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ESTIMATION METHOD OF RESIDUAL LIFE OF HOLLOW METAL PART, HAVING WORKED UNDER CREEPING CONDITIONS AT HIGH PROCESS TEMPERATURE AND PRESSURE

机译:在高温高压下蠕变条件下工作的空心金属零件的剩余寿命估算方法

摘要

FIELD: test equipment.;SUBSTANCE: after the equipment is stopped, the time τe from the indicated part operation start up to the indicated stop of exploitation is fixed, check if there are any microdamages in various areas of the outer surface of the controlled part, as well as the maximum level of the microdamage in the most damaged area. The target value of the residual life is calculated bythe mathematical relation τrl=Krl⋅τe, where Krl - residual life coefficient, determined on the basis of its experimental dependence on the level of microdamage Ωcp of the controlled part. The section of the metal is cut from the least loaded part of the controlled part to produce the round section samples series, each of the samples is tested for creeping before fracture with the continuous load at the temperature above the operating value during the CP operating process. Based on the test results of these samples, plot the graphical dependence of the sample microdamage level Ωsam from the worked out durability share τwdsik, where τi - is the current time from the test start, τk - time from the tests start up to the sample fracture. For several points (i) of the indicated graphical dependence, calculate the values of the residual life coefficient Krl of the sample, starting from the mathematical relation τrli=Krli⋅τi, where τrlik⋅(1-τwds). Plot the new graphical dependence of Krl=f(Ωsam) with the exception of the time parameter. Calculate the residual life of the controlled part, use the mathematical ratio τrl=Krl⋅τe, where Krl is defined from the specified graphical dependence according to the Krl=f(Ωsam). The series consists of at least two pairs of samples. One of the samples of each pair is left solid, and the other is made with the annular tapped notch in the central part, that simulates in the known way the specified value of the controlled part surface microdamage, so that the sample section damage by the indicated annular notch level ω corresponds to the microdamage level Ω. The samples tests are done at the specific load within the range 0.9-1.1 of the operating value and the temperature for each subsequent pair higher than the previous one by 10-50°C. The minimum from these indicated temperatures is selected from the condition, that the time up to the fracture of the sample does not exceed 6200 hours. The sample with the annular notch of each pair selected for testing is given its own value ω. When plotting the indicated dependence of the microdamage level Ωsam=f(τwds), the solid sample relative loading time of each mentioned pairs prior its rupture on the mentioned graphical relationship is fixed as τk=1, and the relative loading time of the sample with the annular notch prior to its destruction - as τwds.;EFFECT: elimination of the intermediate stops and measurements necessity during the samples testing.;6 dwg, 3 tbl
机译:现场:测试设备;实质:设备停止运行后,从指示的零件运行开始到指示的开采停止时间τ e 是固定的,请检查各个区域是否存在任何微损伤受控部件外表面的最大损伤程度以及最受损区域的微损伤的最大程度。通过数学关系式τ rl = K rl ⋅τ e 计算剩余寿命的目标值,其中K rl -剩余寿命系数,根据其对受控部件微损伤Ω cp 的水平的实验依赖性确定。从受控零件的最小负载部分切下金属部分,以生成圆形截面样品系列,在CP操作过程中,在温度高于操作值的温度下,连续载荷在破裂之前测试每个样品的蠕变,然后进行破裂。根据这些样品的测试结果,从计算出的耐久性份额τ wds i 绘制样品微损伤水平Ω sam 的图形依赖性。 Sub> /τ k ,其中τ i -是从测试开始的当前时间,τ k -从测试开始到当前的时间样品断裂。对于指示的图形依存关系的几个点(i),从数学关系τ rli = K <开始计算样品的剩余寿命系数K rl 的值Sub> rli ⋅τ i,其中τ rli k ⋅( 1-τ wds )。绘制除时间参数外的K rl = f(Ω sam )的新图形依存关系。计算受控零件的剩余寿命,使用数学比率τ rl = K rl ⋅τ e ,其中K rl < / Sub>是根据K rl = f(Ω sam )从指定的图形依存关系定义的。该系列包括至少两对样本。每对样品中的一个保持固体状态,另一个在中心部分带有环形螺纹缺口,以已知方式模拟受控零件表面微损伤的指定值,从而使样品截面受到损伤。所示的环形缺口水平ω对应于微损伤水平Ω。样品测试是在操作值的0.9-1.1范围内的特定负载下进行的,随后每对温度比前一对温度高10-50°C。这些指示温度中的最小值是从以下条件中选择的,即直至样品破裂的时间不超过6200小时。选择用于测试的每对均具有环形槽口的样品具有自己的值ω。当绘制指示的微损伤水平Ω sam = f(τ wds )的依赖性时,每个破裂对在其破裂之前的固体样品相对加载时间均取决于所述图形关系固定为τ k = 1,样品在破坏前具有环形缺口的相对加载时间为τ wds 。;效果:消除中间体在样品测试过程中停止并进行必要的测量。6dwg,3 tbl

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