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1.
本文通过理论分析和数值模拟系统地研究了辐射热损失对球形火焰传播速度的影响。研究结果表明辐射热损失的影响分为直接影响和间接影响;直接影响指辐射热损失会降低火焰温度,从而降低火焰传播速度;间接影响指辐射热损失导致的冷却会引起逆向火焰传播的流动,从而降低火焰传播速度。对近可燃极限预混气体,直接影响起主导作用;对高辐射强度预混气体,间接影响起主导作用。本文研究的结果对球形火焰法测量火焰传播速度有着重要的指导意义。  相似文献   

2.
本文围绕可燃性纯质以及混合工质制冷剂的爆炸极限问题,提出了一种新的推算常温常压下可燃性制冷剂爆炸极限浓度的理论方法。在理论分析的基础上,通过合理设计,建立了一个精度较高的爆炸极限测试系统。通过对一系列可燃性制冷剂爆炸极限的测定,表明爆炸极限对于保证可燃性冷剂在生产和储存过程中的安全方面的重要性。  相似文献   

3.
本文对甲烷预混气在多孔介质中的火焰传播特性进行了实验研究,在开口竖直管中充填多孔介质,通过改变预混气氧含量使火焰在不同多孔介质中传播并测量火焰传播速度。预混气中氧含量最高达到29%。实验结果表明:多孔介质中甲烷可燃预混气火焰传播速度大于其层流火焰传播速度,可达到5倍以上(当量比的甲烷-空气预混气);多孔介质当量孔直径越大,或预混气层流火焰速度越高,则预混气火焰传播速度越高;多孔介质中可燃混气的火焰传播界限变小,当量孔直径大的多孔介质其界限值较大。实验结果与Babkin提出的多孔介质中的火焰传播机理相符。  相似文献   

4.
应用定循环运行压比优化方法,对采用环保型二元混合工质的单级压缩一次分凝循环,进行了-60℃温度位的循环性能数值优化。计算结果表明,影响循环COP的因素有混合工质成分(工质组元、工质浓度)和循环压力位(循环低压和循环压比),必须综合考虑进行优化。不可燃混合工质R23/R134a、R23/R227ea和R23/R236ea中,R23摩尔浓度为0.55和0.6的R23/R236ea循环在压比为7和10时,分别有最大的COP;自然混合工质R170/R290、R170/R600a和R170/R600中,R170摩尔浓度为0.65和0.7的R170/R600循环在压比为7和10时,分别有最大的COP。  相似文献   

5.
CO_2/DME(Dimethyl ether二甲醚)混合工质作为制冷剂既可以降低CO_2单独使用时过高的工作压力,又可抑制二甲醚的可燃性。针对跨临界热泵系统中制冷剂在超临界压力下放热时复杂的传热性能,本文对超临界CO_2/DME混合工质和超临界CO_2在螺旋管内流动冷却的换热过程进行了数值模拟研究。结果表明,与纯CO_2相比,在高温区CO_2/DME混合工质的换热性能更优;通过比较不同配比的CO_2/DME混合工质的换热特性,得到了不同温度范围对应的换热性能最优的CO_2/DME混合工质配比。此外,对固定质量比的CO_2/DME混合工质,分别分析了不同质量流速和热流密度下的流体温度、壁面温度及传热系数的变化规律,并与纯CO_2传热系数的变化进行了对比。该研究为制冷剂选取及热泵系统中气冷器的优化设计提供了理论依据。  相似文献   

6.
朱军韬  张华 《低温与超导》2012,40(1):53-56,61
由于压缩机压比的局限,制约着单一制冷剂的压缩回热循环发展,本系统采用单一压缩机和混合工质的自复叠制冷循环系统取得了较好的制冷效果。文中对单级自动复叠制冷系统进行了理论模拟,并设计和搭建了实验台进行分析。通过理论和实验数据的分析得出混合工质组合R600a/R23,并初步得到最优配比。  相似文献   

7.
论文对合R134a、R227ea的制冷剂爆炸特性进行理论和实验研究.提出含有阻燃组元的混合工质燃爆特性燃爆特性模型,给出实验与计算结果的比较。  相似文献   

8.
空调制冷工质R143a/R227ea、R125/R227ea的理论与实验研究   总被引:3,自引:0,他引:3  
1前言制冷剂R22的替代迫在眉睫,还未有一致的意见。但一般认为,R22的替代,无纯质可寻,只能采用混合工质。本文将从理论和实验两方面,探讨混合工质R143a/R227ea、R125/R227ea做为空调制冷系统,尤其是变浓度容量调节系统的循环工质的可行性。2R143a/R227ea、R125/R227ea的热力性质分析考虑到国内外对丙烷、丁烷衍生物制冷工质的研究较少,二元混合工质的组成纯质将不仅从甲烷、乙烷系列中筛选,还将考虑采用丙烷、丁烷衍生物中的一些热物性和物理化学性质研究较充分的物质。从组成纯质及变浓度等几个角度加以筛选,本文推荐采…  相似文献   

9.
空调循环中HCs/阻燃剂混合工质的泄漏特性   总被引:4,自引:0,他引:4  
结合空调循环分析了非共沸HCs/阻燃剂混合工质的泄漏特性,包括一定泄漏率下引起最大组成变化的泄漏点和工质相态、泄漏率-总组成变化关系、泄漏引起的组成变化对HCs/阻燃剂混合工质安全性与循环性能的影响分析。  相似文献   

