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Impact of Heat Shield Structure in the Growth Process of Czochralski Silicon Derived from Numerical Simulation 被引量:8
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作者 ZHANG Jing LIU Ding +1 位作者 ZHAO Yue JIAO Shangbin 《Chinese Journal of Mechanical Engineering》 SCIE EI CAS CSCD 2014年第3期504-510,共7页
Further development of the photovoltaic industry is restricted by the productivity of mono-crystalline silicon technology due to its requirements of low cost and high efficient photocells. The heat shield is not only ... Further development of the photovoltaic industry is restricted by the productivity of mono-crystalline silicon technology due to its requirements of low cost and high efficient photocells. The heat shield is not only the important part of the thermal field in Czochralski(Cz) mono-crystalline silicon furnace, but also one of the most important factors influencing the silicon crystal growth. Large-diameter Cz-Si crystal growth process is taken as the study object, Based on FEM numerical simulation, different heat shield structures are analyzed to investigate the heater power, the melt-crystal interface shape, the argon flow field, and the oxygen concentration at the melt-crystal interface in the process of large Cz-Si crystal growth. The impact of these factors on the growth efficiency and crystal quality are analyzed. The results show that the oxygen concentration on the melt-crystal interface and the power consumption of the heater stay high due to the lack of a heat shield in the crystal growth system. Argon circumfluence is generated on the external side of the right angle heat shield. By the right-angle heat shield, the speed of gas flow is lowered on the melt free surface, and the temperature gradient of the free surface is increased around the melt-crystal interface. It is not conducive for the stable growth of crystal. The shape of the melt-crystal interface and the argon circulation above the melt free surface are improved by the inclined heat shield. Compared with the others, the system pulling rate is increased and the lowest oxygen concentration is achieved at the melt-crystal interface with the composite heat shield. By the adoption of the optimized composite heat shield in experiment, the real melt-crystal interface shapes and its deformation laws obtained by Quick Pull Separation Method at different pulling rates agree with the simulation results. The results show that the method of simulation is feasible. The proposed research provides the theoretical foundation for the thermal field design of the large diameter Cz-Si monocrystalline growth. 展开更多
关键词 Czochralski mono-crystalline silicon heat shield thermal field numerical simulation
