转速对压气机级间篦齿封严影响的实验

对压气机级间篦齿封严进行了实验研究.不同压比下（1.05~1.3）,研究转速（1500~8100r/min）对压气机级间篦齿封严的工作间隙变化、泄漏特性、温升特性和旋流特性的影响.结果表明:随转速的增大,工作间隙减小,流量降低;小压比时流量系数降低,较大压比时流量系数变化微小.系统风阻温升随转速增大而增大,转速越大时,其温升越明显.另外,随转速的增大,出口盘腔同一径向位置的旋转比增大;同一转速下,随出口盘腔径向位置的增大,旋转比降低.      

反压诱导方式对超燃冲压发动机隔离段流动特性影响

为了探究传统机械限流方式同燃烧释热对隔离段流动特性影响的异同,采用实验结合数值计算的方法研究了限流方式与实际燃烧诱导压升的差异.使用氢燃料进行不同当量比的燃烧实验,并使用燃烧室出口安装楔块的方式进行限流实验,对比了来流条件相同,且隔离段出口压比相同时两种实验下的压力分布.使用经过验证的数值方法模拟了不同隔离段出口压力下燃烧状态及对应的限流状态,对比了两种状态下隔离段流场细节.实验结果表明:激波链即将进入隔离段时,两者的压力分布大致相同;激波链进入隔离段后,隔离段出口压比2.3,两者的壁面压力分布有明显差别.此状态下的计算结果表明:燃烧状态下隔离段内分离区首先出现于下壁面,激波链向上偏折;而限流状态分离区出现于上壁面,两者的流场会有一定差异.反压继续增大的计算结果表明:隔离段出口压比达3.0时,两者的隔离段内流场差别逐渐减小并最终趋于一致.燃烧反压场与限流实验的模拟反压场一致时,才能直接采用限流实验的结果评估反压对进气道的扰动风险.      

一种基于模型的涡扇发动机容错控制策略

针对民用涡扇发动机,研究了一种基于模型的航空发动机容错控制策略.在发动机原有闭环控制系统的基础上,该策略对发动机各控制量进行容错控制修正,达到缓和甚至消除故障对控制系统影响的目的.针对民用涡扇发动机常见的高压压气机和高压涡轮性能退化故障,提出了以恢复发动机运行性能为目的的性能指标,通过遗传算法离线计算得到容错控制计划表,并利用插值计算实现在线容错控制.经仿真验证,该策略控制性能良好、实现简单.结果表明:在确保各温度限制不超标的情况下,受影响较大的增压级喘振裕度恢复至故障发生前的水平,同时风扇与高压压气机喘振裕度的降幅不超过5%,推力的降幅不超过3%.      

Microstructure control techniques in primary hot working of titanium alloy bars:A review

How to control the microstructure of titanium alloy bars is important to fabricating high-performance aerial forgings. This paper gives a thorough survey of the manufacturing meth-ods and microstructure control techniques for titanium alloy bars. It summarizes the effects of pro-cessing parameters on the mechanisms and laws of microstructure evolution during b working and (a+b) working, including the kinetics and grains size of dynamic recrystallization (DRX) during b deformation and the kinetics and grains size of spheroidization during (a+b) deformation. The trends in microstructure control techniques are presented for fabricating titanium alloy bars with high efficiency, low cost, and high quality by means of b/(a+b) working, and the puzzles and chal-lenges in the future are also pointed out.     

Cutting tool temperature prediction method using analytical model for end milling

Dramatic tool temperature variation in end milling can cause excessive tool wear and shorten its life, especially in machining of difficult-to-machine materials. In this study, a new analyt-ical model-based method for the prediction of cutting tool temperature in end milling is presented. The cutting cycle is divided into temperature increase and decrease phases. For the temperature increase phase, a temperature prediction model considering real friction state between the chip and tool is proposed, and the heat flux and tool-chip contact length are then obtained through finite element simulation. In the temperature decrease phase, a temperature decrease model based on the one-dimension plate heat convection is proposed. A single wire thermocouple is employed to mea-sure the tool temperature in the conducted milling experiments. Both of the theoretical and experi-mental results are obtained with cutting conditions of the cutting speed ranging from 60 m/min to 100 m/min, feed per tooth from 0.12 mm/z to 0.20 mm/z, and the radial and axial depth of cut respec-tively being 4 mm and 0.5 mm. The comparison results show high agreement between the physical cutting experiments and the proposed cutting tool temperature prediction method.     

Vibration suppression of thin-walled workpiece machining considering external damping properties based on magnetorheological fluids flexible fixture

Milling of the thin-walled workpiece in the aerospace industry is a critical process due to the high flexibility of the workpiece. In this paper, a flexible fixture based on the magnetorheological(MR) fluids is designed to investigate the regenerative chatter suppression during the machining.Based on the analysis of typical structural components in the aerospace industry, a general complex thin-walled workpiece with fixture and damping constraint can be equivalent as a rectangular cantilever beam. On the basis of the equivalent models, natural frequency and mode shape function of the thin-walled workpiece is obtained according to the Euler–Bernoulli beam assumptions. Then,the displacement response function of the bending vibration of the beam is represented by the product of all the mode shape function and the generalized coordinate. Furthermore, a dynamic equation of the workpiece-fixture system considering the external damping factor is proposed using the Lagrangian method in terms of all the mode shape function and the generalized coordinate, and the response of system under the dynamic cutting force is calculated to evaluate the stability of the milling process under damping control. Finally, the feasibility and effectiveness of the proposed approach are validated by the impact hammer experiments and several machining tests.     

离心锤变桨距机构设计与优化研究

针对现有高空飞艇螺旋桨推进系统中,采用变桨距技术重量代价大、能源消耗多的问题,设计一种基于离心力的离心锤变桨距机构,分析该机构的工作原理,并利用ADAMS软件进行机构运动学和动力学仿真分析;对离心锤进行参数化建模,建立约束方程后,以桨距优化角为目标函数,对离心锤的空间位置进行优化.结果表明:当外界条件引起螺旋桨转速变化时,该机构可以很好地实现螺旋桨变桨距功能;在现有平台上,48°的离心锤安装角具有最优的变距效果.     

确定微型固体火箭发动机燃烧时间的CAA与CAD技术

应用计算机辅助分析(CAA)与计算机辅助绘图(CAD)方法,确定微型固体火箭发动机燃烧时间t_b。该方法自动化程度高、精度好,有可靠的理论依据。用它替代传统的没有任何理论根据的手工画角分线法,以提高小型固体火箭发动机内弹道数据处理的精度和速度是十分必要的。实践证明这是一种科学的可行的方法,值得推广。     

复合材料结构可靠性分析与设计

本文根据复合材料结构可靠性分析的特点提出复合材料结构的基本元件层压板的可靠性分析的方法。在此基础上将常规的优化设计发展为在可靠性基础上的优化设计并提出在板层压可靠性基础上铺层优化设计的方法。最后提出复合材料结构系统可靠性分析方法和确认主要破坏模式的方法。     

BTT导弹时变滑态变结构自适应自动驾驶仪设计

针对倾斜转弯导弹的具体特点, 提出了一种基于模型参考时变全程滑态变结构控制理论的协调式耦合自动驾驶仪的设计方法, 并分别针对滚转通道、俯仰/偏航耦合通道进行了设计分析; 最后进行了三通道联合仿真, 得到了满意的结果