共查询到19条相似文献,搜索用时 156 毫秒
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为了提高光学加工效率,缩短大口径光学元件制造周期,本文提出了一种具有公自转运动模式的新型高效抛光方式,对其结构、工作原理以及去除特性进行了研究。首先,介绍了公自转抛光装置机械结构及工作原理。接着,根据Hertz接触理论和Preston方程进行了去除函数建模,讨论了不同转速比情况下的去除函数形状。然后,根据理论模型进行了去除函数实验、工艺参数实验以及稳定性实验,研究了压入深度、转速等工艺参数对去除结果的影响。最后,进行了200 mm口径SiC工件的仿真加工。实验结果表明:在2 mm压入深度、200 rpm转速情况下,去除区域直径为19.23 mm,体去除率达到0.197 mm~3/min,去除效率高于同等去除区域大小的传统小磨头加工方式;仿真加工结果表明:SiC仿真镜经过3.7 h加工,面形从3.008λPV,0.553λRMS提高到0.065λPV,0.005λRMS,收敛效率为达到98.18%。 相似文献
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光学镜面离子束加工去除函数工艺可控性分析 总被引:1,自引:0,他引:1
实验分析了离子束加工去除函数的工艺可控性问题并进行了初步修形实验。从工艺实现的角度分析光学镜面离子束加工技术对去除函数的要求,以去除函数环半峰全宽、体积去除率和峰值去除率为评价指标研究去除函数的长时稳定性、线性性、小扰动鲁棒性以及大参数调节变化等特征,以此分析结果为依据,对Φ100mm K4平面样件进行了修形,经过三次迭代面形RMS误差从0.149λ收敛到0.013λ。实验结果表明:离子束加工中的去除函数具有较长时稳定性,去除量对时间具有线性关系,对工艺参数小扰动的鲁棒性,可以通过调节离子源电源参数优化选取去除函数的宽度和幅值;利用离子束可以对镜面进行高效地修形。 相似文献
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在离子束抛光工艺过程中,材料确定性去除特性对预测光学元件的各工位材料去除量和驻留时间具有极其重要的作用。采用射频离子源对熔石英光学元件的离子束刻蚀特性进行了研究,利用ZYGO激光干涉仪获得准确的去除函数,系统分析了气体流量、屏栅电压、离子束入射角和工作距离等因素对熔石英去除函数的影响,并分析了各单一工艺因素微小扰动时,材料峰值去除率、半高宽和体积去除率的相对变化率。实验结果表明,相同工作真空条件下,工作气体质量流量的微小变化对去除函数影响极小,在典型的工艺条件下,屏栅电压在±5 V、离子束入射角±1°、工作距离在±0.5 mm范围内变化时,熔石英峰值去除率、体积去除率和峰值半高宽的相对变化均小于5%,去除函数具有较好的确定性和稳定性。 相似文献
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随着水资源的日益缺乏,如何获取更多的淡水资源越来越得到重视,尤其体现在一些严重干旱地区。为解决干旱地区淡水资源短缺的问题,研究并探索了一种利用沙漠中土壤与大气环境温差来实现空气取水装置。空气中含有大量的水蒸气可以利用,本文为此设计了一种新型空气取水系统,利用温度较为恒定的土壤作为冷源,整个系统使用极低的能耗,通过降温的方式达到空气取水的效果。搭建试验台进行了相关实验,发现系统的取水能力主要受空气温度的影响,通过模型实验与计算的方法确定了空气取水过程中送风速度与冷凝水量的关系式,得出最优风量为11.37 m/s,此时取水系统的取水效率最高。 相似文献
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Changes in the chemical composition of lichens exposed to pollutants are investigated by means of FTIR spectroscopy. According
to model experiments, alkyl nitrates, ammonium salts, amines, and sulfones develop in the lichen thallus through the action
of ammonia and nitric and sulfuric acids. Spectroscopic data of modeling experiments enabled nitrogen- and sulfur-containing
substances to be identified as the main air pollutants in the vicinity of a pig-breeding complex and information to be obtained
on the content of the pollutants and their impact on the lichens. 相似文献
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光催化反应器性能参数及其简便测试方法 总被引:7,自引:0,他引:7
本文分析了光催化反应器降解有机挥发化合物(VOCs)的特性,提出了反应器总降解常数的概念,提出了一种测量光催化反应器性能参数-传质单元数、反应有效度和总降解常数的方法。管状光催化反应器降解空气中微量甲醛的实验验证了该方法的可行性。实验表明:在空气温度22-24℃,空气湿度40%附近,甲醛的光催化反应在不同浓度区间近似为一次反应,在1.6-12.4 mg/m3浓度区间内其总降解常数最大。 相似文献
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甲醛(HCHO)是目前室内空气主要污染物之一,长期暴露在过量甲醛环境中会对人的眼睛、皮肤、呼吸器官等产生严重危害,甚至可能导致神经系统功能的丧失[1]以及耳、鼻和喉癌[2]。因此,快速、高效、准确地实现甲醛气体的检测,对于保障人类健康具有重大的意义。当前有很多种方法可以用于甲醛气体的检测。例如,气相色谱法(GC)[3]和高效液相色谱法(HPLC)[4],色谱仪器能够提供低至μg·m-3级别的浓度检测,但是仪器较为大型笨重,并且检测非常耗时,难以实现实时连续地对甲醛气体浓度的监测;基于气敏薄膜的半导体气体传感器具备响应时间短,稳定性高以及可连续监测等优点,然而这类传感器通常检测限较高(>300 μg·m-3),并且选择性差[5];基于酶的生物传感器通常有较好的灵敏性和选择性,但是其热稳定性通常较差,这严重限制了其应用[6]。比色法和荧光法由于响应速度快,灵敏度高,检测限低,选择性好以及传感器简单便宜等特点,被广泛地应用于甲醛气体传感器的设计中去[7-9]。这种方法是利用探针分子与甲醛发生特异性结合,形成新的物质,从而引起探针吸收光谱的变化或者发出荧光,实现对甲醛的定量测量。Descamps等使用4-氨基-3-戊烯-2-酮(Fluoral-P)作为探针分子,设计了一种手提式的甲醛检测仪[10]。Fluoral-P是一种烯氨酮结构的物质,能与甲醛特异性结合形成环状化合物3,5-diacetyl-1,4-dihydrolutidine(DDL)。由于Fluoral-P自身的特征吸收带与DDL的吸收带相隔较远,同时与甲醛结合后能够产生大斯托克斯位移的荧光峰,因而被广泛应用于甲醛检测。然而,Fluoral-P在空气中有水分子存在的情况下极其不稳定,容易发生水解,形成乙酰丙酮和氨气,严重限制了Fluoral-P在甲醛检测上的应用[10]。采用紫外可见吸收光谱、稳态荧光光谱和气相色谱质谱(GC-MS)技术研究了Fluoral-P的一种衍生物,4-氨基-1,1,1-三氟-3-丁烯-2-酮(3F-FP),与甲醛溶液相互作用的光学和化学特性。实验发现,Fluoral-P的水解速率为k=1.555 9×10-5 L2·mol-2·s-1,然而,3F-FP具有非常低(接近0)的水解速率,水溶液环境下表现出了极好的稳定性。同时,3F-FP可以与甲醛反应生成一种类似DDL的环状化合物6F-DDL,使得3F-FP在430 nm处出现了一个新的吸收带,并且在峰值489 nm处的荧光强度也得到了明显增强,增强因子为12,在峰值处的荧光增长速率为k=7.881×103 h-1。下一步我们将使用多孔玻璃作为3F-FP探针的载体,不仅可以提高3F-FP分子浓度,也可以增加探针分子与甲醛的接触表面积[11],荧光增长速率还可以得到进一步的提高,因此3F-FP分子在甲醛气体检测领域具备了良好的应用前景。 相似文献