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Hydrothermal Synthesis of Cs_xWO_3 and the Effects of N_2 Annealing on its Microstructure and Heat Shielding Properties 被引量:6
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作者 Fei Shi Jingxiao Liu +3 位作者 Xiaoli Dong Qiang Xu Jiayu Luo Hongchao Ma 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2014年第4期342-346,共5页
Cesium tungsten bronze (CsxW03) powders were synthesized by hydrothermal reaction at 190 ℃ by using sodium tungstate and cesium carbonate as raw materials, and the effects of N2 annealing on the microstructure and ... Cesium tungsten bronze (CsxW03) powders were synthesized by hydrothermal reaction at 190 ℃ by using sodium tungstate and cesium carbonate as raw materials, and the effects of N2 annealing on the microstructure and near-infrared (NIR) shielding as well as heat insulation properties of CsxW03 were investigated. The results indicated that the synthesized CsxW03 powders exhibited hexagohal CSo.32WO3 crystal structure, and subsequent N2 annealing could further improve the crystallinity of CsxW03 particles. Moreover, the NIR shielding and heat insulation properties of CsxW03 could be further improved after N2 annealing at appropriate temperature for a period of time. Particularly, the 500 ℃-annealed CsxW03 products in the N2 atmosphere showed the best NIR shielding and heat insulation properties. When the N2 annealing temperature was higher than 700 ℃, the NIR shielding properties decreased again. The 800 ℃-annealed samples in the N2 atmosphere showed higher visible light transmittance, however, the NIR shielding properties were lower than that of the non-annealed samples. 展开更多
关键词 Hydrothermal synthesis Oxide nanoparticles ANNEALING Optical properties heat shielding
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Heat Shielding Effects in the Earth's Crust 被引量:2
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作者 Yixian Xu Lupei Zhu +2 位作者 Qinyan Wang Yinhe Luo Jianghai Xia 《Journal of Earth Science》 SCIE CAS CSCD 2017年第1期161-167,共7页
Knowledge of heat flow and associated variations of temperature with depth is crucial for understanding how the Earth functions. Here, we demonstrate possible heat shielding effects that result from the occurrence of ... Knowledge of heat flow and associated variations of temperature with depth is crucial for understanding how the Earth functions. Here, we demonstrate possible heat shielding effects that result from the occurrence of mafic intrusions/layers(granulitic rocks) within a dominantly granitic middle crust and/or ultramafic intrusions/layers(peridotitic rocks) within a dominantly granulitic lower crust; heat shielding is a familiar phenomenon in heat engineering and thermal metamaterials. Simple one-dimensional calculations suggest that heat shielding due to the intercalation of granitic, granulitic and peridotitic rocks will increase Moho temperatures substantially. This study may lead to a rethinking of numerous proposed lower crustal processes. 展开更多
