Meter-Scale Thin-Walled Structure with Lattice Infill for Fuel Tank Supporting Component of Satellite:Multiscale Design and Experimental Verification

Lightweight thin-walled structures with lattice infill are widely desired in satellite for their high stiffness-to-weight ratio and superior buckling strength resulting fromthe sandwich effect.Such structures can be fabricated bymetallic additive manufacturing technique,such as selective laser melting(SLM).However,the maximum dimensions of actual structures are usually in a sub-meter scale,which results in restrictions on their appliance in aerospace and other fields.In this work,a meter-scale thin-walled structure with lattice infill is designed for the fuel tank supporting component of the satellite by integrating a self-supporting lattice into the thickness optimization of the thin-wall.The designed structure is fabricated by SLM of AlSi10Mg and cold metal transfer welding technique.Quasi-static mechanical tests and vibration tests are both conducted to verify the mechanical strength of the designed large-scale lattice thin-walled structure.The experimental results indicate that themeter-scale thin-walled structure with lattice infill could meet the dimension and lightweight requirements of most spacecrafts.

VIBRATION IN HIGH-SPEED MILLING OF THIN-WALLED COMPONENTS

To investigate the vibration principle in machining thin-walled components, a dynamic model for end milling of flexible structures is built based on considering the variations in the dynamic chip thickness and the differences between up-milling and down-milling. Two milling experiments verify the model. Experimental results show that the model can predict the milling force and displacements simultaneously in the dynamic milling process.

Fundamentals and Processes of Fluid Pressure Forming Technology for Complex Thin-Walled Components

A new generation of fluid pressure forming technology has been developed for the three typical structures of tubes,sheets,and shells,and hard-to-deform material components that are urgently needed for aerospace,aircraft,automobile,and high-speed train industries.in this paper,an over all review is introduced on the state of the art in fundamentals and processes for lower-pressure hydroforming of tubular components,double-sided pressure hydroforming of sheet components,die-less hydroforming of ellipsoidai shells,and dual hardening hot medium forming af hard-to-deform materiais Particular attention is paid to deformation behavior,stress state adjustment,defect prevention,and typical applications.In addition,future development directions of fluid pressure forming technology are discussed,including hyper lower-loading forming for ultra-large non-uniform components,precision for ming for intermetallic compound and high-entropy alloy components,intelligent process and equipment,and precise finite element simulation of inhomogeneous and strong anisotropic thin shells.

Topological Optimization Method for Aeronautical Thin-Walled Component Fixture Locating Layout

Fixture locating layout has a direct and influential impact on aeronautical thin-walled component(ATWC)manufacturing quality.The purpose is to develop a topological optimization method for ATWC fixture locating layout to minimize the manufacturing deformation.Firstly,a topological optimization model that takes the stiffness of ATWC as the objective function and the volume of the locating structure as the constraint is established.Secondly,ATWC and the locating structure are regarded as an integrated entity,and the variable-density method based topological optimization approach is adopted for the optimization of the locating structure using ABAQUS topology optimization module(ATOM).Thirdly,through a subsequent model reconstruction referring to the obtained topological structure,the optimal fixture locating layout is achieved.Finally,a case study is conducted to verify the proposed method and the comparison results with firefly algorithm(FA)coupled with finite element analysis(FEA)indicate that the number and positions of the locators for ATWC can be optimized simultaneously and successfully by the proposed topological optimization model.

High-efficiency forming processes for complex thin-walled titanium alloys components: state-of-the-art and perspectives

Complex thin-walled titanium alloy components play a key role in the aircraft,aerospace and marine industries,offering the advantages of reduced weight and increased thermal resistance.The geometrical complexity,dimensional accuracy and in-service properties are essential to fulfill the high-performance standards required in new transportation systems,which brings new challenges to titanium alloy forming technologies.Traditional forming processes,such as superplastic forming or hot pressing,cannot meet all demands of modern applications due to their limited properties,low productivity and high cost.This has encouraged industry and research groups to develop novel high-efficiency forming processes.Hot gas pressure forming and hot stamping-quenching technologies have been developed for the manufacture of tubular and panel components,and are believed to be the cut-edge processes guaranteeing dimensional accuracy,microstructure and mechanical properties.This article intends to provide a critical review of high-efficiency titanium alloy forming processes,concentrating on latest investigations of controlling dimensional accuracy,microstructure and properties.The advantages and limitations of individual forming process are comprehensively analyzed,through which,future research trends of high-efficiency forming are identified including trends in process integration,processing window design,full cycle and multi-objective optimization.This review aims to provide a guide for researchers and process designers on the manufacture of thin-walled titanium alloy components whilst achieving high dimensional accuracy and satisfying performance properties with high efficiency and low cost.

