EFFECT OF HEAT TREATMENT ON INTERMEDIATE TEMPERATURE STRESS RUPTURE PROPERTIES OF ALLOY K403

ＥＦＦＥＣＴＯＦＨＥＡＴＴＲＥＡＴＭＥＮＴＯＮＩＮＴＥＲＭＥＤＩＡＴＥＴＥＭＰＥＲＡＴＵＲＥＳＴＲＥＳＳＲＵＰＴＵＲＥＰＲＯＰＥＲＴＩＥＳＯＦＡＬＬＯＹＫ４０３ＺｈｅｎｇＹｕｎｒｏｎｇ，ＬｉＳｈｕｙｕａｎ，ＭａＳｈｕｗｅｉ（ＢｅｉｊｉｎｇＩｎｓｔｉｔ...     

连续变形带斜缠防热层技术研究

介绍了一种用连续变形带来斜缠制造防热层的新技术。通过对工艺和材料性能等多方面的对比试验,结果表明用连续变形带材料,斜缠防热层的制造工艺性得到了很大的改善,缠绕件较为密实,布层排列非常规整,防热层表面无布层扭曲和皱折等缺陷,非常有利于控制防热层的滚转特性,而且材料的力学等性能也有很大程度的提高。由于连续变形带本身具有很强的可设计性,因此本技术有着很大的发展潜力和应用前景。     

应用基于FEM的预成形最优化方法提高锻件变形均匀性

锻件变形分布不均匀将导致锻件各部位的组织和性能产生很大差异。应用基于正向有限元数值模拟和最优化方法进行坯料预成形设计的新方法,可显著提高锻件各部位的变形均匀性。首先介绍了以提高锻件变形分布均匀性为目的的坯料预成形最优化方法的基本原理,并针对典型的IN718合金涡轮盘锻件进行了坯料预成形设计。给出了预成形坯料与普通圆柱坯料的对比结果,并进行了相应的试验验证。结果表明,应用这种方法对IN718合金涡轮盘锻件进行坯料预成形设计,可使盘锻件各部位变形均匀性明显改善。     

Aeroacoustic and aerodynamic optimization of propeller blades

It is of great significance to develop a high-efficiency and low-noise propeller optimization method for new-generation propeller aircraft design. Coupled with free form deformation method, dynamic mesh interpolation technology, optimization algorithm, surrogate model, aerodynamic calculation and aeroacoustic prediction model module, the integrated aerodynamic and aeroacoustic design method of propeller is built. The optimization design for the six-blade propeller is carried out. The non-reduction in efficiency, thrust coefficient and the minimum of aerodynamic noise is treated as the optimization design objective. The spatial vorticity distribution of the propeller before and after the design is also analyzed by using unsteady computational fluid dynamics method. The results show that the optimized propeller can effectively reduce the aerodynamic noise level. The maximum total sound pressure level can be reduced by 5 dB without reducing its aerodynamic performance. The developed method has good application potential in low-noise optimization design of propeller and other rotating machinery.     

Study of seasonal and long-term vertical deformation in Nepal based on GPS and GRACE observations

Lithospheric deformation signal can be detected by combining data from continuous global positioning system (CGPS) and satellite observations from the Gravity Recovery and Climate Experiment (GRACE). In this paper, we use 2.5- to 19-year-long time series from 35 CGPS stations to estimate vertical deformation rates in Nepal, which is located in the southern side of the Himalaya. GPS results were compared with GRACE observations. Principal component analysis was conducted to decompose the time series into three-dimensional principal components (PCs) and spatial eigenvectors. The top three high-order PCs were calculated to correct common mode errors. Both GPS and GRACE observations showed significant seasonal variations. The observed seasonal GPS vertical variations are in good agreement with those from the GRACE-derived results, particularly for changes in surface pressure, non-tidal oceanic mass loading, and hydrologic loading. The GPS-observed rates of vertical deformation obtained for the region suggest both tectonic impact and mass decrease. The rates of vertical crustal deformation were estimated by removing the GRACE-derived hydrological vertical rates from the GPS measurements. Most of the sites located in the southern part of the Main Himalayan Thrust subsided, whereas the northern part mostly showed an uplift. These results may contribute to the understanding of secular vertical crustal deformation in Nepal.     

关于圆轴含有弯弯组合的合成弯矩图形状的讨论

本文结合弯弯扭组合变形的例题，利用相关数学知识，证明了圆轴含有弯弯组合的合成弯矩图如果出现曲线，则该曲线必是(上)凹的。     

一种地下壳体结构内力和变形的简化计算

对锚喷与金属支架联合支护结构的内力和变形 ,本文根据壳体理论提出了一种简化力学模型 ,建立起它的微分方程并推导出简化计算公式。同时 ,结合工程实例对这种联合支护结构的内力和变形特点进行了分析 ,讨论了它的危险截面位置和强度设计的控制因素 ,为其结构设计提供理论基础     

耦合六自由度运动弹性飞机阵风响应数值模拟

耦合飞机刚体六自由度运动,考虑飞机结构气动弹性变形,基于全湍流Navier—Stokes方程流场数值模拟方法．建立了离散阵风作用下弹性飞行器气动载荷与飞行姿态响应的数值模拟技术。其中模态空间中结构动力学方程以及六自由度运动方程分别采用四阶R—K进行时间推进求解,采用RadialBasicFunction（RBF）技术进行气动／结构数据耦合。对应飞机姿态以及弹性变形采用RBF与TFI组合模式的动网格方法进行网格更新;以飞翼布局弹性飞机为数值研究对象,研究了离散阵风作用下飞行器的气动载荷响应以及飞行姿态的变化,对比分析了刚性飞行器与弹性飞行器对离散阵风响应的区别,为进一步系统地分析真实飞机飞行品质提供数值平台。     

推进剂贮箱锥柱形金属膜片的翻转特性研究

基于MSC.Marc非线性有限元软件,对推进剂贮箱锥柱形金属膜片的变形进行仿真研究。模拟了膜片的翻转变形过程,分析了膜片翻转变形规律和失效因素,提出了膜片有效稳定翻转的条件。     

人体变形中局部坐标系旋转失真问题

分析了人体变形中选取3个基轴构建坐标系所存在的缺陷,提出了一种位置-四元数的方法,解决了曲线骨架驱动的旋转失真现象.采用四元数球面线形插值和B样条四元数插值的方法构建人体变形中曲线骨架的局部坐标系,采用位置-四元数-缩放的方式代替传统的转化矩阵,通过人体表面顶点在该坐标系下的绑定,实现人体皮肤、肌肉的变形.试验结果显示:该方法有效地消除了局部坐标系的旋转失真现象,适用限制少,易于实现.