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Development of Sinter-Resistant Core-Shell LaMn_xFe_(1-x)O3@mSiO2 Oxygen Carriers for Chemical Looping Combustion

机译:开发烧结芯壳LAMN_XFE_(1-X)O3 @ MSIO2用于化学环燃烧的氧气载体

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This work investigates the possibility of using LaMn_(.07)Fe_(0.3)O_(3.15)@mSiO2 as oxygen carriers for chemical looping combustion (CLC), CLC is a new combustion technique with inherent separation of CO2 from atmospheric N2. LaMn_(0.7)Fe_(0.3)O_(3.15)@SiO2 core—shell materials were prepared by coating a layer of mesostructured silica around the agglomerated perovsldte particles. The oxygen carriers were characterized using different methods, such as X-ray diffraction (XRD), scanning electron microscopy (SEM), transmission electron microscopy (TEM), N2 sorption, hydrogen temperature-programmed reduction (H2-TPR), and temperature-programmed desorption of oxygen (TPD-O2). The reactivity and stability of the carrier materials were tested in a special reactor, allowing for short contact time between the fluidized carrier and the reactive gas [Chemical Reactor Engineering Centre (CREC) fluidized riser simulator]. Multiple reduction—oxidation cycles were performed. TEM images of the carriers showed that a perfect mesoporous silica layer was formed around samples with 4, 32, and 55 nm in thickness. The oxygen carriers having a core—shell structure showed higher reactivity and stability during 10 repeated redox cycles compared to the LaMn_(0.7)Fe_(0.3)O_(3.15) core. This could be due to a protective role of the silica shell against sintering of the particles during repeated cycles under CLC conditions. The agglomeration of the particles, which occurred at high temperatures during CLC cycles, is more controllable in the core—shell-structured carriers, as confirmed by SEM images. XRD patterns confirmed that the crystal structure of all perovsldtes remained unchanged after multiple redox cycles. Methane conversion and partial conversion to CO2 were observed to increase with the contact time between methane and the carrier. Indeed, more oxygen from the carrier surface, grain boundaries, and even from the bulk lattice was released to react with methane. Upon rising the contact time, less CO was formed, which is desirable for CLC application. Increasing the reaction temperature and methane partial pressure lead to enhanced conversions of CH4 under CLC conditions.
机译:这项工作使用调查的兰姆的可能性_(07)Fe_(0.3)O_(3.15)@ mSiO2作为化学循环燃烧(CLC)的氧载体,CLC是从大气压N2 CO2的固有分离了新的燃烧技术。 LaMn_(0.7)Fe_(0.3)O_(3.15)@的SiO 2芯 - 壳材料通过涂敷周围附聚颗粒perovsldte介孔结构的二氧化硅构成的层制备。使用不同的方法,如X射线衍射(XRD)中的氧载体进行了表征,扫描电子显微镜(SEM),透射电子显微镜(TEM),N2吸附,氢程序升温还原(H2-TPR),和温度氧的程序升温脱附(TPD-O2)。载体材料的反应性和稳定性在一个特殊的反应器进行了测试,允许流化的载体和反应性气体[化学反应器工程中心(CREC)流化床冒口模拟器]之间的短接触时间。进行多个还原 - 氧化循环。载体的TEM图像显示,一个完美的介孔二氧化硅层形成的样品与周围厚度为4,32和55纳米。具有核 - 壳结构的载氧体相比LaMn_(0.7)Fe_(0.3)O_(3.15)芯期间10个重复氧化还原循环显示较高的反应性和稳定性。这可能在CLC的条件下重复循环是由于对所述颗粒的烧结二氧化硅壳的保护作用。颗粒的结块,这发生在在CLC循环高温,是在芯 - 壳结构的载流子更可控的,由SEM图像证实。 XRD图证实,所有perovsldtes的晶体结构保持多个氧化还原循环后保持不变。观察到甲烷的转化率和部分转化为CO 2以增加与甲烷和载体之间的接触时间。实际上,更多的氧气从载体表面,晶界,甚至从体晶格被释放到与甲烷发生反应。一旦上升的接触时间,更少的CO形成,这是理想的应用CLC。提高反应温度和甲烷分压会导致CLC条件下CH4的增强的转换。

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