固体火箭技术
固體火箭技術
고체화전기술
JOURNAL OF SOLID ROCKET TECHNOLOGY
2009年
5期
578-582
,共5页
姚冬梅%程文%邹武%郑金煌
姚鼕梅%程文%鄒武%鄭金煌
요동매%정문%추무%정금황
含硅芳基乙炔%固化%炭化机理%热分解动力学
含硅芳基乙炔%固化%炭化機理%熱分解動力學
함규방기을결%고화%탄화궤리%열분해동역학
PSAA%cure%pyrolytic mechanism%thermal pyrolysis kinetics
通过FTIR、DSC、TG和XRD等分析了新型含硅芳基乙炔树脂的组成、固化反应、炭化过程、炭化机理及热分解动力学.结果表明,树脂主链上含有Si元素,在222℃发生Diels-Alder固化反应;固化树脂的起始热分解温度为380 ℃,900 ℃的残留率为89.5%.热解动力学分析表明,树脂的炭化分为几个阶段,在250~445 ℃阶段,为引发阶段,结构变化小;450~725 ℃为热分解阶段,聚合物的主链破坏并转变为玻璃态炭结构;在830~855 ℃是芳环发生脱氢交联反应引起的放热阶段;860~895 ℃为碳化物逐渐向乱层石墨结构转变,此阶段以后热稳定性高.XRD和拉曼光谱表明, 1 500 ℃处理后出现SiC峰,2 200 ℃处理后出现石墨峰,表明材料在高温处理时可发生部分石墨化.
通過FTIR、DSC、TG和XRD等分析瞭新型含硅芳基乙炔樹脂的組成、固化反應、炭化過程、炭化機理及熱分解動力學.結果錶明,樹脂主鏈上含有Si元素,在222℃髮生Diels-Alder固化反應;固化樹脂的起始熱分解溫度為380 ℃,900 ℃的殘留率為89.5%.熱解動力學分析錶明,樹脂的炭化分為幾箇階段,在250~445 ℃階段,為引髮階段,結構變化小;450~725 ℃為熱分解階段,聚閤物的主鏈破壞併轉變為玻璃態炭結構;在830~855 ℃是芳環髮生脫氫交聯反應引起的放熱階段;860~895 ℃為碳化物逐漸嚮亂層石墨結構轉變,此階段以後熱穩定性高.XRD和拉曼光譜錶明, 1 500 ℃處理後齣現SiC峰,2 200 ℃處理後齣現石墨峰,錶明材料在高溫處理時可髮生部分石墨化.
통과FTIR、DSC、TG화XRD등분석료신형함규방기을결수지적조성、고화반응、탄화과정、탄화궤리급열분해동역학.결과표명,수지주련상함유Si원소,재222℃발생Diels-Alder고화반응;고화수지적기시열분해온도위380 ℃,900 ℃적잔류솔위89.5%.열해동역학분석표명,수지적탄화분위궤개계단,재250~445 ℃계단,위인발계단,결구변화소;450~725 ℃위열분해계단,취합물적주련파배병전변위파리태탄결구;재830~855 ℃시방배발생탈경교련반응인기적방열계단;860~895 ℃위탄화물축점향란층석묵결구전변,차계단이후열은정성고.XRD화랍만광보표명, 1 500 ℃처리후출현SiC봉,2 200 ℃처리후출현석묵봉,표명재료재고온처리시가발생부분석묵화.
Composition, cure reaction, pyrolytic mechanism and thermal decomposition kinetics of PSAA were investigated by u-sing FTIR,DSC,TG and XRD. The results show that main chain of resin contains Si element, and Diels- Alder cure reaction occurs at 222℃; initial thermal decomposition temperature of cured resin is 380℃,and the char yield at 900℃ is 89.5%. Thermal pyroly-sis kinetic analysis shows that the pyrolytic process of resin could be divided into four steps,i. e. less structure change stage at 250 ~445℃,thermal decomposition stage at 450~725℃,during which main-chain of polymer can be destructed and transited into glass carbon structure,exothermic reaction stage at the 830~855℃ due to aromitic ring dehydrogenation,and the stage at 860~ 895℃,during which the carbide can be changed into random layer graphite structure and the thermal stability becomes higher. XRD and Raman spectra shows that the SiC and graphite peak appear after 1 500℃ and 2 200℃ treatment respectively, which indicates that resin had been graphitized partly during high-temperature treatment.