飞行器机身结构耐撞性分析与设计

耐撞性不仅是飞行器设计中的重要问题,而且还是其取得适航证的必要条件。该文对美国、欧盟和日本等在耐撞性研究方面的研究进行了总结,阐述了耐撞性设计中采用的数值模拟和试验研究方法及其主要问题。主要针对各种飞行器结构耐撞性设计方法进行介绍,对比了轻型固定翼飞机、直升机和大中型民用飞机的耐撞性设计特点。能量吸收结构是耐撞性设计的关键问题之一,对提高飞行器机身能量吸收能力的机身底部结构、机身加强框和客舱地板撑杆结构等设计方法进行详细介绍,总结了飞行器耐撞性可靠性分析和优化设计方法。最后对飞行器结构耐撞性设计的发展作了展望。     

机械冲击耐撞性与稳健设计

碰撞冲击是机电产品损坏失效的常见原因,轻则造成产品外形丧失美观,重则造成产品内在功能失效,甚至机毁人亡,因而机械产品的耐撞性受到日益广泛的关注。本文从产品跌落冲击和运载工具碰撞两个领域论述了机械系统碰撞动力学和耐撞性设计研究的发展、两领域耐撞性研究的阶段性和特点,分析了机械冲击耐撞性中的冲击参数到性能参数传递过程中的不确定性,进而探讨了机械系统产品耐撞性稳健设计优化框架。     

飞机风挡夹层结构耐撞性数值分析

用LS-DYNA3D软件,建立了由钢化玻璃和PU、PVB塑料薄膜组成的风挡夹层结构鸟撞数值模型。鸟体采用ALE格式和与应变率相关的随动硬化材料模型,夹层结构用Lagrange格式和双线性材料模型,对11种风挡夹层结构进行了数值计算,分析了撞击过程的损伤和应力,讨论了夹层结构耐撞性的评估方法,为风挡夹层结构设计提供理论依据。     

PBM算法在近场爆炸数值模拟中的运用研究

为探究爆炸粒子算法(PBM)在近场爆炸问题中的适用性,分别采用PBM法及任意拉格朗日-欧拉算法(ALE&S-ALE),开展AL-6XN不锈钢板近场爆炸的仿真模拟.结合T B?rvik的试验结果,对比了ALE、S-ALE和PBM方法的计算精确度和运算效率;采用PBM算法对不同爆心距的钢板近场爆炸工况进行仿真计算,分析了粒...     

某焦煤车间钢梁的耐撞性分析

利用非线性有限元动力分析软件ANSYS/LS-DYNA研究了某焦煤车间制动梁的耐撞性问题,通过计算机数值模拟计算,分析了装煤钢方斗对制动梁的影响。结果表明:装煤钢方斗的作用为类矩形脉冲荷载;梁的下翼缘的应力很大,被撞区和支座处的腹板和加劲肋应力也很大,这表明可以适当加大下翼缘和腹板的厚度和减小上翼缘的厚度。     

A型不锈钢地铁车体耐撞性研究

轨道车辆车体基本性能的研究需要考虑多方面的因素,车体耐碰撞性是重要指标之一。以A型不锈钢地铁车体为研究对象,基于LS-DYNA碰撞仿真平台,分析了车辆在不同碰撞速度下车体的耐撞性能;然后,采用逼近法,获取了该型地铁车的最大碰撞安全速度,为车体的耐撞性设计提供了理论支撑。     

响应表面法在薄壁构件耐撞性优化设计中的应用研究

汽车结构的耐撞性及碰撞吸能优化是现代汽车工业重要的研究内容。耐撞性的优化涉及材料与结构的众多参数。传统的设计、碰撞仿真及试验往往只能在一定程度上改善结构的碰撞性能而无法达到限定条件下的最优状态。利用国际上近年来新发展起来的一种优化理论方法--响应表面法,结合传统的优化手段以及非线性有限元程序对薄壁构件的耐撞性问题进行了优化研究。耐撞性优化的结果表明,该方法具有较高的精确性和有效性。     