关键词 GEOTHERM crustal laminated structure heat shielding heat conductivity peridotitic in-trusions North Tibet magnetotelluric data.
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Effect of Spacecraft Aerodynamics and Heat Shield Characteristics on Optimal Aeroassisted Transfer
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作者 Antonio Mazzaracchio Mario Marchetti 《Engineering(科研)》 2012年第6期307-320,共14页
A spacecraft designed to operate in a planetary atmosphere must have an adequate heat shield to withstand the high heat fluxes and heat loads that are generated by aerodynamic heating. Very often, the mass of the ther... A spacecraft designed to operate in a planetary atmosphere must have an adequate heat shield to withstand the high heat fluxes and heat loads that are generated by aerodynamic heating. Very often, the mass of the thermal protection system is a significant fraction of the total mass of the vehicle. In contrast, performing maneuvers in the atmosphere, that would be very costly in terms of propellant consumption if they were performed completely outside of the atmosphere in a classic way, is a very attractive prospective technique. The advantages and disadvantages in terms of total mass spared must be determined. The mission investigated involves an aeroassisted coplanar transfer from a high to a low Earth orbit. The approach uses a combination of three propulsive impulses in space together with an aerodynamic maneuver in the atmosphere. The heat shield adopted is fully ablative, given the expected high values of the entering heat flux. The convenience of the aeroassisted maneuver and the influence of the parameters involved are evaluated in comparison to a conventional Hohmann transfer. In particular, a parametric analysis is performed by varying the following characteristics of the vehicle: aerodynamic efficiency, mass-to-surface ratio, deorbit impulse, and initial altitude of the orbit. The influence of the thermal protection system is examined by assessing the impact of the type of ablative material employed, the thermal safety factor, and the allowable temperature for the adhesive layer on the substructure. The analysis is conducted with a highly representative thermal model by coupling the dynamic and thermal analyses and using a genetic optimizer. The optimization methodology and the thermal model are completely original. The results indicate the importance of choosing low-density ablative materials, of adopting a suitable thermal safety factor, and of choosing high-performance adhesives. The optimal trajectories obtained correspond to a zero second propulsive impulse. 展开更多
关键词 Aeroassisted MANEUVER heat shield Optimization ORBITAL TRANSFER Thermal Protection System
