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1.434 we shall take the sample to test its physical properties (mechanical properties, tensile strength, yield point, percentage elongation, reduction of area, impact value, brinell hardness).
我们将取样试验其物理性能(机械性能、抗张强度、屈服点、延伸率、断面收缩率、冲击、布氏硬度)。收藏指正
2.Adopting sectional accelerated speed liner increase achieve inflexion smooth transition of saw liner accelerated speed,to reduce impact value.
同时采用部分加速度段线性增长的方法实现了锯车线性加速曲线拐点的平滑过渡 ,减小了冲击收藏指正
3.After heat treating (0.75%C) , u~= 1265MPa, 6514.5%, ak(20?C)=16.72J/cm2, the pearlite interlamellar spacing is to 0.09965pm, the 9?
经热处理后(0.75%C)σ_b=1265MPa,δ_5=14.5%,室温冲击16.72J/cm~2,金相组织为细片状珠光体,片间距为收藏指正
4.1. The mechanical property were achieved with as roll CrNb (0.75%C) rail steel: Gb-l O65MPa, 6~=1 0.5%, ak(20C) =1 3.3J/cm2,K1c(-20 t)33.OMPam? , the pearlite interlamellar spacing is to 0.1895pm, seven grade size of austenite grain is determined.
1.CrNb试验钢轨热轧后(0.75%C)σ_b=1065MPa,δ_5=10.5%,室温冲击13.3J/cm~2,-20℃下K_(IC)=33.0MPam~(1/2),金相组织为细片状珠光体,片间距0.1895μm,奥氏体晶粒度7级。收藏指正
5.This research revises the current theory of fragility and makes cushioning design for product more precise and more actual.
该研究完善了当前冲击理论,使缓冲包装设计更精确,更符合实际。收藏指正
6.Result The data of impact acceleration of return-cabins of "SZ-3"and "SZ-4" were accurately recorded during landing. Most reliable and scientific data were gotten.
结果设备在“神舟”3号、“神舟”4号飞行试验任务中准确记录了飞船返回舱返回着陆过程中的冲击加速度 ,获得了可靠的科学试验数据。收藏指正
7.1The heavy pulse current test results using the optimal grounding electrode obtained from the simulation experiment,suggest that the impulse coefficient α is not a fixed value which is related with the impulse current peak value,the type and arrangement of the electrodes.
通过对模拟试验中最优化的电极进行冲击大电流试验,得出冲击系数α的大小与冲击电流幅、电极形状和布置形式有关,不是一个定;收藏指正
8.The results show that the hardness and impact toughness of the alloy ZG30SiMnCr austempered at 300 ℃ for 60 min reach 47.13 HRC and 134.70 J/cm2,respectively. The alloy has an excellent comprehensive mechanical property. It has typical dual-phases austenitic-bainitic structure without carbides.
研究结果表明,ZG30SiMnCr经300℃×60 min等温淬火,试样的硬度达47.13 HRC,其冲击韧度为134.70 J/cm2,综合力学性能好,组织为典型的奥氏体-贝氏体组织,无碳化物相。收藏指正
9.The stress factor for the ladle turret or ladle support when pot is being received are described. From the view points of energy exchange, the theoretical calculation formula for the impact coefficient of ladle turret cantilever when pot is being received it also deduces and the affecting factor of the impact coefficient kd value. In addition is analyzes, example for checking the impact factor of Demag ladle turret is gived.
分析了钢包回转台或钢包座架受罐时的受力因素,并从能量转换观点出发,推导出钢包回转台悬臂梁受罐冲击理论计算公式,分析了冲击系数kd的影响因素,并举例核算了德马克设计的钢包回转台的冲击系数。收藏指正
10.The effects of quenching temper ature, aging temperature and time on microstrain △a/a have been investigated by means of X-ray diffraction. As shown in the electron transmission micro graph the reverted austenite disperses along ihebound aries of martensite, thus improving the impact toughness ak.
用X光衍射研究了淬火温度、时效温度及时间对微观应变△a/a的影响,透射电镜照片表明回火奥氏体沿马氏体边界析出,提高了冲击韧性ak收藏指正
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