典型薄壁结构抗鸟撞动响应试验及数值模拟研究EI北大核心CSCD

设计满足鸟撞适航条款要求的飞机薄壁结构,必须进行典型薄壁结构抗鸟撞动响应试验及数值模拟研究。对某飞机机头上壁板薄壁结构进行了鸟撞试验,并采用光滑粒子流体动力学-有限元法(smoothed particle hydrodynamics-finite element method,SPH-FEM),基于商用显式有限元分析软件PAM-CRASH,建立了鸟撞上壁板薄壁结构数值计算模型。计算结果表明,上壁板结构损伤模式主要包括蒙皮撕裂和铆钉断裂,计算结果与试验结果良好的一致性验证了该数值计算模型及方法的合理性。在此基础上,建立了鸟撞典型薄壁结构数值计算模型,研究了鸟弹不同撞击角度和速度下典型薄壁结构蒙皮极限厚度值,结果表明,随着撞击速度的增大,蒙皮极限厚度的变化对撞击角度十分敏感。拟合了典型薄壁结构蒙皮极限厚度与鸟弹撞击角度和速度之间的数学关系,为飞机薄壁结构抗鸟撞设计提供技术支撑。     

基于欧拉—拉格朗日方法的复合材料机翼前缘鸟撞模拟

复合材料大面积用于飞机结构后,其鸟撞问题变得更加突出。利用大型通用有限元程序ABAQUS,采用耦合欧拉—拉格朗日方法（CEL）对某型无人机复合材料机翼前缘的鸟撞问题进行模拟,研究了鸟体速度、密度和蒙皮铺层形式等对鸟撞动响应的影响,计算了机翼前缘填充泡沫后的鸟撞损伤,对复合材料蒙皮的鸟撞破坏机理进行了分析,所得结果对工程设计具有参考意义。     

地铁列车双锥内嵌隔板矩形管的耐撞性优化

为设计具有良好耐撞性能的地铁列车吸能结构,将矩形吸能管的一组对称面引入锥度,并在内部嵌入多个隔板.建立该双锥内嵌隔板矩形管和传统矩形管的有限元模型,对两者耐撞性进行对比,通过准静态轴向压缩试验验证有限元分析的准确性.以双锥内嵌隔板矩形管三个部分的厚度为设计变量,进行试验设计并建立代理模型,为最大化比吸能和最小化峰值力,...     

Rigid body water impact-experimental tests and numerical simulations using the SPH method

Statistics show that water impact of an aircraft in emergency is likely to have tragic consequences and therefore new researches on this topic are recommendable. In 2005, the GARTEUR AG15 was established to improve the SPH method for application to helicopter ditching. As a contribution, water impact drop tests using rigid bodies were performed at the Politecnico di Milano LAST Crash Lab to collect data and validate the numerical models. During the tests, impact decelerations were measured and suitably pressure transducers were developed to measure the impact pressures. Numerical simulations were carried out by adopting the SPH method to model the fluid region. A close experimental-numerical correlation was obtained. Findings are reported and guidelines for further investigations are proposed.     

On computing upper and lower bounds on the outputs of linear elasticity problems approximated by the smoothed finite element method

Verification of the computation of local quantities of interest, e.g. the displacements at a point, the stresses in a local area and the stress intensity factors at crack tips, plays an important role in improving the structural design for safety. In this paper, the smoothed finite element method (SFEM) is used for finding upper and lower bounds on the local quantities of interest that are outputs of the displacement field for linear elasticity problems, based on bounds on strain energy in both the primal and dual problems. One important feature of SFEM is that it bounds the strain energy of the structure from above without needing the solutions of different subproblems that are based on elements or patches but only requires the direct finite element computation. Upper and lower bounds on two linear outputs and one quadratic output related with elasticity—the local reaction, the local displacement and the J‐integral—are computed by the proposed method in two different examples. Some issues with SFEM that remain to be resolved are also discussed. Copyright © 2010 John Wiley & Sons, Ltd.     

