticizer on glass transition temperature( Tg) of NBR insulation was also studied. The results showed that the optimum linearosion rate is 45 μm/ s when the content of aramid fiber pulp is 10 to 15 portions and the content of aramid fiber staple is 4 to 6 portions, and when the content of plasticizer DOS is 10 portions, DBP or ATBC is 20 portions,Tg of the NBR insulation can reach -40℃. In addition, mechanical performance, specific heat capacity and conduction coefficient were tested respectively. The results showed that mechanical and erosion perfomances of the NBR insulation by using aramid fiber are excellent,and it made solid rocket engines endure the condition with the temperature from -40℃ to 60℃.

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陈 蓉,宋 博,伏 玲,寇朝辉.耐低温无石棉绝热层研制[J].宇航材料工艺,2014,44(3):34-37.

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  • 收稿日期:2014-04-09
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  • 在线发布日期: 2016-11-28
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第十一届航天复合材料成形与加工工艺技术中心交流会 征文通知

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