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聚氨酯-丙烯酸酯核-壳乳液的制备及其包覆的RDX 被引量:11

Preparation of Polyurethane-acrylate Core-shell Latex and its Coating of RDX
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摘要 以甲苯二异氰酸酯(TDI)、聚氧化丙烯二醇DL-400(Mn=340)、二羟甲基丙酸(DMPA)、1,4-丁二醇(BDO)为主要原料,制得水性聚氨酯乳液(WPU),用FTIR表征了其结构。以WPU、水、丙烯酸丁酯为原料,分别以AIBN、(NH4)2S2O8-NaHSO3作引发剂,采用种子乳液聚合的方法制备了聚氨酯-丙烯酸酯乳液(PUA),运用TEM表征了PUA乳液的粒子形态。结果表明:以AIBN为引发剂合成了具有核壳结构的PUA乳液,壳层为黑色的聚氨酯胶粒,核层为白色的聚丙烯酸酯胶粒;而(NH4)2S2O8-NaHSO3引发的乳液不具有核-壳结构,黑白粒子相间分布。采用加入10%明矾水溶液使核-壳乳液破乳的方法包覆RDX,并用SEM观察RDX的表面变化,证实包覆后的RDX表面有均匀的包覆层,且颗粒间流散性较好。 Waterborne polyurethane(WPU) was prepared with TDI,DL-400(M_n=340),DMPA and BDO as main materials, whose structure was characterized by FTIR .Polyurethane-acrylate(PUA) latex was synthesized through the method of the seed-latex polymerization with WPU, water and butyl acrylate as starting materials, two kinds of initiator, AIBN and (NH_4)_2S_2O_8-NaHSO_3. Latex particles shape of PUA were determined through TEM, and the results indicated that PUA latex with core-shell structure was synthesized with AIBN as initiator, whose shell were black polyurethane particles and core white polyacrylate ones. PUA latex initiated by (NH_4)_2S_2O_8-NaHSO_3 has no core-shell structure. The method was used for the first time to deposit core-shell latex to coat RDX with 10% KAl (SO_4)_2·12H_2O solution. distilled water,40℃. Through SEM, the surface of RDX was observed to have been covered with a layer of even film after being coated with PUA, and the particles among RDX were perfectly dispersed.
出处 《火炸药学报》 EI CAS CSCD 2004年第3期17-20,共4页 Chinese Journal of Explosives & Propellants
关键词 推进剂 RDX 水性聚氨酯 聚氨酯-丙烯酸酯乳液 包覆 propellant RDX waterborne polyurethane polyurethane-acrylate core-shell structure coating
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参考文献3

  • 1[1]Allen H C.Composite solid propellant with additive to improve the mechanical properties thereof[P].USP 3 745 074.1973.
  • 2[2]Oberth A E,Bruenner R S .Binder filler interaction and propellant mechanical properties[M].Transaction of society of Technology.1965,9:165.
  • 3刘云飞,杨荣杰,谭惠民.包覆奥克托今颗粒的燃烧性能[J].火炸药学报,2000,23(1):20-22. 被引量:5

二级参考文献9

  • 1曹泰岳.关于硝胺复合推进剂燃速特性和燃烧模型的述评[J].推进技术,1989,10(3):54-59. 被引量:5
  • 2NSCohen etal 姚润森译.HMX的燃烧模型与燃烧化学[J].国外固体火箭技术,1987,(3):23-23.
  • 3张仁.复合固体推进剂的稳态燃烧[M].长沙:国际科技大学出版社,1983.
  • 4N S Cohen, C F Price. Combustion of nitramine propellants[J]. J. Spacecraft rocket, 1975,12(10):608.
  • 5Ben-Reuven M. and L H Caveny. Nitramine flame chemistry and deflagratian interpreted in termos a flame model[J]. AIAA.J.,1981,19(10):1276.
  • 6M W. Beckstecd, et al. A model of composite solid propellant combustion based on multiple flames[J]. AIAA. J. , 1970.8(12): 2200.
  • 7N S Cohen. et al, Model and chemistry of HMX combustion[J]. AIAA. J., 1985,23(2):276.
  • 8刘云飞,杨荣杰,谭惠民.固体推进剂中填料的聚合物包覆[J].火炸药,1997,20(4):45-48. 被引量:2
  • 9刘云飞,杨荣杰,谭惠民,黄志刚.聚丙烯酸乙酯包覆奥克托金(HMX)的研究[J].北京理工大学学报,1998,18(3):370-374. 被引量:16

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