酒石酸铅锆的制备、表征及其燃烧催化作用

以酒石酸、硝酸氧锆和硝酸铅为原料,合成出了双金属盐酒石酸铅锆,采用有机元素分析、X射线荧光光谱和FTIR对其进行了表征。在程序升温条件下,利用TG/DTG、DSC、固相原位反应池/FTIR联用技术,研究了酒石酸铅锆的热行为和热分解机理,描述了酒石酸铅锆的热分解过程,分析得出其最终分解产物为ZrO2、PbO和C。利用螺压工艺制备了含酒石酸铅锆的推进剂样品,研究了酒石酸铅锆对双基系推进剂燃烧性能的影响,分析了其燃烧催化作用。结果表明,酒石酸铅锆对双基系推进剂的燃烧具有良好的催化作用,是一种高效的燃烧催化剂;酒石酸铅锆热分解的最终产物PbO是催化燃烧的主要活性物质,推进剂燃烧过程中形成了氧化铅-铅循环催化体系,而锆和碳则起辅助催化的作用。     

柠檬酸铋的热分解机理、 非等温反应动力学及其对双基推进剂燃烧的催化作用

用TG和DSC以及变温固相原位反应池/傅里叶红外光谱(RSFTIR)联用技术研究了柠檬酸铋的热分解行为, 提出了可能的反应机理, 并计算了主分解反应的动力学参数. 柠檬酸铋主分解反应的表观活化能和指前因子分别为213.82 kJ/mol和1016.48 s-1. 将柠檬酸铋应用到双基推进剂配方中研究其对双基推进剂燃烧性能的影响, 结果表明, 柠檬酸铋对双基推进剂燃烧有良好的催化作用, 能显著提高双基推进剂的燃速, 降低压力指数, 特别是与少量炭黑(CB)复合后, 对双基推进剂燃烧的催化效果更好.     

超级铝热剂的制备、表征及其燃烧催化作用

用纳米铝粉和纳米氧化铅、纳米氧化铜和纳米三氧化二铋为原料,采用超声分散复合的方法,制备了纳米超级铝热剂Al/PbO、Al/CuO和Al/Bi₂O₃。采用X射线粉末衍射(XRD)、扫描电镜及能谱分析(SEM-EDS)和红外光谱(IR)对原料和产物的物相、组成、形貌和结构进行分析表征;运用差示扫描量热仪(DSC)评估三种超级铝热剂与双基推进剂主要组分的相容性;研究了3种超级铝热剂对双基推进剂燃烧性能的影响。结果表明,Al/PbO、Al/CuO和Al/Bi₂O₃与推进剂主要组分硝化棉(NC)、硝化棉/硝化甘油(NC/NG)混合物和吉纳(DINA)的相容性均良好,而与黑索今(RDX)和1,3-二甲基-1,3-二苯基脲(C₂)相对较为敏感;含三种纳米超级铝热剂的双基推进剂表现出优异的燃烧性能。     

BTATz-Pb复合物对双基和RDX-改性双基推进剂的热行为、非等温动力学及燃烧性能的影响

制备了含3,6-双(1-氢-1,2,3,4-四唑-5-氨基)-1,2,4,5-四嗪(BTATz)铅复合物(LCBTATZ)的双基推进剂和改性双基推进剂. 采用热重-微商热重法(TG-DTG)及差示扫描量热法(DSC)研究了其热分解行为和非等温分解动力学并在此基础上评价了其热安全性. 结果表明, LCBTATz-DB复合物中在350-540 K之间只存在一个放热分解峰, LCBTATz-CMDB复合物中存在两个连续的放热分解峰在390-540 K温度范围内, 其机理方程分别为: f(α)=α^-1/2和f(α)=2(1-α)^3/2. 计算了热加速分解温度(T_SADT)、热爆炸临界温度(T_b)、热点火温度(T_TIT)和绝热至爆时间(t_Tlad),其值分别为: DB001复合物T_SADT=444.50 K, T_TITT=453.96 K, T_b=471.84 K; t_Tlad=39.36 s; CMDB100复合物, T_SADT=442.38 K, T_TITT=452.89 K,T_b=464.13 K,t_Tlad=21.3 s,并以此来评价化合物的热安全性. 考察了LCBTATz-DB以及LCBTATz-CMDB的燃烧性能, 结果表明LCBTATZ 是一种高效的双基燃烧催化剂, 在较大的压力范围内可以显著的提高燃速并且大幅度的降低压力指数. 对于双基推进剂在2-8 MPa压力范围内出现了明显的超燃速现象, 8-12 MPa出现了“麦撒”效应, 对于改性双基推进剂的压力指数降到0.18.     