Sheet Bulk Forming of Thin-Walled Components with External Gearing through Upsetting Using Controllable Deformation Zone Method

Sheet-bulk metal forming(SBMF)is a promising process for manufacturing complex sheet components with functional elements.In this study,the entire forming process for a typical thin-walled component with external gearing is investigated,including sheet forming and bulk forming processes.Deep drawn cups are prepared during sheet forming;subsequently,upsetting is performed on the sidewall to form external gearing.The upsetting method performed is known as upsetting with a controllable deformation zone(U-CDZ).Compared with the conventional upsetting method,a floating counter punch with a counter force is used in the U-CDZ method such that the forming mechanism is changed into the accumulation of the deformation zone instead of deformation throughout the entire sidewall.The effects of the counter force and material flow are investigated to understand the mechanism.The forming quality,i.e.,the formfilling and effective strain distribution,improved,whereas a high forming load is avoided.In addition,a punch with a lock bead is used to prevent folding at the inner corner during the experiment.

Vibrations in High Speed Milling of Thin-walled Components

Thin-walled structures have been widely used in the aerospace industry.The dynamic interaction between the milling cutter and thin-walled workpiece can easily lead to vibration.This paper investigates the vibration caused during milling the thin-walled workpiece on the NC machining center,presents a theoretical milling vibration model of thin-walled beam.The model was verified by using milling experiments and numerical simulations.Some valuable conclusions are derived,this will be references to scientific research and guides to the vibration-free milling of thin-walled structures at different cutting speeds.

Recent Developments on Damage and Fracture of Thin-Walled Complex Components Produced by Spinning

The spinning technique has been widely used in the manufacture of aerospace thin-walled axisymmetric components because of its excellent formability. Damage and fracture,as the important defects that often occur and must be avoided in the forming and service stages of components,have attracted much attention of researchers. In this paper,the fracture behavior and laws of spinning components such as conical parts,tubular parts,and components with inner ribs are summarized,the typical coupled and uncoupled ductile fracture models are introduced,and their applications in spinning are analyzed. Meanwhile,the recent developments on the modified ductile fracture model in analyzing damage and fracture mechanisms of spinning are emphatically introduced. The results could provide guidance for the selection and establishment of appropriate ductile fracture models in the finite element simulation for the accurate prediction and analysis of fracture moment,location,form,damage mechanism,and evolution law,and help the development of precision spinning techniques for high-performance thin-walled complex components.

ON THE CALCULATION OF STRESS INTENSITY FACTOR K FOR FRAME COMPONENTS

The stress intensity factor K in the tip of crack which is in the corner of the frame component has been calculated indirectly by means of numeric calculation of J Integral. Some laws and relationships among the stress intensity factor K, the applied load

Collaborative manufacturing technologies of structure shape and surface integrity for complex thin-walled components of aero-engine:Status,challenge and tendency

Presently,the service performance of new-generation high-tech equipment is directly affected by the manufacturing quality of complex thin-walled components.A high-efficiency and quality manufacturing of these complex thin-walled components creates a bottleneck that needs to be solved urgently in machinery manufacturing.To address this problem,the collaborative manufacturing of structure shape and surface integrity has emerged as a new process that can shorten processing cycles,improve machining qualities,and reduce costs.This paper summarises the research status on the material removal mechanism,precision control of structure shape,machined surface integrity control and intelligent process control technology of complex thin-walled components.Numerous solutions and technical approaches are then put forward to solve the critical problems in the high-performance manufacturing of complex thin-wall components.The development status,challenge and tendency of collaborative manufacturing technologies in the high-efficiency and quality manufacturing of complex thin-wall components is also discussed.

Effect of assisted transverse magnetic field on distortion behavior of thin-walled components in WEDM process

Machining performance of thin-walled components made by aeronautical difficult-toprocess materials is a significant issue in the aviation manufacturing industry.Although wire electric discharge machining-low speed(WEDM-LS)is one of typical non-contact machining processes without macro cutting force,which does well in removing hardness and brittleness materials via pulsed discharge at high temperature,but few researchers have studied the thermal distortion behavior leading to a considerable geometric error in the WEDM-LS of thin-walled components.In this paper,a transverse magnetic field assisted method is applied for affecting the uniformity of discharge point distribution so as to reduce the distortion in WEDM-LS processing thin-wall component.First,the generation mechanism of this new distortion behavior and the impact mechanism of transverse magnetic field(TMF)on distortion are demonstrated by theoretical analysis.In order to further figure out the distortion behavior in the TMF-WEDM process,a new thermophysical model considering the discharge point distribution is established to simulate temperature field,residual stress field and distortion profiles.Then a large number of Taguchi experiments are carried out to investigate the influences of process parameters including pulse discharge energy(pulse on time,pulse off time,and current)and magnetic field strength on distortion in WEDM-LS.To comparatively analyze simulated and experimental results,the accuracy of established thermophysical model is verified within a relative error of 18.38%in distortion.Moreover,it can be revealed that transverse magnetic field contribute to significantly improve the longitudinal distribution uniformity with maximum increase of 12.32%at magnetic field strength:0.15 T,leading to significant reductions of 32.77%in distortion and 22.68%in recast layer.Eventually,we also presented the variation of residual stress and recast layer along thickness direction under different distortion behavior,which are in good agreement with that of distortion behavior.