民用飞机机载电子系统分布式体系架构研究

为了解决机载电子系统处理平台高度综合带来系统资源竞争及深度耦合的问题,将系统综合扩展到前端机电领域,采用分布式综合模块化机载电子系统(DIMA)架构理念,把计算资源分离到与信号源相近的区域,以分离式小机柜取代集中式大机柜,采用高速总线进行分布式机柜互联,重点分析了航电全双工交换式以太网(AFDX网络)、时间触发式以太网(TTE网络)、基于以太网的无源光网络(EPON网络)在DIMA系统中的应用,对比了这3种总线网络技术特点,最后以空客分布式机载电子系统架构为例分析了分布式机载电子系统架构的优势和特点．通过采用DIMA系统架构,解决了机载电子系统处理平台资源竞争和深度耦合问题,同时简化了背板结构,在民用飞机上具有广阔的应用空间．     

An enhanced cell‐based smoothed finite element method for the analysis of Reissner–Mindlin plate bending problems involving distorted mesh

In this work, an enhanced cell‐based smoothed finite element method (FEM) is presented for the Reissner–Mindlin plate bending analysis. The smoothed curvature computed by a boundary integral along the boundaries of smoothing cells in original smoothed FEM is reformulated, and the relationship between the original approach and the present method in curvature smoothing is established. To improve the accuracy of shear strain in a distorted mesh, we span the shear strain space over the adjacent element. This is performed by employing an edge‐based smoothing technique through a simple area‐weighted smoothing procedure on MITC4 assumed shear strain field. A three‐field variational principle is utilized to develop the mixed formulation. The resultant element formulation is further reduced to a displacement‐based formulation via an assumed strain method defined by the edge‐smoothing technique. As the result, a new formulation consisting of smoothed curvature and smoothed shear strain interpolated by the standard transverse displacement/rotation fields and smoothing operators can be shown to improve the solution accuracy in cell‐based smoothed FEM for Reissner–Mindlin plate bending analysis. Several numerical examples are presented to demonstrate the accuracy of the proposed formulation.Copyright © 2013 John Wiley & Sons, Ltd.     

飞机典型薄壁复合材料夹层结构整体屈曲

为了研究飞机机身无筋无框复合材料典型薄壁夹层结构在型号上应用的可行性,本文采用解析方法、有限元方法和试验方法对蜂窝夹层复合材料结构的面内压缩和剪切整体屈曲开展系统研究。基于经典层合板理论和工程解析方法推导蜂窝夹层复合材料的压缩和剪切屈曲载荷随试验件尺寸的变化规律。依据某型飞机机身典型结构分别设计压缩和剪切试验件尺寸大小、边界条件和加载方式。利用有限元商用软件ABAQUS对试验设计建立虚拟试验分析,对比验证解析方法和有限元方法的一致性。最后通过真实试验方法确定解析方法和有限元方法的有效性,并验证典型薄壁夹层结构的承载能力和破坏模式。结果显示,压缩试验结果失效模式与理论预测一致,故3种方法得到的结构整体失稳载荷相近,验证了理论方法的有效性;剪切试验结果发生局部破坏,故试验结果偏低,但有限元方法与解析方法所得结果一致,解析方法相对保守。     

A saturated discrete particle model and characteristic-based SPH method in granular materials

Based on the discrete particle model for solid-phase deformation of granular materials consisting of dry particulate assemblages, a discrete particle–continuum model for modelling the coupled hydro-mechanical behaviour in saturated granular materials is developed. The motion of the interstitial fluid is described by two parallel continuum schemes governed by the averaged incompressible N–S equations and Darcy's law, respectively, where the latter one can be regarded as a degraded case of the former. Owing to the merits in both Lagrangian and mesh-free characters, the characteristic-based smoothed particle hydrodynamics (SPH) method is proposed in this paper for modelling pore fluid flows relative to the deformed solid phase that is modelled as packed assemblages of interacting discrete particles. It is assumed that the formulation is Lagrangian with the co-ordinate system transferring with the movement of the solid particles. The assumed continuous fluid field is discretized into a finite set of Lagrangian (material) points with their number equal to that of solid particles situated in the computational domain. An explicit meshless scheme for granular materials with interstitial water is formulated. Numerical results illustrate the capability and performance of the present model in modelling the fluid–solid interaction and deformation in granular materials saturated with water. Copyright © 2007 John Wiley & Sons, Ltd.     