纳米Pb(II)-没食子酸配合物的合成及其燃烧催化性能

采用液相分散沉淀法制备了纳米Pb(II)-没食子酸配合物粉体. 用热重分析(TG)、X射线衍射仪(XRD)、透射电镜(TEM)、核磁共振仪(¹H NMR)、红外光谱仪(IR)、激光散射粒径分析仪和元素分析仪对样品的物相、形貌、粒径和组成进行了表征. 研究了没食子酸的浓度和分散剂用量对产物的粒子大小的影响. 并测试了产物对推进剂燃烧的催化作用. 结果表明: 产物的平均粒径约为30 nm. 没食子酸的浓度降低和分散剂用量增加均使产物的粒子减小. 产物能明显改善推进剂的燃烧性能, 使推进剂的燃速提高88%, 压强指数降低了70%.     

溶液燃烧法制备的Ni基催化剂及其浆态床甲烷化催化性能

分别以硝酸铝、硝酸氧锆、硝酸镧和硝酸铈为载体前驱体,与硝酸镍和尿素配制水溶液,采用溶液燃烧法制备了Ni-Al₂O₃、Ni-ZrO₂、Ni-La₂O₃和Ni-CeO₂催化剂,研究了浆态床CO甲烷化催化性能,并进行了低温N₂吸附-脱附、XRD、SEM、TEM、H₂-TPR和H2化学吸附等表征分析.结果表明,以硝酸铝为前驱体制备Ni-Al₂O₃催化剂时燃烧火焰稳定且持续时间长,达23 s,样品比表面积(468 m²·g^-1)和金属Ni表面积(10 m²·g^-1)均较大、Ni粒径小(3~5 nm)且分散度高,CO甲烷化催化活性和稳定性好,CO转化率和CH₄选择性分别达到94%和95%,在100 h的甲烷化反应中未出现明显失活;以硝酸氧锆和硝酸镧为前驱体制备样品时未出现明显的燃烧火焰,持续时间仅为12 s和5 s,催化剂比表面积、金属表面积及催化活性均较低;以硝酸铈为前驱体制备样品时燃烧过程迅速而剧烈,样品比表面积(22 m²·g^-1)和金属Ni表面积(5 m²·g^-1)小、Ni粒径大且分散性差,甲烷化催化性能最差,CO转化率仅为41%,CH₄选择性仅为89%.     

二硫代钨酸铵晶体的合成、表征与热分解机理的研究

本工作用偏钨酸铵和硫化铵为原料，在水溶液中合成二硫代钨酸铵晶体[(NH₄)₂WO₂S₂]。用紫外-可见光谱(UV-Vis)的方法研究了二硫代钨酸铵晶体的形成机理。采用元素分析、X射线衍射(XRD)、傅里叶变换红外光谱(FTIR)、激光拉曼光谱(LRS)等对化合物进行了表征。结果表明采用该方法制备出的二硫代钨酸铵晶体，晶型良好。热重-差热分析(TG-DTA)、原位X射线衍射(in situ XRD)和FTIR等结果表明二硫代钨酸铵晶体在氢气气氛下的热分解主要发生在160～450 ℃之间，分两步进行，首先分解为{WOS₂}，随后转化为二硫化钨。     

过渡金属氧化物对阻燃剂聚磷酸铵热分解的影响机制

过渡金属氧化物(MO)可以显著影响聚磷酸铵(APP)的热分解过程, 进而改善APP复配膨胀阻燃聚合物材料的阻燃效率。将ZnO、Fe₂O₃、TiO₂掺入到APP中, 采用热失重分析(TGA)、X射线光电子能谱(XPS)和X射线衍射分析(XRD), 考察了3种MO对APP热分解行为的影响, 分析了相互作用过程中金属原子和磷原子化学结合状态的变化以及高温热分解产物的物相结构。TGA和XPS图谱分析结果表明, MO可降低APP的起始热分解温度, 并催化APP释放NH₃和H₂O, 而在热分解后期由于金属磷酸盐的形成可显著增加APP的高温残留量。3种MO催化APP热分解脱NH₃和H₂O的活性由大到小的顺序是:ZnO>Fe₂O₃>TiO₂, 而对APP凝聚相热分解P-O产物的交联能力从大到小的顺序为:Fe₂O₃>ZnO>TiO₂。XRD结果显示, ZnO在高温下与APP反应生成了Zn(PO₃)₂晶体, 而Fe₂O₃和TiO₂与APP反应分别生成了Fe₄(P₂O₇)₃和TiP₂O₇晶体。     

仲丁基膦酸-2-丁基辛酯与希土固体配合物的研究

合成了仲丁基膦酸-2-丁基辛酯(HBO/BP)与希土(Ⅲ)(Ln=La, Gd, Ho, Y, Er, Yb)新的固体配合物，其组成为Ln(BO/BP)₃，对配合物的性质进行了表征。热分析表明，在空气中，热分解分两步完成，热分解产物是Ln₂P₄O₁₃。测定了配合物的红外光谱，对其主要吸收谱带进行了归属，配合物中Ln-O键具有较高的离子特性。     