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Evidence of vapor shielding effect on heat flux loaded on flowing liquid lithium limiter in EAST 被引量:1
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作者 Chenglong LI Guizhong ZUO +13 位作者 R MANIGI K TRITZ D ANDRUCZYK Bin ZHANG Ruirong LIANG D OLIVER Zhen SUN Wei XU Xiancai MENG Ming HUANG Zhongliang TANG Binfu GAO Ning YAN Jiansheng HU 《Plasma Science and Technology》 SCIE EI CAS CSCD 2022年第9期45-51,共7页
A lithium(Li)vapour layer was formed around a flowing liquid Li limiter to shield against the plasma incident power and reduce limiter heat flux in the EAST tokamak.The results revealed that after a plasma operation o... A lithium(Li)vapour layer was formed around a flowing liquid Li limiter to shield against the plasma incident power and reduce limiter heat flux in the EAST tokamak.The results revealed that after a plasma operation of a few seconds,the layer became clear,which indicated a strong Li emission with a decrease in the limiter surface temperature.This emission resulted in a dense vapour around the limiter,and Li ions moved along the magnetic fleld to form a green shielding layer on the limiter.The plasma heat flux loaded on the limiter,measured by the probe installed on the limiter,was approximately 52%lower than that detected by a fast-reciprocating probe at the same radial position without the limiter in EAST.Additionally,approximately 42%of the parallel heat flux was dissipated directly with the enhanced Li radiation in the discharge with the liquid metal infused trenches(LIMIT)limiter.This observation revealed that the Li vapour layer exhibited an excellent shielding effect to liquid Li on plasma heat flux,which is a possible beneflt of liquid-plasma-facing components in future fusion devices. 展开更多
关键词 liquid Li limiter Li vapor shielding heat flux EAST
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Effect of heat treatment temperature on microstructure and electromagnetic shielding properties of graphene/SiBCN composites 被引量:2
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作者 Wei Yue Yongsheng Liu +2 位作者 Mingxi Zhao Fang Ye Laifei Cheng 《Journal of Materials Science & Technology》 SCIE EI CAS CSCD 2019年第12期2897-2905,共9页
Three-dimensional(3D) graphene/SiBCN composites(GF/SiBCN) were prepared by depositing SiBCN ceramics in 3D graphene foam via the chemical vapor infiltration technique. The effect of the heat treatment temperature on t... Three-dimensional(3D) graphene/SiBCN composites(GF/SiBCN) were prepared by depositing SiBCN ceramics in 3D graphene foam via the chemical vapor infiltration technique. The effect of the heat treatment temperature on the microstructure, phase composition, and electromagnetic properties of the GF/SiBCN composite was investigated. The SiBCN ceramics maintained an amorphous structure in the composite below 1400℃ above which the crystallinity of the free carbon phase gradually increased.While the Si3N4 and B4C phases started to crystallize at 1500℃ and their crystallinity increased with temperature, SiC was observed at 1700℃. The electromagnetic shielding effectiveness of GF/SiBCN increased with the heat treatment temperature. 展开更多
