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1.
《中国航空学报》2020,33(3):1074-1084
Marciniack–Kuczinski (M–K) model is widely used to predict material’s forming limit curve (FLC). The prediction of FLC traditionally neglected through-thickness normal stress. However, it cannot be neglected in some forming processes. Much work has been done to study the effect of through-thickness normal stress on FLC with constant through-thickness normal stress or constant ratio of through-thickness normal stress and maximum principal stress. In addition, based on Nakazima test process, the ratio of through-thickness normal stress and maximum principal stress has been derived, which was a function of instantaneous thickness and loading path. Here, initial groove angle in M–K model was not considered. In this paper, uniaxial tension tests and Nakazima tests were performed on 7B04 aluminum alloy. Based on Hill 48 yield criterion and M–K model, the prediction model of FLC was established. The increase of thickness can enhance FLC. Meanwhile, it is necessary to consider through-thickness normal stress and initial groove angle in prediction model. On the left side of FLC, the effect of initial groove angle on FLC is weakened by increasing sheet thickness. On the right side of FLC, the effect of initial groove angle on FLC is strengthened by increasing sheet thickness. On the right side of FLC, the relation between limit strain points with different thicknesses is linear under one certain loading path. Thickness has decisive effect on through-thickness normal stress level and the changing trendy of through-thickness normal stress during calculation is different under different stress condition.  相似文献   
2.
用北京卫星环境工程研究所的18mm口径二级轻气炮(TLGG)和20 J激光驱动微小飞片装置(LDFF-20)对用作航天器舷窗玻璃的熔融石英玻璃的超高速撞击损伤特性进行了实验研究和分析.其中,TLGG发射的球形铝弹丸直径分别为1 mm和3 mm,速度2~6.5 km/s;LDFF-20发射的圆柱形飞片厚度7 μm,直径1 mm,速度1~8.3 km/s.撞击结果为:对12 mm厚的熔融石英玻璃,直径为3mm的弹丸甚至在2.8 km/s的低速下就将其穿透,而直径为1 mm的弹丸在6.5km/s的高速下没有穿透,这说明弹丸直径对撞击损伤特性有很强的影响;LDFF-20发射的微小飞片的撞击仅在玻璃表面产生很浅的凹坑,没有裂纹产生,但微小飞片的累积撞击损伤明显地降低了玻璃的透光性.实验初步获得了侵彻深度PC、侵彻直径D1与弹丸撞击速度Vp、弹丸质量Mp之间的经验关系.依据实验结果和目前的微流星体/空间碎片(M/OD)环境工程模型,建议对于高度为400 km、轨道倾角42°、寿命为3年的典型航天器,其舷窗玻璃的临界安全(非穿透)厚度至少为12mm.  相似文献   
3.
位移序列多进制扩频通信方式   总被引:2,自引:0,他引:2  
提出用 m序列的位移序列做扩频序列的多进制扩频通信方式 ,并给出了它的系统模型 ,分析了它的通信性能。理论分析证明 ,用 m序列的位移序列构成的多进制扩频通信方式具有很高的通信有效性和通信可靠性  相似文献   
4.
Ni-Cr-W-Al-Ti-MoS2 self-lubricating composites were prepared through the powder metallurgy (P/M) method. Their friction properties were investigated by a pin-on-disk tribometer in the range from the room temperature to 600 ℃. Alumina, silicon nitride and nickel-iron-sulfide alloys were selected as the counterface materials. Results indicate that the lowest friction coefficients under 0.22 can be obtained at 600 ℃ when rubbed against alumina. When rubbed against nickel-iron-sulfide alloys, are presented the lowest wear rates in the magnitude of 10-6 mm3/N·m, one order of magnitude lower than those when rubbed against ceramics. In the case of three rubbing pairs, the wear rates of the composite containing MoS2 present themselves inversely proportional to friction coefficients. With alumina ceramics used as a counterface, transfer films and glaze layers will form on the contact surface playing a main role in lubrication at high temperatures. However, when silicon nitride and nickel-iron-sulfide alloy are used, the lubricating transfer films appear not to be promi-nent.  相似文献   
5.
