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简介大型低温液体贮槽绝热系统的绝热材料及其主要性能指标;叙述了绝热系统的结构设计、氮封系统设计和基础设计,并分析了目前大型低温液体贮槽在订货、设计和使用中可能存在的几个问题和解决方法。 相似文献
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大型储油罐底板由中幅板和边缘板构成,采用对接和搭接接头,底板厚度较薄、面积大、焊缝数量多。因焊接应力和焊缝收缩的存在,焊接时易产生严重的焊接变形。通过制定合理的焊接工艺措施和对焊接过程进行有效的控制,以达到控制焊接变形的目的。 相似文献
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奥氏体不锈钢的低温力学性能优良,很适合于制造低温贮槽和装置,空分行业中用于贮存液氮、液氧、液氩等的真空粉末绝热低温液体贮槽就是由奥氏体不锈钢制成。本文详细介绍了这类贮槽的焊接技术。图2表1。 相似文献
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鉴于国内外大型常压低温液体贮槽设计完整性的管理要求,结合我国目前设计理念的发展程度,提出了完整性设计的概念。论述了完整性设计文件的要求,包括设计、采购、预制、安装和检验等方面的设计文件内容,为提升我国低温液体贮槽设计文件的详细程度,满足国内外用户对设计、制造、安装一体化要求提供了建议性的思路和要求。 相似文献
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从工艺流程、结构设计、力学计算、技术要领等方面阐明了大型常压低温液体贮槽设计、制造的诸多问题 ,特别是就如何保证大型常压低温液体贮槽的可靠性、先进性的关键问题作了一些分析。并简述了发展前景 相似文献
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简介大型低温液体贮槽的结构及地震破坏形式,以及储罐抗震设计的国内外标准。结合对几种典型容积大型低温液体贮槽采用不同标准进行抗震计算得到的结果,分析比较了采用国内外标准进行抗震设计的优缺点;最后,针对大型低温液体贮槽结构的特殊性,提出在进行抗震设计时值得注意的一些问题。 相似文献
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压力低温液体贮槽在使用过程中,所贮存的液体损耗率经常偏大,其主要原因为外界热量进入或气体和液体的泄漏。本文就以上两方面原因的现象及判断进行了详细分析。图1。 相似文献
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《低温学》2017
Liquid-nitrogen (LN2) circulation systems with altitude variation are investigated and designed for application to practical long-length HTS cables. This study is motivated by the KEPCO’s immediate plan to install new HTS cables in existing utility tunnels including inclined and vertical sections. The distribution of pressure and temperature along the LN2 circulation loop is examined for various geographic conditions, taking into account the gravitational effect of altitude variation. The cryogenic cooling requirements are defined in terms of the pressure and temperature of LN2, and a design process is graphically demonstrated on phase diagram. It is concluded that the LN2 flow rate along the cable with altitude variation should be carefully determined with the constraints on pressure and temperature, and the proposed graphical method is useful in the design. 相似文献
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主要通过氧化-还原反应的原电池原理阐述用碳钢制造液体CO2贮槽,贮存CO2中水分圣筒体内表面化学反应而腐蚀损耗所带来的影响以及防范措施。 相似文献
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本文介绍了子母型储罐、双层球罐、组合储罐各自的特点以及优缺点;结合三种不同结构的储罐,表明了奥氏体不锈钢可以良好用于深冷储罐。最后提出了选型的建议。 相似文献
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《低温学》2016
Liquid hydrogen (LH2) and liquid oxygen (LO2) cryogenic propellants can dramatically enhance NASA’s ability to explore the solar system due to their superior specific impulse (Isp) capability. Although these cryogenic propellants can be challenging to manage and store, they allow significant mass advantages over traditional hypergolic propulsion systems and are therefore enabling for many planetary science missions. New cryogenic storage techniques such as subcooling and the use of advanced insulation and low thermal conductivity support structures will allow for the long term storage and use of cryogenic propellants for solar system exploration and hence allow NASA to deliver more payloads to targets of interest, launch on smaller and less expensive launch vehicles, or both. These new cryogenic storage technologies were implemented in a design study for the Titan Orbiter Polar Surveyor (TOPS) mission, with LH2 and LO2 as propellants, and the resulting spacecraft design was able to achieve a 43% launch mass reduction over a TOPS mission, that utilized a traditional hypergolic propulsion system with mono-methyl hydrazine (MMH) and nitrogen tetroxide (NTO) propellants. This paper describes the cryogenic propellant storage design for the TOPS mission and demonstrates how these cryogenic propellants are stored passively for a decade-long Titan mission that requires the cryogenics propellants to be stored for 8.5 years. 相似文献
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A. Gütlein C. Ciemniak C. Coppi F. v. Feilitzsch C. Isaila J.-C. Lanfranchi L. Oberauer S. Pfister W. Potzel S. Roth W. Westphal 《Journal of Low Temperature Physics》2008,151(3-4):629-634
In Coherent Neutrino Nucleus Scattering (CNNS) the neutrinos interact coherently with all nucleons leading to a cross section
which is much larger than for all other neutrino interactions. Because of the small momentum transfer as well as the small
recoil energy in CNNS, and the relatively low count rate, a low energy threshold and a large target mass (several hundred
grams) are required to observe CNNS. Our aim is to build a cryodetector for that purpose. Such a cryodetector, installed in
the vicinity of a nuclear power plant, could probe new physics like non-standard neutral current interactions or a neutrino
magnetic moment. We describe the results of three detectors, with Ge absorbers of 0.8 and 3.2 g and with a CaWO4 absorber of 10 g. For Ge (0.8 g) an energy threshold of 0.43 keV and an energy resolution of 0.27 keV at ∼6 keV could be
reached. We demonstrate that surface roughness effects deteriorate both threshold and resolution. For the 10 g CaWO4 absorber we obtained 0.27 keV and 0.35 keV for threshold and energy resolution at ∼6 keV respectively.
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介绍空分制氮装置采用膨胀机循环与液氮循环的两种工艺流程及能量平衡 ,示出了两种循环的实例比较。指出外供液氮可以作为冷源替代膨胀机 ,且单耗低、操作更方便 ,设备维护量更小、氮气提取率更高 相似文献
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Tarek Saab 《Journal of Low Temperature Physics》2008,151(3-4):790-799
It is now well established and accepted that the universe has a total density equal to the critical density (Ω=1) and that
roughly 25% of that amount is accounted for by non-relativistic particles. That these particles, referred to as Dark Matter,
have remained a mystery has served to motivate physicists to design more ingenious and far reaching experiments in an attempt
to identify and understand them. This paper will review various ongoing and proposed Dark Matter searches which employ cryogenic
techniques to both detect the rare Dark Matter interactions as well as reject the vast number of background events from cosmic
ray and radioactive backgrounds. Such experiments are already sensitive to and are able to reject certain models of supersymmetry,
and with the increases in sensitivity projected over the next few years may even be able to detect these elusive particles.
相似文献