关键词 Silicon-Boron carbonitride ceramics Chemical vapor deposition and infiltration heat treatment Electromagnetic shielding effectiveness
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The Application of Radiation Shields for Thermal Control of Superheater Tubes in Boiler
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作者 Shahram Falahatkar Tayeb Pour-Reza Habib Karimi 《Energy and Power Engineering》 2012年第2期77-84,共8页
Superheater tubes temperature control is a necessity for long lifetime, high efficiency and high load following capability in boiler. This study reports a new approach for the control strategy design of boilers with s... Superheater tubes temperature control is a necessity for long lifetime, high efficiency and high load following capability in boiler. This study reports a new approach for the control strategy design of boilers with special shields. The presented control strategy is developed based on radiation thermal shields with low emissivity coefficient and high reflectivity or scattering coefficient. In order to simulate the combustion event in boiler and heat transfer to superheater tubes, an effective set of computational fluid dynamic (CFD) codes is used. Results indicate a successful identification of over- heated zones on platen superheater tubes and effect of radiation shields for solving this problem. 展开更多
关键词 Platen SUPERheatER heat TRANSFER COMBUSTION RADIATION Thermal shieldS BOILER CFD
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Study on release rate of latent heat in Czochralski silicon growth 被引量:1
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作者 REN Bingyan YANG Jiankun LI Yanlin LIU Xiaoping WANG Minhua 《Rare Metals》 SCIE EI CAS CSCD 2006年第z2期51-54,共4页
The pulling rate in czochralski silicon (CZSi) growth is important for reducing the cost of solar cell. In this paper, double-heater, heat shield and composite argon duct system were introduced in the Ф450 mm hot zon... The pulling rate in czochralski silicon (CZSi) growth is important for reducing the cost of solar cell. In this paper, double-heater, heat shield and composite argon duct system were introduced in the Ф450 mm hot zone of a Czochralski furnace. The pulling rate under different thermal system was recorded in experiments. Argon flow and temperature fields were simulated by finite element method(FEM). Experimental results and numerical simulation indicate that double-heater and composite argon duct system can enhance obviously the release rate of latent heat. In Φ 200 mm Czochralski silicon (CZSi) growth, average pulling rate can increase from 0.6 mm·min-1 in the conventional hot zone to 0.8 mm·min-1 in the modified hot zone. 展开更多