采用交、直流磁粉检验并结合金相试验、电子探针试验及微量元素含量分析的方法,对300M钢磁痕现象的本质进行了分析。结果表明,采用磁粉检验方法对航空优质钢进行纯洁度检验是可信的。  相似文献   
6.
利用回归分析方法得到国家财政部分主要支出项目,部分税收收入与国内生产总值构成的回归方程,由此构成线性规划问题的约束方程组。再用M单纯形法求最优解。  相似文献   
7.
随着电子产品小型化、高集成度的发展趋势,电子产品的封装技术正逐步迈入微电子封装时代。本文对微电子封装的关键技术进行了介绍,介绍了芯片互连工艺、典型封装技术和MCM技术。同时,本文对微电子封装技术的发展趋势及应用前景进行了综述。  相似文献   
8.
We use hourly monthly median values of propagation factor M(3000)F2 data observed at Ouagadougou Ionospheric Observatory (geographic12.4°N, 1.5°W; 5.9o dip), Burkina Faso (West Africa) during the years Januar1987–December1988 (average F10.7 < 130 × 10−22 W/m2/Hz, representative of low solar flux conditions) and for January 1989–December1990 (average F10.7 ? 130 × 10−22 W/m2/Hz, representative of high solar epoch) for magnetically quiet conditions to describe local time, seasonal and solar cycle variations of equatorial ionospheric propagation factor M(3000)F2 in the African region. We show that that seasonal trend between solar maximum and solar minimum curves display simple patterns for all seasons and exhibits reasonable disparity with root mean square error (RMSE) of about 0.31, 0.29 and 0.26 for December solstice, June solstice and equinox, respectively. Variability Σ defined by the percentage ratio of the absolute standard deviation to the mean indicates significant dissimilarity for the two solar flux levels. Solar maximum day (10–14 LT) and night (22–02 LT) values show considerable variations than the solar minimum day and night values. We compare our observations with those of the IRI 2007 to validate the prediction capacity of the empirical model. We find that the IRI model tends to underestimate and overestimate the observed values of M(3000)F2, in particular, during June solstice season. There are large discrepancies, mainly during high solar flux equinox and December solstice between dawn and local midnight. On the other hand, IRI provides a slightly better predictions for M(3000)F2 between 0900 and 1500 LT during equinox low and high solar activity and equinox high sunspot number. Our data are of great importance in the area of short-wave telecommunication and ionospheric modeling.  相似文献   
9.
通过分析碳纤维复合材料的性能特点及对切削加工性能的影响,提出了铣削刀具材料和几何结构形式的选用原则,介绍了几种适于碳纤维复合材料铣削的加工刀具。针对碳纤维复合材料中常用的M40/4211复合材料层合板进行加工缺陷试验和切削试验,总结出影响M40/4211复合材料层合板加工质量的因素及规律,得到每种刀具加工M40/4211复合材料层合板的最佳加工参数,较高的切削速度配合恰当的进给速度可以有效提高M40/4211复合材料层合板的加工质量和加工效率。  相似文献   
10.
 针对飞机结构部件在服役过程中存在的缝隙积水导致结构材料腐蚀的问题,通过研究腐蚀产物、形貌、失重、腐蚀速率、腐蚀损伤度以及积水溶液与暴露金属的面容比、pH值等的变化,探讨了300M超高强度钢在模拟积水环境中的腐蚀行为。结果表明,300M钢在模拟积水中的腐蚀是从点蚀开始,然后点蚀坑扩展合并,逐渐发展为全面腐蚀,其腐蚀失重和腐蚀损伤度随腐蚀时间的增加而增大,腐蚀损伤度则呈现出幂函数变化趋势;随腐蚀时间的延长,模拟积水环境中的pH值从初期的4.2升到5.2再下降到4.8~5.0,平均腐蚀速率也从0.289 g/(m2·h)线性减小到0.120 g/(m2·h);电化学交流阻抗结果表明随腐蚀时间的延长,容抗弧半径逐渐增大,说明腐蚀产物对基体起到一定的保护作用,这与腐蚀速率变化规律一致;另外,不同的面容比(腐蚀介质体积与300M钢暴露面积之比)对腐蚀过程的影响是:随面容比的增加,腐蚀失重与腐蚀速率均增大。  相似文献   
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