Experimental and numerical study on the orthogonal and oblique impact on water filled pipes

A 300 mm long piece of copper (ASTM B280) pipe with an outer diameter of 35 mm and 0.7 mm wall thickness was subjected to a rigid steel pipe impact under a drop weight loading configuration where the pipe was simply supported at its ends. Differences in deformation features for a pipe filled with water and an empty pipe were investigated for two configurations namely orthogonal and oblique impact. Compared to orthogonal pipe impact the oblique pipe impact has not been reported in the literature. It is hoped that current work would serve as a first step in this direction. Finite Element Method coupled with Smooth Particle Hydrodynamics (SPH) available in LS-DYNA was used to simulate the empty and water filled pipe impacts under orthogonal and oblique configurations respectively. Fluid structure interaction (FSI) during the water filled pipe impact was successfully modeled using SPH which is a simple method for predicting the short duration FSI events. Experimental results of the effect of varying D/T ratio on the empty and water filled pipes have been reported.     

涡桨飞机机体外表面噪声源计算与实验验证

针对某型涡桨飞机在巡航状态下机体表面的主要噪声源（附面层噪声和螺旋桨噪声）分别进行了计算及结果验证。利用VA-One软件开展了机身表面不同位置处附面层噪声数值计算,同时利用半经验公式进行了螺旋桨近场噪声的计算研究。综合考虑两种噪声源的计算结果,与该型涡桨飞机的机体外表面噪声实测结果进行了对比研究。结果表明,仿真和理论计算相结合的计算结果与实测结果吻合较好,验证了算法的正确性。该算法可应用于涡桨飞机机身外表面噪声载荷及舱内噪声预计。     

Analysis and reduction of quadrature errors in the material point method (MPM)

The material point method (MPM) has demonstrated itself as a computationally effective particle method for solving solid mechanics problems involving large deformations and/or fragmentation of structures, which are sometimes problematic for finite element methods (FEMs). However, similar to most methods that employ mixed Lagrangian (particle) and Eulerian strategies, analysis of the method is not straightforward. The lack of an analysis framework for MPM, as is found in FEMs, makes it challenging to explain anomalies found in its employment and makes it difficult to propose methodology improvements with predictable outcomes. In this paper we present an analysis of the quadrature errors found in the computation of (material) internal force in MPM and use this analysis to direct proposed improvements. In particular, we demonstrate that lack of regularity in the grid functions used for representing the solution to the equations of motion can hamper spatial convergence of the method. We propose the use of a quadratic B‐spline basis for representing solutions on the grid, and we demonstrate computationally and explain theoretically why such a small change can have a significant impact on the reduction in the internal force quadrature error (and corresponding ‘grid crossing error’) often experienced when using MPM. Copyright © 2008 John Wiley & Sons, Ltd.     

Impact analysis of arbitrarily‐shaped bodies using a finite element method and a smoothed particle hydrodynamics method

We propose a new method to obtain contact forces under a non‐smoothed contact problem between arbitrarily‐shaped bodies which are discretized by finite element method. Contact forces are calculated by the specific contact algorithm between two particles of smoothed particle hydrodynamics, which is a meshfree method, and that are applied to each colliding body. This approach has advantages that accurate contact forces can be obtained within an accelerated collision without a jump problem in a discrete time increment. Also, this can be simply applied into any contact problems like a point‐to‐point, a point‐to‐line, and a point‐to‐surface contact for complex shaped and deformable bodies. In order to describe this method, an impulse based method, a unilateral contact method and smoothed particle hydrodynamics method are firstly introduced in this paper. Then, a procedure about the proposed method is handled in great detail. Finally, accuracy of the proposed method is verified by a conservation of momentum through three contact examples. Copyright © 2016 John Wiley & Sons, Ltd.