关键词 CZSI latent heat double-heater heat shield numerical simulation
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等离子弧焊接热处理对1J85坡莫合金焊接接头微观组织及磁性能的影响
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作者 孙建 谷文举 +3 位作者 张丽炜 姚秀聪 耿燕飞 陈希章 《材料工程》 北大核心 2026年第1期178-186,共9页
针对1J85坡莫合金焊接过程中磁性能恶化的问题,采用等离子弧直焊(plasma arc welding,PAW)和等离子弧焊接热处理(plasma arc heat treatment welding,PAHTW)两种工艺对1.5 mm厚环形1J85坡莫合金开展对比实验,系统探究两种工艺对焊接接... 针对1J85坡莫合金焊接过程中磁性能恶化的问题,采用等离子弧直焊(plasma arc welding,PAW)和等离子弧焊接热处理(plasma arc heat treatment welding,PAHTW)两种工艺对1.5 mm厚环形1J85坡莫合金开展对比实验,系统探究两种工艺对焊接接头微观组织和磁性能的影响。采用光学显微镜、扫描电镜、能谱分析及软磁性能测试等手段对比分析接头的微观组织、元素分布、磁导率及矫顽力。结果表明:PAW工艺下,焊缝接头的形貌呈上宽下窄的漏斗状结构;PAHTW工艺下,焊缝区形成多层次区域分界,晶粒显著长大,胞状亚晶数量减少,晶界密度降低。能谱分析显示,焊缝区非磁性元素Si的含量较PAW工艺减少约50%。与PAW工艺相比,PAHTW处理后接头的初始磁导率从40.12 mH/m提升至78.81 mH/m,最大磁导率从72.63 mH/m提升至113.41 mH/m,矫顽力从1.70 A/m降低至1.24 A/m。 展开更多
关键词 磁屏蔽 1J85坡莫合金 焊接接头 等离子弧焊接热处理 微观组织 磁性能
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High-efficiency Gas Shielded Multi-arc Welding Technology 被引量:1
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作者 TANG Yingying ZHU Zhiming +1 位作者 YANG Zhongyu YU Yingfei 《电焊机》 2016年第11期9-20,共12页
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感应加热炉磁场和温度场的数值模拟及磁屏蔽环的参数优化
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作者 姬军鹏 张宁 +2 位作者 路景杰 张志刚 常宏 《铸造》 2025年第4期529-536,共8页
针对感应加热炉磁屏蔽环异常发热问题,以30 t坩埚型感应加热炉为对象,采用COMSOL有限元分析软件计算并通过试验验证了带磁屏蔽环感应加热炉的磁感应强度和磁屏蔽环的温度场分布规律。结果表明,通过调节磁屏蔽环与加热线圈的间距可以抑... 针对感应加热炉磁屏蔽环异常发热问题,以30 t坩埚型感应加热炉为对象,采用COMSOL有限元分析软件计算并通过试验验证了带磁屏蔽环感应加热炉的磁感应强度和磁屏蔽环的温度场分布规律。结果表明,通过调节磁屏蔽环与加热线圈的间距可以抑制磁屏蔽环的异常发热;增加磁屏蔽环的横截面积,可以降低其发热温度。通过数值模拟结果对比得到了优化方案:磁屏蔽环与加热线圈的间距为480 mm,磁屏蔽环横截面积为1000 mm^(2)。现场测量结果表明,磁屏蔽环设计优化后漏磁场的磁感应强度由20.21 mT减小到19.54 mT,且温度由338℃降低到267℃,在保证屏蔽效果的基础上,抑制了磁屏蔽环的异常发热。 展开更多
关键词 感应加热 数值模拟 磁场屏蔽 系统优化 温度场
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集成热力学排气系统的蒸气冷却屏对液氢储罐自增压过程的影响
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作者 李科 朱顺 +1 位作者 文键 王斯民 《中南大学学报(自然科学版)》 北大核心 2025年第7期2953-2965,共13页
为进一步提升液氢储罐的绝热性能,首先,将氢气在热力学排气系统(TVS)释放冷量后,再将其引入真空多层绝热结构中的蒸气冷却屏(VCS),吸收从外部进入绝热结构的热量,从而形成冷遮挡;其次,利用MATLAB构建了真空多层绝热液氢储罐的自增压模型... 为进一步提升液氢储罐的绝热性能,首先,将氢气在热力学排气系统(TVS)释放冷量后,再将其引入真空多层绝热结构中的蒸气冷却屏(VCS),吸收从外部进入绝热结构的热量,从而形成冷遮挡;其次,利用MATLAB构建了真空多层绝热液氢储罐的自增压模型,包括了耦合热力学排气系统冷量源项的流体域传热传质模型和耦合蒸气冷却屏冷量源项的多层绝热结构导热模型;再次,研究了抽液氢或抽气氢时热力学排气系统、蒸气冷却屏、热力学排气系统串联蒸气冷却屏(VCST)对储罐休眠期的影响,休眠期由所定义的量纲一休眠期延长因子η_(d)表征;最后,讨论了储存过程中漏热热流密度以及TVS、VCS和VCST的吸热功率。研究结果表明:在抽液氢时,采用VCS或VCST时,使η_(d)最大化的蒸气冷却屏量纲一位置ld(表征了蒸气冷却屏在多层绝热结构中的位置)分别为0.400和0.489,对应的最大η_(d)分别为0.2237和0.3087;在蒸气冷却屏的基础上引入热力学排气系统,使η_(d)增大了38.00%。但抽气氢时,采用VCST相比于采用VCS时的η_(d)增加幅度非常小,额外添加TVS几乎不起作用。 展开更多
