激光冲击强化对Ti2AlNb合金微观组织及残余应力的影响

Ti2AlNb(O-Ti2AlNb)具有优异的力学性能,在航空发动机方面有远大应用前景.激光冲击强化(Laser Shock Peening,LSP)是一种先进的表面改性技术,能够在材料表面诱导产生高幅值、大深度的残余压应力,改善材料微观组织,提高材料抗疲劳、高温氧化等性能.本文采用激光冲击强化对Ti2AlNb合金进行表面改性,并研究其组织演变、残余应力以及高温环境对性能的影响.结果表明:激光冲击强化能够显著减小Ti2AlNb合金近表面的晶粒尺寸.显微硬度由冲击前的350 HV提升到395 HV;在冲击区域近表面产生了约-377 MPa的残余压应力;而在高温环境中,由激光冲击强化所诱导的材料近表面残余应力随时间逐渐释放,在600℃条件下,残余应力释放较为缓慢;而在720℃条件下,残余应力迅速释放.     

一种控制高层结构随机地震反应的新策略

以某高层剪切型钢框架结构为工程背景,提出TMD与LRB联合作用的T-L控制策略,利用非线性随机振动理论分别对无控制、TMD控制和T-L控制3种控制结构的非线性运动方程进行等效线性化处理,利用复模态理论给出以第一振型表示的3种控制结构随机地震反应解析解的计算方法。研究结果表明:新提出的T-L控制策略比TMD控制更能显著降低结构位移、速度和加速度反应方差;新算法同样可用于求解LRB层间隔震高层结构随机地震反应。算例在T-L控制下的最大位移、速度和加速度反应方差比TMD控制下的分别降低了29.3%、27.8%和31.6%。     

考虑鲁棒性的超临界翼型激波控制鼓包减阻研究

本文主要采用CFD方法研究超临界翼型的激波控制鼓包减阻技术,分析了鼓包形状参数对减阻效果和鲁棒性的影响规律.计算结果显示,鼓包的减阻效果受位置影响较大,当鼓包最高点与干净翼型的激波位置相同时减阻效果较好,鼓包高度过高对减阻效果不利,而较长的鼓包可在更大的高度范围内实现减阻.鼓包还可以通过弱化激波,抑制附面层分离,延缓超临界翼型抖振现象的发生.计算结果显示,鼓包减阻技术整体而言工作范围较窄.但经过设计,较长且较低的鼓包可以在较大的升力范围内具有减阻效果,并且减阻效果对形状变化及雷诺数变化不敏感,还能有效提高阻力发散马赫数,鲁棒性要明显优于较短较高的鼓包,具有工程应用的潜力.     

Monitoring and analysis of shock wave in water for underwater drilling blasting

Taking the underwater reef blasting in Gulei sea channel of Xiamen Port as an example, the forming characteristic of shock wave in water for underwater drilling blasting is analyzed. By field monitoring, the pres- sure of shock wave in water for different distances is attained; the major parameters such as pressure amplitude and positive action time, and the propagation attenuation rule of shock wave in water are analyzed in this paper. The results can be helpful for engineering design and construction and environmental safety assessment.     

重度腹外伤后并发腹腔高压综合征的诊断及治疗

目的总结分析重度腹外伤后并发腹腔高压综合征的诊断及治疗经验.方法分析2例重度腹外伤伴失血性休克并发ACS病例,根据临床表现确定ACS诊断后,及时行腹腔减压,分别以腹壁覆盖及塑料袋缝合暂时性关腹.结果及时认识治疗ACS并行腹腔减压适量延长切口,结果满意,病患恢复平稳.结论对ACS的认识是及时诊断及治疗的关键,开腹减压以保证患者平稳渡过水肿期,选择合适的材料,有利于患者的康复.     