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Akihiro Hayakawa Yuta Hirano Ekenechukwu C. Okafor Hirofumi Yamashita Taku Kudo Hideaki Kobayashi 《Proceedings of the Combustion Institute》2021,38(2):2409-2417
Ammonia has widely attracted interest as a potential candidate not only as a hydrogen energy carrier but also as a carbon free fuel for internal combustion engines, such as gas turbines. Because ammonia contains a nitrogen atom in its molecule, nitrogen oxides (NOx) and other pollutants may be formed when it burns. Therefore, understanding the fundamental product gas characteristics of ammonia/air laminar flames is important for the design of ammonia-fueled combustors to meet stringent emission regulations. In this study, the product gas characteristics of ammonia/air premixed laminar flames for various equivalence ratios were experimentally and numerically investigated up to elevated pressure conditions. In the experiments, a stagnation flame configuration was employed because an ammonia flame can be stabilized by using such a configuration without a pilot flame. The experimental results showed that the maximum NO mole fraction was about 3,500 ppmv, at an equivalence ratio of 0.9 at 0.1 MPa. The NO mole fraction decreased as the equivalence ratio increased. In addition, the maximum value of the NO mole fraction decreased with an increase in mixture pressure. Furthermore, it was experimentally clarified that the simultaneous reduction of NO and unburnt ammonia can be achieved at an equivalence ratio of about 1.06, which is the target equivalence ratio for emission control in rich-lean two-stage ammonia combustors. Comparison of experimental and numerical results showed that even though the reaction mechanisms employed have been optimized for predicting the laminar burning velocity of ammonia/air flames, they failed to satisfactorily predict the measured species in this study. Sensitivity analysis was used to identify elementary reactions that control the species profiles but have negligible effects on the burning velocity. It is considered that these reaction models need to be updated for accurate prediction of product gas characteristics of ammonia/air flames. 相似文献
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Charles Lhuillier Pierre Brequigny Francesco Contino Christine Mounaïm-Rousselle 《Proceedings of the Combustion Institute》2021,38(4):5859-5868
Ammonia combustion appears as a meaningful way to retrieve stored amounts of excess variable renewable energy, and the spark-ignition (SI) engine has been proposed as a practical conversion system. The present work aims at elucidating the combustion characteristics of ammonia blends in engine-relevant turbulent conditions. To that end, laminar and turbulent flame experiments were conducted in a constant-volume vessel at engine-relevant conditions of 445 K and 0.54 MPa to assess the combustion behavior of ammonia/hydrogen/air, ammonia/methane/air and methane/hydrogen/air mixtures observed in an all-metal single-cylinder SI engine. Results show that the respective accelerating or decelerating effects of hydrogen or methane enrichment observed in the SI engine could not be sufficiently explained by the measured laminar burning velocities