关键词 热力学排气系统 蒸气冷却屏 自增压 休眠期 传热传质模型 导热模型
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热屏影响下直拉法单晶硅生长能耗及传热路径研究
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作者 祁超 李登辇 +3 位作者 李早阳 杨垚 钟泽琪 刘立军 《人工晶体学报》 北大核心 2025年第6期949-959,共11页
单晶硅是太阳能电池的主要原材料,其生长成本直接影响电池的制造成本。因此,降低单晶硅生长能耗对光伏产业的降本增效至关重要。本文建立了直拉单晶硅生长的全局3D数值模型,考虑了单晶炉中加热器、电极等非旋转对称结构,能够更精确地模... 单晶硅是太阳能电池的主要原材料,其生长成本直接影响电池的制造成本。因此,降低单晶硅生长能耗对光伏产业的降本增效至关重要。本文建立了直拉单晶硅生长的全局3D数值模型,考虑了单晶炉中加热器、电极等非旋转对称结构,能够更精确地模拟单晶炉内的流动和传热过程。基于所建立的数值模型,研究了热屏冷、热侧发射率对单晶炉内能耗分配及辐射、对流和导热传热路径的影响规律。结果表明,冷、热侧发射率的降低均可取得明显的降耗效果,且降低冷侧发射率能够更加显著地降低能耗。在辐射传热方面,随着热屏冷、热侧发射率的降低,石墨坩埚和热屏热侧的吸热,以及硅熔体和热屏冷侧的放热均不断减小;随着热侧发射率的降低,顶保温的吸热出现了一定的增加。在对流传热方面,随着热屏冷侧发射率的降低,水冷屏吸热及热屏冷侧放热均不断增大,与冷侧相比,热侧发射率对对流传热的影响则相对较小。在导热传热方面,随着热屏冷热侧发射率的降低,热屏热侧到冷侧、石墨坩埚到石英坩埚,以及石英坩埚到硅熔体的导热均不断减小。本文研究结果可以为工业直拉单晶炉的精细化、深度化降耗提供重要的参考。 展开更多
关键词 热屏 能耗 传热路径 直拉单晶硅 数值模拟
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隔热屏结构对喷管壁面冷却影响的数值模拟
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作者 侯圣文 王强 +2 位作者 胡海洋 潘思霖 薄澜 《航空动力学报》 北大核心 2025年第1期78-89,共12页
以加力状态下的轴对称喷管为研究对象,数值对比研究了隔热屏翻边方式对喷管壁面冷却的影响。结果表明:无论对隔热屏进行两侧翻边还是出口翻边,隔热屏的最高温度和平均温度随着翻边高度的增加呈现先减小后增加的变化规律;对隔热屏进行两... 以加力状态下的轴对称喷管为研究对象,数值对比研究了隔热屏翻边方式对喷管壁面冷却的影响。结果表明:无论对隔热屏进行两侧翻边还是出口翻边,隔热屏的最高温度和平均温度随着翻边高度的增加呈现先减小后增加的变化规律;对隔热屏进行两侧翻边会增加收敛段壁面的平均温度和最高温度。相反,出口翻边则会降低收敛段壁面的最高温度和平均温度;两侧翻边时,扩张段壁面最高温度和平均温度最多可以降低2.6%和1.1%。出口翻边时,扩张段壁面的最高温度和平均温度受翻边高度影响较大,分别最多可以下降14.6%和23.5%。当以喷管扩张段壁面的冷却为研究目标时,则出口翻边更有利于喷管壁面冷却。 展开更多
关键词 加力状态 轴对称喷管 隔热屏结构 喷管壁面冷却 推力系数
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月面热管核反应堆电源系统方案研究
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作者 马明阳 李兵 +4 位作者 谢奇林 王三丙 张杨 梁文峰 钱达志 《载人航天》 北大核心 2025年第5期672-680,共9页
针对月球科研站等应用场景对大功率、长寿命电源潜在供给需求,开展了基于热管冷却技术的核反应堆电源系统总体方案设计分析研究。从不同层面进行了备选技术方案的比选分析,识别出影响任务完成度的潜在故障清单并提出了对策。结果表明:... 针对月球科研站等应用场景对大功率、长寿命电源潜在供给需求,开展了基于热管冷却技术的核反应堆电源系统总体方案设计分析研究。从不同层面进行了备选技术方案的比选分析,识别出影响任务完成度的潜在故障清单并提出了对策。结果表明:相同功率斯特林发电系统的单位质量比功率明显高于温差发电系统;采用相同能量转换技术,系统发电功率规模越大、单位质量比功率越高;月表以及能量转换模块、辐射散热器对中子和伽马的散射效应显著,需要有足够高的月壤挡墙或微型山脉对其遮挡方能保证人员所受辐照剂量不超限值;系统的故障模式按照严重程度可分为5类,需要制定专门的应对措施。相关分析结果和建议对月面核反应堆电源系统技术路线的优选和设计有一定参考价值。 展开更多
关键词 月球 能源 核反应堆 热管 辐射屏蔽
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变相位差双层波纹隔热屏冷却效率及流阻特性
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作者 王子文 刘海涌 +3 位作者 刘存良 傅松 黄晓锋 白晓辉 《航空动力学报》 北大核心 2025年第5期221-232,共12页
为了解决加力燃烧室纵向波纹隔热屏冷气用量多与波纹结构特征带来的局部低冷效区域的问题,提出了双层波纹隔热屏冷却结构。采用数值模拟方法,研究了变相位差、变振幅比条件下双层波纹隔热屏的冷却效率和流阻特性的变化规律。结果表明:... 为了解决加力燃烧室纵向波纹隔热屏冷气用量多与波纹结构特征带来的局部低冷效区域的问题,提出了双层波纹隔热屏冷却结构。采用数值模拟方法,研究了变相位差、变振幅比条件下双层波纹隔热屏的冷却效率和流阻特性的变化规律。结果表明:当相位差范围在-π/4~π/4时,局部低冷效区得到改善,同时隔热屏整体的面平均综合冷却效率和均温性得以提高。相位差为π/8时,双层波纹隔热屏的相对面平均综合冷效和冷效均匀度最高,分别为10.49%和13.44%。相位差在正、负方向过大会导致气膜孔流量分配不合理,增大气膜孔入口的突缩损失。另外发现,振幅比的增加可以有效提高波峰附近的冷却效率,减少波峰和波谷的冷效差值,振幅比为2时效果最优。 展开更多
关键词 加力燃烧室 纵向波纹隔热屏 冲击发散冷却 综合冷却效率 流阻特性
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液氢储罐中耦合蒸气冷却屏的连续变密度多层绝热的序列二次规划优化