10.
制冷系统可燃工质泄漏喷射过程的模拟研究   总被引:7,自引:1,他引:6  
本文提出了制冷系统气相可燃工质泄漏量的计算方法。并根据射流原理,对可燃工质泄漏过程的速度场与浓度场进行了模拟计算。根据计算结果提出了局部着火与爆炸的概念。  相似文献   

11.
秦彪  李瑛  王芳  陈敏 《低温与超导》2012,(8):49-53,22
依据国家标准GB/T7725-2004《房间空气调节器》、GB/50016-2006《建筑设计防火规范》和上海出入境检验检疫局技术协议要求,设计并建造一套可燃制冷剂空调器性能测试实验室。目前,国内主要采用空气焓值法对空调器进行其性能的测试。为了保护臭氧层及降低温室效应,现代制冷工业以逐渐开始用环境友好型碳氢化合物制冷剂取代传统制冷剂,并已在家用空调器中逐渐开始使用。  相似文献   

12.
The results of experimental studies on using an electrical discharge with an extended streamer structure in a quasioptical microwave beam in the multipoint ignition of a propane–air mixture have been reported. The pulsed microwave discharge was initiated at the interior surface of a quartz tube that was filled with the mentioned flammable mixture and introduced into a microwave beam with a subbreakdown initial field. Gas breakdown was initiated by an electromagnetic vibrator. The dependence of the type of discharge on the microwave field strength was examined, the lower concentration threshold of ignition of the propane–air mixture by the studied discharge was determined, and the dynamics of combustion of the flammable mixture with local and multipoint ignition were compared.  相似文献   

13.
The work presents the results of cycle computation for vapor compression pumps based on ozone-safe mixed refrigerants. Non-azeotropic binary refrugerants R32/R152a (30/70) and R32/R134a (30/70) were considere as working substances. Properties of non-azeotropic refrigerants were calculated according to the additivity method of thermodynamic functions and method of Lemmon and Jacobsen. Deviations in the values of thermophysical properties obtained with two methods have been determined. It is shown that at the use of nonazeotropic mixture R32/R152a (30/70), energy conversion ratio increases by 2.2–3.6 % compared with the results for R32/R134a (30/70) at temperature difference between the processes of boiling and condensation from 28 to 53 °C.  相似文献   

14.
主要利用NIST8.0软件,针对R23/R134 a,R23/R600 a,R23/R125,R23/R14等二元混合工质在Linde-Hampson循环下进行了理论分析,设计一套可制得-60℃的单级压缩节流回热循环系统。通过对工质成分特性分析对比,研究其对循环的热力学性能的影响规律,得到了最佳制冷剂组合。  相似文献   

15.
R22/R23自动复叠低温冷柜的分析   总被引:1,自引:1,他引:0  
对一采用 R2 2 / R2 3自动复叠的低温冷柜进行了试验研究 ,建立该装置各部件火用分析模型并分析各部件火用流情况。结果显示该装置中压缩机的火用损最大  相似文献   

16.
符号表G流量密度,kg/m‘·s人阻力系数,N/mZg气相M质量流量,kg/S6修正系数i,j组分w速度,m/s下角标l液相长度,me临界状态印两相1前言毛细管的设计是小型制冷装置设计的一个重要组成部分,由于毛细管的管径和壁厚已标准化,所以毛细管的设计是长度的设计。毛细管内流体为一典型汽一液两相流动过程,机理复杂,目前人们对毛细管的研究主要集中在纯质方面K叫。由于制冷**C替代工质现多为二元或三元混合工质,与纯质系统有所不同,因此有必要对混合工质在毛细管内两相流动规律进行研究,为毛细管的设计提供依据。2理论模型2.1基…  相似文献   

17.
The study of edge flames has received increased attention in recent years. This work reports the results of a recent study into two-dimensional, planar, propagating edge flames that are remote from solid surfaces (called here, “free-layer” flames, as opposed to layered flames along floors or ceilings). They represent an ideal case of a flame propagating down a flammable plume, or through a flammable layer in microgravity. The results were generated using a new apparatus in which a thin stream of gaseous fuel is injected into a low-speed laminar wind tunnel thereby forming a flammable layer along the centerline. An airfoil-shaped fuel dispenser downstream of the duct inlet issues ethane from a slot in the trailing edge. The air and ethane mix due to mass diffusion while flowing up towards the duct exit, forming a flammable layer with a steep lateral fuel concentration gradient and smaller axial fuel concentration gradient. We characterized the flow and fuel concentration fields in the duct using hot wire anemometer scans, flow visualization using smoke traces, and non-reacting, numerical modeling using COSMOSFloWorks. In the experiment, a hot wire near the exit ignites the ethane-air layer, with the flame propagating downwards towards the fuel source. Reported here are tests with the air inlet velocity of 25 cm/s and ethane flows of 967-1299 sccm, which gave conditions ranging from lean to rich along the centerline. In these conditions the flame spreads at a constant rate faster than the laminar burning rate for a premixed ethane-air mixture. The flame spread rate increases with increasing transverse fuel gradient (obtained by increasing the fuel flow rate), but appears to reach a maximum. The flow field shows little effect due to the flame approach near the igniter, but shows significant effect, including flow reversal, well ahead of the flame as it approaches the airfoil fuel source.  相似文献   

18.
Density (ρ), viscosity (η) and ultrasonic velocity (u) of binary mixtures of methyl orange and water were measured at different concentrations and at different temperatures; several useful parameters such as excess volume, excess velocity, and excess adiabatic compressibility have been calculated. These parameters are used to explain the nature of intermolecular interactions taking place in the binary mixture. The above study is helpful in understanding the dye/solvent interaction at different concentration and temperatures.  相似文献   

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