强5飞机减摆器轴断裂原因初探

强５飞机减摆器是防止前轮摆振的关键构件。本文用疲劳断裂理论估算该构件的安全寿命和裂纹扩展寿命，并提出了维修及设计改进建议。     

接管断裂失效概率估算的抽样方法研究

提出了用分层抽样－重要性抽样复合法计算接管的断裂失效概率，并与直接抽样的ＭｏｎｔｅＣａｒｌｏ法进行了比较，结果表明：用复合法计算接管断裂失效概率不但精度高，而且大幅度节省机时，提高效率。     

Evaluation of mixed mode-I/II criteria for fatigue crack propagation using experiments and modeling

In this study, in-plane mixed mode-I/II fatigue crack growth simulations and experiments are performed for the Al 7075-T651 aluminum alloy which is widely used in the aerospace industry. Tests are carried out under different mode mixity ratios to evaluate the applicability of a fracture criterion developed in a previous study to mixed mode-I/II fatigue crack growth tests. Results obtained from the analyses and experiments are compared with existing and developed criteria in terms of crack growth lives. Compact Tension Shear (CTS) specimens, which enable mixed mode loading with loading devices under different loading angles, are used in the simulations and experiments. In an effort to model and simulate the actual conditions in the experiments, crack surfaces of fractured specimens are scanned, crack paths are modeled exactly, and contacts are defined between the contact surfaces of a specimen and the loading device for each crack propagation step in the analyses. Having computed the mixed mode stress intensity factors from the numerical analyses, propagation life cycles are predicted by existing and the developed mixed mode-I/II criteria and then compared with experimental results.     

仅值班供油时斜流驻涡燃烧室出口温度分布特性研究

为深入了解和掌握仅值班供油时斜流驻涡燃烧室出口温度分布特性,开展了不同进气速度和油气比下燃烧室出口温度径向分布、不均匀性及出口温度分布系数(OTDF)和出口径向温度分布系数(RTDF)的研究,并结合凹腔内火焰形态分析了出口温度分布特性的变化原因.结果表明,不同进气速度和油气比下出口温度径向分布都呈现为中间高、两端低,温...     

Improving surface integrity when drilling CFRPs and Ti-6Al-4V using sustainable lubricated liquid carbon dioxide

In the quest for decreasing fuel consumption and resulting gas emissions in the aeronautic sector, lightweight materials such as Carbon Fiber Reinforced Polymers (CFRPs) and Ti-6Al-4V alloys are being used. These materials, with excellent weight-to-strength ratios, are widely used for structural applications in aircraft manufacturing. To date, several studies have been published showing that the use of metalworking fluids (MWFs), special tool geometries, or advanced machining techniques is required to ensure a surface quality that meets aerospace component standards. Conventional MWFs pose a number of environmental and worker health hazards and also degrade the mechanical properties of CFRPs due to water absorption in the composite. Therefore, a transition to more environmentally friendly cooling/lubrication techniques that prevent moisture problems in the composite is needed. This research shows that lubricated LCO₂ is a viable option to improve the quality of drilled CFRP and titanium aerospace components compared to dry machining, while maintaining clean work areas. The results show that the best combination of tool geometry and cooling conditions for machining both materials is drilling with Brad point drills and lubricated LCO₂. Drilling under these conditions resulted in a 90 % improvement in fiber pull-out volume compared to dry machined CFRP holes. In addition, a 33 % reduction in burr height and a 15 % improvement in surface roughness were observed compared to dry drilling of titanium.     

Developing a novel radial ultrasonic vibration-assisted grinding device and evaluating its performance in machining PTMCs

Particle-reinforcing titanium matrix composites(PTMCs) exhibit the sharp raising applications in modern industries owing to its extraordinary physical and mechanical properties. However, the poor grindability and unstable grinding processes due to the existence of TiC particles and TiB short fibres inside PTMCs, leading to the sudden grinding burn and low material removal rate.In this work, a novel radial ultrasonic vibration-assisted grinding(RUVAG) device with a special cross structure was dev...     

柔性隔热材料拉伸断裂模式分析

以三种不同陶瓷纤维缝线缝制而得的柔性隔热材料为研究对象,比较了上述材料在300、600 和

900益热处理30 min 后拉伸强度的变化。通过对材料断裂模式的分析,提出纤维表面处理剂的挥发和非晶质

纤维的晶型转变,是导致柔性隔热材料高温拉伸强度降低的主要原因。

     

Micro powder injection molding of boron carbide components with SiC-Al2O3-Y2O3 sintering additives

Sintering additives and micro-powder injection molding offer an effective method to densify boron carbide（B₄C） and make B₄C components with complex shapes. By adjusting the proportion of three kinds of powders（SiC, Al₂O₃ and Y₂O₃）, four kinds of sintering additives were prepared. The feedstock uniformity, debinding behavior, phase composition and microstructure of micro injection molded B₄C components with different sin...     

车铣复合切削加工技术及其应用研究进展

综述了车铣复合切削过程中的运动学原理、刀具磨损、切屑形貌、切削力和表面完整性方面的最新研究进展；阐述了车铣复合在航空零部件和轴类零件加工中的应用；展望了车铣复合切削加工的研究方向。     

微织构刀具对钛合金切屑形成影响的仿真研究

针对微织构刀具对钛合金Ti6Al4V切屑形成以及微槽二次切削机理分析的不足，通过建立热-力耦合仿真模型对比研究不同微织构刀具、微织构几何尺寸以及切削速度对切屑形成的影响规律。数值仿真结果表明：微织构刀具更有利于断屑，二次切削作用使切屑的弯曲半径变大，微织构可以减小刀屑之间实际接触面积，降低切削温度。增大微织构宽度可以增强微槽的二次切削作用，利于断屑，但应注意其对刀具强度的削弱作用，而增大相邻微槽间距则会出现相反的二次切削作用机制。提高切削速度对各刀具均有利于断屑，弧形微织构刀具的降温效果最好，V形微织构刀具次之，矩形微织构刀具降温效果最差。研究结果对进一步理解微织构刀具对钛合金切屑的二次切削作用机理提供一定参考。