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作 者:艾尚坤[1] 周定[1] 孙金镖[2] 侯文华[3] 周抗寒[2]
机构地区:[1]哈尔滨工业大学,哈尔滨150001 [2]北京航天医学工程研究所,北京100094 [3]中国环境科学研究院,北京100012
出 处:《航天医学与医学工程》2000年第4期277-280,共4页Space Medicine & Medical Engineering
摘 要:目的研制用于大气再生技术Sabatier二氧化碳还原反应的低温催化剂 ,以降低Sabatier反应的起动温度。方法从催化剂活性组分、载体的选择、催化剂的制备方法和条件等方面进行低温催化剂的设计研制 ,建立催化剂性能测试装置 ,对低温催化剂的性能进行实验研究。结果研制了以钌为催化剂活性组分 ,以活性r Al2 O3为载体的Sabatier反应低温催化剂 ,其反应起动温度可降到 1 1 0℃ ,起动时间 8min ;在温度为 2 0 0~ 30 0℃时 ,贫组分一次通过转化率均高于 95% ;产物水较为纯净 ,无色透明 ,呈中性。结论Sabatier反应低温催化剂的性能达到了设计目的 ,有进一步研究的价值。Objective To develop a low temperature catalyst for the Sabatier CO 2 reduction of the atmospheric regeneration system and lower the start up temperature of the Sabatier reaction. Method A low temperature catalyst was designed from the considerations of the active composition, the choice of the carrier, the production method and condition of the catalyst. Then the performance of the newly developed low temperature catalyst was tested. Result A new low temperature catalyst for the Sabatier reaction using Ru as the active composition and using r Al 2O 3 as the carrier was developed. The start up temperature was lower than 110℃ and the start up time was 8 min; The conversion efficiency of the lean component (H 2 or CO 2) was over 95 percent when the temperature of the reactor was from 200℃ to 300℃; The reaction product water was nearly colorless, transparent and neutral. Conclusion The test results showed that the goals of the design are achieved and it is worthwhile to make further studies on the low temperature catalyst.
关 键 词:SABAtier 催化剂 二氧化碳还原 生命保障系统
分 类 号:R852.82[医药卫生—航空、航天与航海医学]
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