考虑填充墙的RC框架结构性能指标限值确定方法

填充墙钢筋混凝土(RC)框架结构是我国应用最为广泛的结构形式之一,而我国规范中给出的此类结构性能指标限值并未充分考虑填充墙对整体结构破坏状态的影响。遵循我国规范中对结构破坏状态的定义原则,提出基于构件破坏率的填充墙RC框架结构性能指标限值确定方法,为此类结构破坏状态与工程需求参数对应关系的研究提供新的思路。以典型结构为例建立数值分析模型,采用该文方法计算考虑填充墙的RC框架结构性能指标限值,并与不考虑填充墙的“纯框架”限值进行了对比分析。相较于“纯框架指标”,该文指标完好、轻微破坏、中等破坏和严重破坏四个破坏状态的层间位移角上限值均更小,其中,完好状态的上限值为1/832,远小于规范中规定的弹性层间位移角限值1/550,说明判定填充墙RC框架结构的破坏状态时,直接应用规范限值会低估结构的破坏程度。

基于构件性能的SRC框架结构抗震性能评估研究

针对位移抗震性能设计的不足,现行规范采用构件损伤程度补充评估结构的抗震性能,但对于型钢混凝土(steel reinforced concrete,SRC)框架结构,其在各性能水平下的损伤构件比例未有明确规定。在此背景下,提出了SRC框架的构件性能状态与结构性能水准的对应关系,建立了基于构件性能的SRC框架结构抗震性能评估方法。对不同高度和抗震设防烈度的SRC框架结构模型进行增量动力分析(incremental dynamic analysis,IDA),明确了结构的层间位移角和构件损伤分布,通过统计多条地震波下结构不同极限状态的构件破坏比例,建立用于体型规则SRC框架结构抗震评估的构件性能指标,并进一步采用地震易损性分析对结构抗震性能进行了评估。

6.4级漾濞地震某RC框架及其非结构部件震害分析

2021年云南漾濞6.4级地震造成了较大范围的建筑破坏,在漾濞县城记录到的地震加速峰值(PGA)高达720.2 gal。在强震作用下,大量土木结构的民居发生了破坏,而约束砌体和钢筋混凝土(RC)结构的震害则相对较轻。现场震害调查发现,部分框架结构的震害明显重于同一区域的其他同类型结构,呈现明显、多样的非结构部件破坏特征。因此,该文对某震害较重的框架进行详细调查,分类分析结构及其非结构部件地震破坏细节;依据图纸及现场考察信息建立精细有限元分析模型,对此次地震的地震动破坏力特征以及该框架结构及其非结构部件的地震破坏机理进行了量化分析。分析结果表明:带填充墙框架仿真模型的分析结果与实际震害现象更接近;框架结构局部大空间、框架底部的约束形式和填充墙的布置形式的综合作用导致结构产生局部过大变形与各类非结构部件的严重破坏。在考虑填充墙对框架结构的作用效应后,结构的不规则性大幅增加,导致结构薄弱层的最大层间位移角相较纯框架模型增加127%,并且明显加剧非结构部件的震害。该文对该建筑震害现象的详细调查与仿真分析,可为结构抗震设计与应急救援决策提供参考。

考虑约束作用的混凝土柱耐火试验加载方式研究

为找到一种在构件耐火试验中能有效考虑整体结构对受火构件约束作用的加载方式,建立了2层2跨的钢筋混凝土框架和受火单柱的有限元模型,对比分析荷载比为0.2、0.4和0.6时,恒载、变位移加载、变力加载和交互加载方式下受火单柱与整体结构的内力、变形和耐火极限的差异。研究结果表明:恒载单柱不能准确反映整体结构受火柱的变形、轴力和耐火极限;变位移加载和变力加载在荷载比为0.2时能较好考虑整体结构中的约束作用,在荷载比为0.4和0.6时误差增大也不能准确反映整体结构的抗火性能;交互加载的相对误差随荷载比增大而增大,且最大误差小于20%。恒载、变位移加载、变力加载和交互加载中,交互加载可以较好考虑整体结构中的约束作用,近似达到整体结构试验的效果。

