我国固体火箭发动机衬层成型技术进展

衬层是推进剂与绝热层或壳体之间的高分子弹性体涂层，衬层成型是固体火箭发动机生产中的一种特种工序。我国固体火箭发动机衬层成型工艺如离心成型、刷涂、拉涂、喷涂等工艺不断向前发展。综述我国固体火箭发动机衬层成型工艺的现状和发展，介绍了无溶剂高固体份衬层抛涂成型新技术的试验结果。     

考虑恶劣天气的班轮多阶段重调度方法

受恶劣天气影响的船舶调度是一个非常复杂的优化问题,也是班轮公司重点关注的问题之一。为此,针对某航运网络上的一家班轮公司的所有营运船舶,以获知设计的多阶段重调度机制时段内最新预报的天气信息和这些船舶的实时位置为前提,重点考虑班轮船期表的限制并兼顾港口间航速变化和船舶容量等现实约束,构建了以固定计划期内所有船舶的航运总成本最小为优化目标的非线性数学模型,并设计了嵌入基因修复算子的改进遗传算法用于求解该模型。由此,可以给出集成租船直运、跨航线调船、反挂和货物中转等解决策略的最佳多阶段重调度方案。通过对大、中、小规模的算例进行实验,实验结果表明,可知与传统等待办法相比,多阶段重调度节约了总航运成本的15%以上,验证了所提模型和方案的有效性;与Cplex相比,改进遗传算法的运算效率大大提高,且偏差值均在5%以内,而与蚁群优化（ACO）算法、禁忌搜索（TS）算法、量子差分进化（QDE）算法相比,改进遗传算法能在有效时间内降低10%左右的成本,验证了算法的科学性。所提方法可为班轮公司的实际船舶调度提供参考。     

Optimized design of biconical liner by orthogonal method

A biconical liner was optimized to improve its penetration ability. Its formation and penetration mechanism was studied through numerical simulation and experiments. And the influence of different liner geometry sizes on the jet performance was analyzed using the orthogonal method. The liner formed the high-speed jet with an explosively formed projectile. The small angle 2α remarkably influenced the jet speed which was inversely proportional to 2α. And the liner thickness t' and large angle 2β had highly significant effect on the projectile speed. The liner was optimized at t' = 0. 14 cm,2α = 50°,2β = 135°,N = 0. 4 or 0. 5,when its jet speed respectively is at 6 613 m /s and 6 839 m /s and projectile speed is at 2 247 m /s and 2 095 m /s,steel target penetration is at 8. 24 cm and 8. 31 cm,and aperture is in 2. 12 cm and 2. 08 cm. The results show that target is penetrated by the high-speed jet and high-speed projectile resulting into double damages. The penetration ability is improved greatly.     

基于时滞不等分法T-S模糊时滞系统稳定性准则

提出一种新的时滞分解方法—时滞不等分法,研究了T-S模糊常时滞系统的稳定性准则问题。基于Lyapunov稳定性理论,构造恰当的Lyapunov-Krasovskii泛函,以线性矩阵不等式形式给出一个决策变量少、运算效率高、保守性小的时滞相关稳定性准则。最后给出数例说明该方法的有效性。     

提高身管寿命的粉末冶金内衬和衬管

本文介绍了国外用粉末冶金制合金内衬方法的特点,工艺过程和应用实例,阐述了钼合金衬管制造方法的研究和进展。     

G32柴油机气缸套的铸造技术

介绍G32重型柴油机合金灰铸铁缸套的生产技术。采用离心铸造、中频炉熔炼，铸件化学成分为：w（C）2．9％～3.2％，w（Si）1．7％～2．0％，w（Mn）0．7％-1．0％，W（P）0．25％-0．30％，w（S）0．08％-0．10％，w（Cr）0．25％-0．30％，w（Mo）0．30％-0．50％，w（Cu）0．6％～0．9％。为改善孕育效果，通过加入硫化铁，有意地提高铁液埘（s）量。铸型转速为695r／min，铸型壁厚为气缸套大端厚度的1．2倍，浇注速度20～40kg／s，旋转成型时间30min。     

硼铸铁缸套激光表面熔凝组织和性能的研究

为了提高硼铸铁缸套的耐磨性能，对硼铸铁气缸套进行激光熔凝处理。利用扫描电子显微镜观察了激光熔凝处理后的显微组织。利用显微硬度计检测了激光熔凝组织的显微硬度，同时进行了以GCr15钢标准环为配副的环块磨损试验。研究结果表明，硼铸铁经激光熔凝处理后得到了共晶莱氏体 马氏体组织，而且激光熔覆层厚度可控，组织和性能稳定，熔凝强化表层显微硬度达到800-1200HV0.2。磨损试验结果显示，激光熔凝处理后，磨损截面积比未处理的试样减小了44.4%，从而表明激光熔凝处理是提高硼铸铁缸套耐磨性能的有效手段。     

低液位铸造技术在铝合金扁锭生产中的应用

介绍低液位铸造技术的核心，石墨内衬对铸造的扁锭提供了理想的表面，铸造出的扁锭表面平滑无偏析瘤，偏析深度仅200μm～500μm，铸锭壳区厚约1μm，可减少铣面量50％，两大面只需铣削2mm～4mm，减少热轧切边量17％，大大提高了扁锭的成材率。     

工业回转窑窑衬清窑机器人多关节并行驱动的液压系统动态仿真研究

设计出了工业回转窑窑衬清理机器人的液压驱动系统,并且绘制出能够反映系统动态特性的多关节并行驱动的液压系统的功率键合图。由此建立了包含11个子系统的非线性动力学状态方程,然后根据每个方程的各状态变量之间形成的输入与输出关系构建了系统动态特性仿真模型,然后利用SIMULINK软件包进行了该方程组的求解,获得了满意的仿真结果。     

Optimization of casting conditions for heat and abrasion resistant large grey iron castings

Numerical simulation technology was applied for optimizing the casting design and conditions in large cast iron castings for marine engine. By the simulation of mold filling and solidification sequences the problems of the previous casting conditions were analyzed and marked improvements for large cylinder liner parts were derived from these results. Especially the amount and positions of chills were optimized to increase the mechanical properties and to minimize the shrinkage and microporosity in the castings. Ultrasonic testing, penetration testing and mechanical property testing were carried out for the parts with the modified casting conditions. It showed that no defects in the castings were found and the productivity could be distinctly increased. The mechanical properties satisfied also the specification demanded.