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991.
本文简述了CO2 气体吸收率的测定原理 ,着重分析了影响连续碳分CO2 气体吸收率的因素 ,提出了提高连续碳分CO2 气体吸收率的途径 相似文献
992.
采用数值模拟和实验相结合的方法研究了钛合金TC4薄板常规及带热沉的钨极氩弧焊焊接过程中温度及应力应变的分布,考察了热沉对温度场和应力应变场的影响规律,探讨了使用该技术实现应力和变形控制的机理.结果表明:带热沉的钨极氩弧焊焊接过程中,紧随热源之后热沉急冷作用使得试件形成马鞍形温度场,而热沉作用部位温度最低.热沉作用部位的急冷收缩对周围金属产生拉伸作用,使得焊缝及近缝区金属升温过程中产生的压缩塑性应变减小,冷却过程中产生的拉伸塑性应变增大,接头中不协调应变减小,残余应力降低.实验测量与有限元模拟结果吻合良好,证实了采用热沉控制应力与变形的有效性和有限元模型的正确性. 相似文献
993.
994.
995.
TBC experience in land- based gas turbines 总被引:1,自引:0,他引:1
This paper summarizes prior and on-going machine evaluations of thermal barrier coatings (TBC) for power generation, that
is large industrial gas turbine applications. Rainbow testing of TBCs on turbine nozzles, shrouds, and buckets are described
along with a test of combustor liners. General Electric Power Generation has conducted more than IS machine tests on TBC turbine
nozzles with various coatings. TBC performance has been quite good, and additional testing, including TBCs on shrouds and
buckets, is continuing. Included is a brief comparison of TBC requirements for power generation and aircraft turbines. 相似文献
996.
997.
S. Gu D. G. McCartney C. N. Eastwick K. Simmons 《Journal of Thermal Spray Technology》2004,13(2):200-213
A computational fluid dynamics (CFD) model is developed to predict particle dynamic behavior in a high-velocity oxyfuel (HVOF)
thermal spray gun in which premixed oxygen and propylene are burnt in a combustion chamber linked to a long, parallel-sided
nozzle. The particle transport equations are solved in a Lagrangian manner and coupled with the two-dimensional, axisymmetric,
steady state, chemically reacting, turbulent gas flow. Within the particle transport model, the total flow of the particle
phase is modeled by tracking a small number of particles through the continuum gas flow, and each of these individual particles
is tracked independently through the continuous phase. Three different combustion chamber designs were modeled, and the in-flight
particle characteristics of Inconel were 625 studied. Results are presented to show the effect of process parameters, such
as particle injection speed and location, total gas flow rate, fuel-to-oxygen gas ratio, and particle size on the particle
dynamic behavior for a parallel-sided, 12 mm long combustion chamber. The results indicate that the momentum and heat transfer
to particles are primarily influenced by total gas flow. The 12 mm long chamber can achieve an optimum performance for Inconel
625 powder particles ranging in diameter from 20 to 40 μm. At a particular spraying distance, an optimal size of particles
is observed with respect to particle temperature. The effect of different combustion chamber dimensions on particle dynamics
was also investigated. The results obtained for both a 22 mm long chamber and also one with a conical, converging design are
compared with the baseline data for the 12 mm chamber. 相似文献
998.
In this article, we proposed a rapid and continuous process for the production of nanoporous coatings for functional applications.
Experiments following two statistical designs were implemented to screen and investigate the spraying parameters’ effects
on coating crystallinity and porosity in order to gain a better understanding. The spraying standoff distance, solution flow
rate and power were identified as having significant effects on coating porosity and crystallinity. The result yielded a peculiar
microstructure comprised of interpenetrating pores and layered structures with embedded pores. A deposition mechanism was
postulated to explain this microstructure. Ethanol gas sensors that are constructed from the coatings had comparable sensitivities
to those reported in the literature for thick-film coatings and had a maximum sensitivity near 200 °C.
This article is an invited paper selected from presentations at the 2007 International Thermal Spray Conference and has been
expanded from the original presentation. It is simultaneously published in Global Coating Solutions, Proceedings of the 2007 International Thermal Spray Conference, Beijing, China, May 14-16, 2007, Basil R. Marple, Margaret M. Hyland, Yuk-Chiu Lau, Chang-Jiu Li, Rogerio S. Lima, and Ghislain
Montavon, Ed., ASM International, Materials Park, OH, 2007. 相似文献
999.
1000.
The conservative method of calculating the Boltzmann collision integral for simple gases, gas mixtures and gases with rotational degrees of freedom of molecules is presented. In all cases the common approach based on the projection technique of summing up the contributions in the collision integral is used. The method is applied for solving the Boltzmann kinetic equation for two fundamental rarefied gas flow problems: the heat transfer problem and the problem of shock wave structure. A comparison with experimental and numerical data of other authors is reported. It is shown that the considered numerical method allows one to solve the Boltzmann equation for real gases with high accuracy. 相似文献