TA15钛合金焊接温度场的仿真模拟分析

薄板钛合金结构在焊接生产中得到了广泛的应用。焊接过程的传热问题十分复杂,焊接过程中的温度分布对于焊接变形有着重要的作用。针对平板TA15钛合金对接接头,对焊接温度场进行了仿真模拟计算,得出了焊接热循环曲线,并进行了试验验证。经过测量比对,焊接热循环曲线变化趋势与模拟所得结果大体一致,说明了模拟计算的正确性。     

基于C/S的飞机钣金成形数据库系统的研究与开发

根据航空工业飞机生产、型号预研、钣金工艺手册、工艺试验等大量数据信息,以Oracle作为后台的数据库管理系统,采用PowerBuilder8.0作为前台的开发工具,研究开发了一套基于C／S,集中了板材性能、成形工艺、机床设备、工装、模具等数据资料的飞机钣金成形数据库系统。     

High-Latitude Particle Precipitation and its Relationship to Magnetospheric Source Regions

Two central issues in magnetospheric research are understanding the mapping of the low-altitude ionosphere to the distant regions of the magnetsphere, and understanding the relationship between the small-scale features detected in the various regions of the ionosphere and the global properties of the magnetosphere. The high-latitude ionosphere, through its magnetic connection to the outer magnetosphere, provides an important view of magnetospheric boundaries and the physical processes occurring there. All physical manifestations of this magnetic connectivity (waves, particle precipitation, etc.), however, have non-zero propagation times during which they are convected by the large-scale magnetospheric electric field, with phenomena undergoing different convection distances depending on their propagation times. Identification of the ionospheric signatures of magnetospheric regions and phenomena, therefore, can be difficult. Considerable progress has recently been made in identifying these convection signatures in data from low- and high-altitude satellites. This work has allowed us to learn much about issues such as: the rates of magnetic reconnection, both at the dayside magnetopause and in the magnetotail; particle transport across the open magnetopause; and particle acceleration at the magnetopause and the magnetotail current sheets.     

ISEE Ion Composition Data with Implications for Solar Wind Entry into Earth's Magnetotail

Energetic (0.1-16 keV/e) ion data from a plasma composition experiment on the ISEE-1 spacecraft show that Earth's plasma sheet (inside of 23 RE) always has a large population of H+ and He++ ions, the two principal ionic components of the solar wind. This population is the largest, in terms of both number density and spatial thickness, during extended periods of northward interplanetary magnetic field (IMF) and is then also the most "solar wind-like" in the sense that the He++/H+ density ratio is at its peak (about 3% on average in 1978 and 79) and the H+ and He++ have mean (thermal) energies that are in the ratio of about 1:4 and barely exceed the typical bulk flow energy in the solar wind. During geomagnetically active times, associated with southward turnings of the IMF, the H+ and He++ are heated in the central plasma sheet, and reduced in density. Even when the IMF is southward, these ions can be found with lower solar wind-like energies closer to the tail lobes, at least during plasma sheet thinning in the early phase of substorms, when they are often seen to flow tailward, approximately along the magnetic field, at a slow to moderate speed (of order 100 km s-1 or less). These tailward flows, combined with the large density and generally solar wind-like energies of plasma sheet H+ and He++ ions during times of northward IMF, are interpreted to mean that the solar wind enters along the tail flanks, in a region between the lobes and the central plasma sheet, propelled inward by ExB drift associated with the electric fringe field of the low latitude magnetopause boundary layer (LLBL). In order to complete this scenario, it is argued that the rapid (of order 1000 km s-1) earthward ion flows (mostly H+ ions), also along the magnetic field, that are more typically the precursors of plasma sheet "recovery" during substorm expansion, are not proof of solar wind entry in the distant tail, but may instead be a time-of-flight effect associated with plasma sheet redistribution in a dipolarizing magnetic field.     

飞机钣金成形信息化现状与关键技术解决途径

钣金成形是飞机制造的关键制造技术之一,钣金成形信息化则是构建先进钣金制造技术的核心所在.分析了钣金成形信息化的内涵,综述了国内外研究现状,提出了航空钣金成形信息化关键技术研究与工程应用的思路,面向工艺过程定义工程模型,驱动全局的工艺过程规划和各个局部工艺过程的参数设计、工装设计、数控编程,建立起全数字量定义、传递与控制模式;对源头各异的钣金成形工艺知识建库和集成使用,支撑工艺过程、加工参数、模具等生产数据的定义,建立起知识的数字化表达、管理和使用模式,从而实现钣金件高效、高质量的制造.     

航空钣金件数字化集成制造系统构建与应用

钣金件数字化制造是航空产品制造数字化的基本组成部分.为满足现代航空产品研制对钣金件制造能力的需求,实现航空钣金件从传统制造模式向数字化制造模式转变,以工艺数据库为核心,数字化技术为手段,基于知识的设计方法为辅助工具,构建了以制造模型定义和工艺数据库为基础的钣金件数字化制造方法与集成制造技术体系,建立了钣金件数字化制造系统,适应了航空产品数字化制造技术的发展要求.     

TB5钛合金薄板微观组织与弯曲性能关系研究

TB5钛合金板材具有优良的冷成形性能,适于成形中等复杂的航空航天用板材零件,但存在板材定形性差、成形后回弹大等问题。本文以TB5钛合金板材的冷成形为背景,探讨了TB5钛合金板材组织在弯曲变形过程中的变形行为及其微结构和成形性能的演变规律。结果表明,随着板材弯曲角度的增大或弯曲半径的减小,板材弯曲回弹角与中心变形处晶粒面积和晶粒横纵比正相关;板材中心变形处硬度和中心变形处晶粒面积正相关,与中心变形处晶粒横纵比负相关。     

化学铣切对6A02薄铝板性能的影响

6A02铝合金薄板在直升机上应用较广泛,有时需进行化铣.通过采用尺寸测量、拉伸性能检测、金相分析等手段,研究了化铣对6A02铝合金薄板厚度、表面质量、力学性能和显微组织影响.结果表明,化铣可将薄板厚度铣削变薄;溶液中的Na2S与三乙醇胺共同作用,可降低合金元素与Al形成的电偶腐蚀作用,使薄板表面质量改善;合金析出相的电...