Cloning,sequencing of the HSC70 gene in Ctenopharyngodon idella

A cDNA encoding heat shock cognate protein 70(HSC70)was cloned from liver of grass carp(Ctenopharyngodon idella)(GenBank JF436930).This cDNA was found out to contain2 346 bp in length,including 1 950 bp of complete coding sequence encoding 649 amino acids(aa),plus 89 bp of 5′-UTR and 307 bp of3′-UTR.Analysis of its genomic structure revealed that its corresponding gene contained seven exons and six introns.Homology analysis indicated that it shared 99%of identity with HSC70 of breams and 86%of identity with HSP70 of Drosophila.Fluorescent RT-PCR analysis revealed that at 28℃,this gene was expressed in abdominal fat,muscle,intestines,brain,middle kidney,head kidney,gonads,swim bladder,liver,heart,spleen,gills,and fins with expression level in liver being the highest(p0.05),followed by that in the gonads;at 36℃,its mRNA expression level was increased at first but then decreased thereafter under heat shock stress,indicating that its expression can be regulated by heat shock.In conclusion,cloning and expression analysis identified a cDNA encoding a constitutive HSP70 gene that is expressed in many tissues of Ctenopharyngodon idella and its expression was down-regulated by heat shock.     

激光冲击处理对小孔构件残余应力场的影响

采用高功率 Nd：glass 激光器对 LY12CZ 铝合金小孔构件表面进行激光冲击强化处理,并对冲击区域进行残余应力场的测试与分析。结果显示,在激光功率密度为1．75 GW/cm2和光斑直径为6 mm 的强激光冲击作用下,冲击区域产生了残余压应力场,层深约1．2 mm,表面最大残余应力为-57 MPa,厚度方向上最大残余应力为-36 MPa。优化后的激光冲击处理工艺参数能够获得较好的残余应力场。     

三维爆炸场冲击波检测与可视化

根据冲击波的物理属性及其在数值模拟结果中的特点,将压力场转换为压力梯度场;然后在压力梯度场的体绘制过程中,通过合理设置空气介质的传递函数,实现了三维爆炸场冲击波特征的检测与可视化处理. 为了提高可视化效率,对基于光线投射的体绘制过程,采用查找表和包围盒等技术进行了加速处理. 算例测试结果表明,本文方法可以清晰展示三维爆炸场的冲击波特征.     

破片对聚能装药战斗部冲击引爆数值模拟分析

针对二次破片引爆车内弹药毁伤效能难评估问题,分析了基于热点学说的冲击引爆临界速度准则. 利用数值模拟方法,以反应度为引爆判断参数,进行了冲击引爆过程中炸药内部压力与状态分析,验证了热点引爆学说;得到了聚能装药撞击位置、破片尺寸、破片材料等参数对冲击引爆影响规律,直径相同时,柱形破片的临界起爆速度比球形破片低;聚能装药残余弹体或二次破片完全有可能引爆车体内弹药,从而导致严重的二次效应,钢质破片有效尺寸约14 cm、速度约1800 m/s,或者钨质破片有效尺寸约14 cm、速度约1500 m/s就能发生冲击引爆.      

Microstructure and oxidation resistance of SiC–MoSi2 multi-phase coating for SiC coated C/C composites

In order to improve the anti-oxidation of C/C composites, a SiC–MoSi2multi-phase coating for SiC coated carbon/carbon composites(C/C)was prepared by low pressure chemical vapor deposition(LPCVD) using methyltrichlorosilane(MTS) as precursor, combined with slurry painting from MoSi2 powder. The phase composition and morphology were analyzed by scanning electron microscope(SEM) and X-ray diffraction(XRD) methods, and the deposition mechanism was discussed. The isothermal oxidation and thermal shock resistance were investigated in a furnace containing air environment at 1500 1C. The results show that the as-prepared SiC–MoSi2coating consists of MoSi2 particles as a dispersing phase and CVD–SiC as a continuous phase. The weight loss of the coated samples is 1.51% after oxidation at 1500 1C for 90 h, and 4.79% after 30 thermal cycles between 1500 1C and room temperature. The penetrable cracks and cavities in the coating served as the diffusion channel of oxygen, resulted in the oxidation of C/C composites, and led to the weight loss in oxidation.