不同架式对‘南太湖特早’葡萄果实香气成分及品质的影响

为探索不同栽培架式对葡萄果实香气成分和品质的影响,以温棚种植的倾斜棚架栽培与常规“厂”字形栽培(CK)的6年生‘南太湖特早’葡萄为试验材料,对倾斜棚架不同结果部位(前部,C1;中部,C2;后部,C3)的果实性状、挥发性香气物质进行评价,利用Flavour Spec■气相离子迁移谱联用仪(gas chromatography-ion mobility spectrometre,GC-IMS)对‘南太湖特早’葡萄进行香气成分分析,测定树体和浆果的相关理化指标。结果表明,‘南太湖特早’葡萄采用倾斜棚架栽培,与棚架其他结果部位及CK相比,从C1部位开始结果枝基粗依次增加,C1浆果的糖酸比适宜,花色苷含量最高,为438.69 mg·L^(-1),比C2、C3和CK分别增加21.4%、108.1%和8.9%。棚架各结果部位的酯类、醇类和醛类香气总量均高于CK,酯类香气物质C1最高,为4944.24μg·L^(-1),比C2、C3和CK分别增加1.5%、21.9%和37.9%;醇类香气物质总量C1最高,为15930.07μg·L^(-1),比C2、C3和CK分别增加了5.8%、7.7%和1.3%,但各结果部位与CK差异均不显著(P>0.05);C1结果部位的醛类总量最高,为8865.41μg·L^(-1),比C2、C3和CK分别增加1.5%、6.6%和17.2%。结果部位C1处的挥发性香气物质丁酸甲酯、(E)-2-己烯醇和α-蒎烯的香气活性值最大,可作为葡萄主要的呈香物质,C1、C3和CK浆果中的挥发性香气种类含量较多,香气更加突出;C1在甜香味上表现更加典型、浓郁。不同架式不同结果部位的‘南太湖特早’葡萄表现出不同的香气特征和风味,研究结果为‘南太湖特早’葡萄的栽培架式选择和风味机理的形成提供理论参考。

一种快速正交分量构造的单相并网逆变器控制

针对单相LCL型并网逆变器控制系统存在网侧电流跟踪性能差的问题,这里提出基于解耦双同步参考坐标系(DDSRF)的单相网侧电流正交分量构造方法,得到直流形式的网侧正负序电流d,q轴分量,并在正负序d,q坐标系下用比例积分(PI)控制器构建电流控制环路,以实现网侧电流无差跟踪。首先介绍所提DDSRF快速构造网侧电流正交分量的工作原理。其次,分析各电流控制环路PI控制器参数的设计方法。最后,在5 kW单相LCL型并网逆变器硬件平台进行实验验证,实验结果证明了所提控制系统的正确性。

装配式混凝土结构构件节点相关技术研究进展

随着我国社会经济水平不断进步,以机械设备和人工现场作业为主的传统建设工程生产施工模式已经逐渐不能适应当前的形势发展.围绕着建筑工业化的理论研究和技术开发一直在相关领域保持着较大的热度.装配式混凝土结构正是与之相关的重要研究对象,而其中大量的研究内容集中在预制构件的连接节点构造上.研究了国内外关于装配式混凝土结构构件节点相关技术的研究进展,并对其主要研究内容和关键结论进行了介绍.

装配整体式混凝土框架结构设计方法研究

装配整体式混凝土框架结构采用“等同现浇”的设计方法,结构体系成熟。在对该结构体系设计方法进行系统、全面归纳与总结的基础上,对其中的一些细部连接设计创新性地给出计算方法与过程,为该结构体系的应用与推广提供了一定的理论支撑。

拉普拉斯金字塔变换算法的光学元件表面疵病检测

为了解决由于光学元件表面疵病造成光的散射、反射或透射现象,影响光学系统成像质量的问题,设计了基于多光谱技术的光学元件表面疵病检测方法。采集光学元件表面疵病的多光谱图像。采用拉普拉斯金字塔变换算法融合光学元件表面疵病的多光谱图像,利用帧差法对两幅光学元件多光谱图像相减处理,获取光学元件表面疵病的二值图像特征,标记光学元件多光谱图像融合结果的连通区域,利用图像连通区域的长宽比等参数,检测光学元件表面疵病的种类、数量、大小。实验结果表明,该方法有效检测光学元件的麻点、划痕、破点等不同类型的表面疵病,表面疵病尺寸检测精度最高为98.15%。