纳米Pb(II)-没食子酸配合物的合成及其燃烧催化性能

采用液相分散沉淀法制备了纳米 Pb(II)-没食子酸配合物粉体. 用热重分析(TG)、X 射线衍射仪(XRD)、透射电镜(TEM)、核磁共振仪(1H NMR)、红外光谱仪(IR)、激光散射粒径分析仪和元素分析仪对样品的物相、形貌、粒径和组成进行了表征. 研究了没食子酸的浓度和分散剂用量对产物的粒子大小的影响. 并测试了产物对推进剂燃烧的催化作用. 结果表明: 产物的平均粒径约为 30 nm. 没食子酸的浓度降低和分散剂用量增加均使产物的粒子减小. 产物能明显改善推进剂的燃烧性能, 使推进剂的燃速提高 88%, 压强指数降低了 70%.     

Preparation,characterization and compatibility studies of poly(DFAMO/AMMO)

Poly(3-difluoroaminomethyl-3-methyl oxetane (DFAMO)/3-azidomethyl-3-methyl oxetane (AMMO)) (PDA) can be used as an energetic pre-polymer in the binder systems of solid propellants and polymer-bonded explosives (PBXs). The cationic solution polymerization affords PDA using butane diol (BDO) and boron trifluride etherate (TFBE) as initiator and catalyst, separately. Its molecular structure is characterized and thermal decomposition behavior is investigated by thermogravimetric analysis (TG), differential scanning calorimetry (DSC) and Fourier transform infrared spectroscopy (FTIR). The copolymer has good thermal stability and exhibits a three-step mass-loss process with the first two steps mainly belonging to the thermal decomposition of difluoroamino and azido groups, respectively. DSC method is performed to evaluate the compatibility of PDA with some energetic components and inert materials. More than half of the selected materials are compatible with PDA, which including cyclotrimethylenetrinitramine (RDX), 2,4,6-trinitrotoluene (TNT), 1,3,5-triamino-2,4,6-trinitrobenzene (TATB), pentaerythritol tetranitrate (PETN), ammonium perchlorate (AP), ammonium nitrate (AN), potassium nitrate (KNO₃), aluminum powder (Al), aluminum oxide (Al₂O₃), 2-nitrodiphenylamine (NDPA) and 1,3-diethyl-1,3-diphenyl urea (C₁).     

The influence of porosity of ammonium perchlorate (AP) on the thermomechanical and thermal properties of the AP/polyvinylchloride (PVC) composite propellants

The influence of porous ammonium perchlorate (P_OAP) on the thermomechanical and combustion behavior of solid rocket propellants based on polyvinylchloride binder has been investigated. Differential scanning calorimetry, differential thermogravimetry, dynamic mechanical thermal analysis, and scanning electronic microscopy measurements were used for thermomechanical and thermal decomposition properties assessment. The results obtained indicate that lower glass transitions of the propellants and catalytic effect of combustion are obtained with P_OAP.     

Physicochemical properties of ceramic tape involving Ca<Subscript>0.05</Subscript> Ba<Subscript>0.95</Subscript> Ce<Subscript>0.9</Subscript>Y<Subscript>0.1</Subscript>O<Subscript>3</Subscript> as an electrolyte designed for electrolyte-supported solid oxide fuel cells (IT-SOFCs)

Energetic materials such as a mixture of guanidine nitrate (GN)/basic copper nitrate (BCN) are used as gas generators in automotive airbag systems. However, at the time of the airbag inflation, the gas generators release toxic combustion gases such as CO, NH₃, and NO_x. In this study, we investigated the combustion and thermal decomposition behaviors of GN/BCN mixture, focusing primarily on their exhaust gas composition. As a result, when the exhaust gas of the combustion under constant pressure in an inert gas stream was analyzed using a detection tube, the amount of NO_x (mainly NO) yielded greater decrease with increasing atmospheric pressure as compared to the amounts of CO and NH₃. Thus, provided GN/BCN is ignited in a closed container, a large amount of NO_x is presumed to have been released during the initial stage of combustion, which yielded comparatively low pressure. Results of the thermogravimetry–differential scanning calorimetry–Fourier transform infrared spectroscopy (TG/DSC/FTIR) indicated that the GN/BCN mixture caused endothermic decomposition at 170 °C and exothermic decomposition at 208 °C, which was accompanied by 66% mass loss. The decomposition gases, CO₂, N₂O, and H₂O, were detected via FTIR spectrum. Because N₂O was not detected in the combustion gas, it was suggested that the detected N₂O was generated at a low temperature and decomposed in high-temperature combustion.     