of the mixtures. Since the latter are very low, the studied combustion regimes are at the boundary between the thin and broken reaction zones regimes, and thus strongly influenced by flame-turbulence interactions. The quantification of the flame response to turbulence shows much higher effects for ammonia blends, than for methane-based fuels. The aforementioned opposite effects of ammonia enrichment with hydrogen or methane are observed on the turbulent burning velocity during the turbulent flame experiments and correlated to the thermochemical properties of the reactants and the flame sensitivity to stretch. The latter may explain an unexpected bending effect on the turbulent-to-laminar velocity ratio when increasing the hydrogen fraction in the ammonia/hydrogen blend. Nevertheless, a very good correlation of the turbulent velocity was found with the Karlovitz and Damköhler numbers, that suggests that ammonia combustion in SI engines may be described following the usual turbulent combustion models. This encourages further investigations on ammonia combustion for the optimization of practical systems, by means of dedicated experiments and numerical simulations. 相似文献
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《Proceedings of the Combustion Institute》2023,39(3):3519-3528
Ammonia is a highly promising energy carrier for achieving a carbon-neutral society. The co-combustion of solid particle clouds–ammonia, in particular, is considered an efficient and feasible method of reducing carbon dioxide emissions. Understanding turbulent flame stabilization and extinguishment processes during the two-phase hybrid-mixture co-combustion of solid particle clouds–ammonia is essential for the co-combustion technology to be used in combustors. To the best of our knowledge, this is the first study to describe the turbulent flame propagation limits and associated mechanism on the co-combustion of solid particle clouds–ammonia–air. Turbulent flame propagation experiments on silica particle clouds–ammonia–air mixing combustion and polymethylmethacrylate (PMMA) particle cloud–ammonia–air co-combustion were conducted in this work using a novel fan-stirred constant-volume vessel to clarify the turbulent flame propagation limits and associate mechanism of solid particle cloud–ammonia–air co-combustion. Results showed that adding inert silica particles contracted the turbulent flame propagation limits of premixed ammonia–air mixtures. However, adding PMMA particles expanded and then contracted the turbulent flame propagation limits of a premixed ammonia–air mixture as the ammonia equivalence ratio increased from lean to rich. In the solid particle cloud–ammonia–air co-combustion, reactive particles induce two types of effects on the turbulent flame propagation limits of premixed ammonia–air mixtures: The local equivalence ratio increment effect is caused by adding volatile matter from preheated particles in the preheat zone of the flame front, and the heat sink negative effect is induced by the unburned particles. 相似文献
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The possibility of creating an integrated-optical chemical sensor that makes it possible to control the content of ammonia and other pollutants in air is demonstrated. A sensor of this type is experimentally studied. The limiting sensitivity of the integrated-optical ammonium sensor is estimated. The possibility of applying integrated-optical sensors in ecological monitoring is discussed. 相似文献