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作者 李科 忻碧平 文键 《化工学报》 北大核心 2025年第3期985-994,共10页
为进一步优化应用于液氢存储的多层绝热结构的绝热性能,提出采用序列二次规划算法对耦合蒸气冷却屏(VCS)的连续变密度多层绝热辐射屏间距进行优化。研究了蒸气冷却屏位置、蒸气冷却屏内仲正转化以及蒸气冷却屏数量对最优辐射屏间距分布... 为进一步优化应用于液氢存储的多层绝热结构的绝热性能,提出采用序列二次规划算法对耦合蒸气冷却屏(VCS)的连续变密度多层绝热辐射屏间距进行优化。研究了蒸气冷却屏位置、蒸气冷却屏内仲正转化以及蒸气冷却屏数量对最优辐射屏间距分布以及绝热性能的影响。结果表明:蒸气冷却屏的引入使多层绝热最优辐射屏间距分布在蒸气冷却屏设置处出现突变,优化后漏热热通量qin相比于优化前下降幅度最大可达到36.1%;引入仲正转化的条件下优化可使qin的下降幅度最大达到28.3%;VCS数量的增加使最内层辐射屏间距显著减小,当蒸气冷却屏数量增加到2时,最小qin相比于单蒸气冷却屏下降50.4%。 展开更多
关键词 传热 优化 真空多层绝热 蒸气冷却屏 仲正转化
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基于主动冷屏绝热的超低温容器保冷性能优化
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作者 王鑫 苏宽 +5 位作者 朱鸣 韩文超 陈耀华 崔栋梁 程亮 陈叔平 《化工学报》 北大核心 2025年第10期5437-5452,共16页
超低温液体储存技术面临被动绝热方案热泄漏高与主动绝热方案能耗大的技术瓶颈。提出主动冷却屏(actively cooled thermal shield,ACTS)绝热与多层绝热(multi-layer insulation,MLI)耦合的热传递模型,以实现超低温容器热泄漏与冷却功耗... 超低温液体储存技术面临被动绝热方案热泄漏高与主动绝热方案能耗大的技术瓶颈。提出主动冷却屏(actively cooled thermal shield,ACTS)绝热与多层绝热(multi-layer insulation,MLI)耦合的热传递模型,以实现超低温容器热泄漏与冷却功耗的协同最小化。基于液氦容器搭建ACTS绝热性能实验装置,分析了MLI和ACTS的瞬态温度变化及热传递规律,验证了理论模型的精度。通过参数优化研究,揭示了ACTS温度、位置及数量对MLI温度梯度场、热通量分布及冷却能耗的影响机制。结果表明,ACTS通过温度梯度扩大了MLI的低温区,减小了低温容器与ACTS之间的温差;单ACTS的最佳温度和位置分别为73.6 K、0.425(位置0为冷端),温度临界值为150 K;双ACTS的最佳位置分别为0.2375、0.5875,其最佳温度为36.4、128.7 K,综合评价因子较单ACTS降低24.6%;三ACTS方案将热通量降低至0.0202 W/m^(2),相较于单/双ACTS分别降低44.6%、28.5%,验证了多个ACTS改善超低温容器绝热性能的显著优势。该研究为超低温容器主动绝热性能控制提供了理论依据与数据支撑。 展开更多
关键词 低温容器 低温绝热 主动冷却屏 传热 热力学 优化
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弹性隔热材料在火箭飞行极端环境下的应用
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作者 余雪敏 杨洋 +2 位作者 卢鹉 鄢东洋 张崇印 《宇航材料工艺》 北大核心 2025年第5期1-7,共7页
针对弹性隔热材料在火箭飞行极端环境下的应用研究进展进行综述。首先,概述了弹性隔热材料在固体火箭发动机热防护中的关键作用,以及其耐高温、耐高压与抗高速气流侵蚀的特性。随后,重点分析了丁腈橡胶、三元乙丙橡胶、硅橡胶及热塑性... 针对弹性隔热材料在火箭飞行极端环境下的应用研究进展进行综述。首先,概述了弹性隔热材料在固体火箭发动机热防护中的关键作用,以及其耐高温、耐高压与抗高速气流侵蚀的特性。随后,重点分析了丁腈橡胶、三元乙丙橡胶、硅橡胶及热塑性聚氨酯四类基体材料的改性策略。策略包括通过纤维增强、纳米填料协同及表面处理等技术,优化材料的烧蚀性能与机械性能。同时,探讨了碳层形成机制及多尺度填料对热防护效果的影响。最后,总结了现有材料在极端热流(>3000℃)下所面临的挑战,如碳层剥落、界面脱黏及环保性不足等问题。未来弹性隔热材料将不断发展创新,旨在提升其在极端环境下的性能,为火箭飞行安全提供保障。 展开更多
关键词 固体火箭发动机 烧蚀隔热 烧蚀隔热材料 弹性体 弹性隔热材料
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隔热屏对双喉道气动矢量喷管影响数值研究
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作者 丁浩元 周骏飞 +1 位作者 徐惊雷 付佳宁 《热能动力工程》 北大核心 2025年第3期45-54,共10页
以某型双喉道气动矢量喷管为研究对象,采用在喷管收缩段内壁面布置隔热屏的冷却方式,基于Realizable k-ε模型的雷诺时均方程,采用数值方法研究了隔热屏与壁面间距Δl分别为1,2,3 mm时尾部翻边结构对喷管壁面冷却效率及矢量性能的影响,... 以某型双喉道气动矢量喷管为研究对象,采用在喷管收缩段内壁面布置隔热屏的冷却方式,基于Realizable k-ε模型的雷诺时均方程,采用数值方法研究了隔热屏与壁面间距Δl分别为1,2,3 mm时尾部翻边结构对喷管壁面冷却效率及矢量性能的影响,并在Δl=2mm下进一步研究了隔热屏气膜孔对喷管冷却效率及矢量性能的影响。比较了喷管壁面冷却效率分布云图及对称面流线图,探究了隔热屏与壁面间距、翻边结构和气膜孔等对于冷却效率及矢量角的影响机理。结果表明:随着隔热屏与壁面间距的增加,喷管壁面冷却效率从0.730 7增加至0.957 4,但喷管矢量角损失也从0.79°增大到1.64°;增加隔热屏尾部翻边结构可提升凹腔上壁面冷却效率并减少隔热屏对喷管矢量性能的不利影响;开设隔热屏气膜孔可进一步提高凹腔侧壁面冷却性能并减小矢量角损失。 展开更多
关键词 气动矢量喷管 气膜冷却 隔热屏 气热耦合 数值模拟
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