Reactivity analysis of ammonium dinitramide binary mixtures based on ab initio calculations and thermal analysis

Ammonium dinitramide (ADN) is a promising high energy oxidizer for rocket propellants because it offers a good oxygen balance and has a significant energy content. As a result, ADN-based energetic ionic liquid propellants (EILPs) have been studied, based on ADN combined with urea and monomethyl ammonium nitrate (MMAN). The thermal decomposition of ADN in the condensed phase affects the combustion of both pure ADN and ADN-based EILPs; thus, it is important to understand the reactions of EILPs in the condensed phase. The present study assessed the reactivity of ADN mixtures in the condensed phase, focussing on hydrogen abstraction reactions with NO₂· formed from the thermal decomposition of ADN. The potential energy surfaces of these reactions were obtained using ab initio calculations. The effects of functional groups and of carbon chain length on hydrogen abstraction by NO₂· were examined. Mixtures of ADN with urea and acetamide (AA) as amide compounds, and with MMAN and monoethanol amine nitrate (MEAN) as nitrate salts, were examined. Thermal analysis was conducted to investigate the properties of these mixtures, using differential scanning calorimetry (DSC). The calculation results shows that AA and MEAN are more reactive with ADN than urea and MMAN, which is supported by the DSC data. Hydrogen abstraction by NO₂· is evidently an important condensed phase reaction in ADN mixtures, and substances having alkyl groups and longer carbon chains are more highly reactive.

     

负载于HZSM-5上的CuO-ZnO-Al2O3纳米粒子：尿素－硝酸盐燃烧合成和理化表征

用尿素-硝酸盐燃烧法制备了一系列的负载于HZSM-5上的CuO-ZnO-Al2O3纳米复合材料(CZA/HZSM-5)。研究了燃料与氧化物的比率对所合成的复合材料的理化性质的影响。用TGA/DTG,FTIR和XRD等研究了尿素-硝酸盐凝胶的热分解和煅烧粉体的相演变过程。FESEM结果表明在燃烧过程中燃料的用量对CZA/HZSM-5的性质有重大影响。CuO和ZnO的晶粒首先随尿素量的增加而增大,然后随尿素量的增加而减小。CuO和ZnO的相对结晶度随燃料量的增加表现为非单调趋势。随着燃料与硝酸盐的比率的增加,CZA/HZSM-5不仅形貌变得超细和均一,而且表面孔隙率也显著增加。FTIR结果表明HZSM-5的结构甚至在负载了CuO-ZnO-Al2O3纳米粒子后也未被破坏,而且在CuO和ZnO与HZSM-5之间还有表面的键合。TGA/DTG结果指出燃烧合成法是一种由若干过程组合起来的方法,例如前驱体的热分解和前驱体间的放热反应等。另外,提出了CuO-ZnO-Al2O3负载在HZSM-5上的生成机理。     

Thermal degradation and evolved gas analysis of N,N′-bis(2 hydroxyethyl) linseed amide (BHLA) during pyrolysis and combustion

The thermal degradation of N,N′-bis(2 hydroxyethyl) linseed amide (BHLA) was investigated by thermogravimetric analysis coupled with Fourier transform infrared spectroscopy and mass spectroscopy (TG–FTIR–MS). Thermogravimetric analysis revealed that the thermal degradation process can be subdivided into three stages: sample drying (<200 °C), main decomposition (200–500 °C), and further cracking (>500 °C) of the polymer. The compound reached almost 800 °C during pyrolysis and combustion. The activation energy at the second step during combustion was slightly higher than that of pyrolysis emissions of carbon dioxide, aliphatic hydrocarbons, carbon monoxide, and hydrogen cyanide, and other gases during combustion and pyrolysis were detected by FTIR and MS spectra. It was observed that the intensities of CO₂, CO, HCN, and H₂O were very high when compared with their intensities during pyrolysis, and this was attributed to the oxidation of the decomposition product.     

Thermal decomposition properties of double-base propellant and ammonium perchlorate

The thermal decomposition properties and the heat of combustion (ΔH) of samples with different ammonium perchlorate (AP)/double base propellant (DB) mass ratios under argon atmosphere were studied by the thermogravimetry–differential scanning calorimetry–mass spectrometry–Fourier transform infrared spectroscopy (TG–DSC–MS–FTIR) and automatic calorimeter method. The results show that decomposition process of AP/DB samples in negative and zero oxygen balance (OB) is different from that in positive OB. With the increasing of AP in the AP/DB samples, the decomposition of the samples becomes more and more severe. When the OB of the samples is positive, the phenomenon of deflagration or explosion could be observed in the decomposition process. The sample with OB = 0 has the greatest heat of combustion.