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微机电系统的国防应用及其制造技术发展述评(下)中国航空信息中心饶勤4微机械制造技术的发展及应用1.微机械制造技术及其应用(1)辅助加工技术包括金刚石微细切削、电火花加工和化学铣削等工艺,这类工艺能以较大的灵活性和较快的速度加工出形状多样的、尺寸在10... 相似文献
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随着水污染与水资源短缺问题的日趋严重,污水减量化与资源化逐渐为人们所重视。兴建的城市污水处理厂及工业废水处理站在一定程度上缓解了水源污染的加剧;以生活污水二级处理出水为原水,对其进行深度处理,回用于工业冷却、道路冲洗、洗车和绿化等,成为缺水城市和地区水资源可持续利用的重要途径。 相似文献
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微机械陀螺是一种新型的陀螺,近年来随着微机电技术的发展,其性能不断得到提高。基于多环谐振微机械陀螺的发展现状,详细评述了多环谐振陀螺的来源以及其由单环到多环的结构发生改变的优点。并基于驻波进动原理,介绍了两种新型的全对称谐振盘陀螺。总结了圆环谐振式微机械陀螺的工艺发展路线,由早期的HARPSS工艺发展到外延多晶硅封装工艺,再到材料性能好的单晶硅热压键合工艺,使得多环谐振陀螺的性能不断得以提升,并分析了其优缺点。最后,展望了未来的高新技术,提出多环谐振陀螺的发展方向。 相似文献
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激光加工小孔工艺及其孔壁再铸层对DZ22高温合金疲劳性能的影响 总被引:2,自引:0,他引:2
介绍了3种激光加工小孔工艺,在疲劳试验基础上分析了激光加工小孔孔壁再铸层及其上微裂纹对DZ22材料疲劳寿命的影响,并比较了3种工艺方法的优劣。 相似文献
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电火花微细孔加工工艺实验研究 总被引:1,自引:0,他引:1
根据电火花微细加工的特点,通过各种工艺实验研究了微能放电参数、电极对材料以及加工液对电火花微细孔加工速度和侧边间隙的影响规律,寻求兼顾加工速度和精度的工艺参数组合。 相似文献
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李晓海%陈贵清%韩杰才%孟松鹤 《宇航材料工艺》2005,35(6):13-16
简要介绍了用于电子束物理气相沉积的设备及其发展,阐述了利用该技术制备微层材料的优点,同时对制备工艺和相应的材料性能作了详细的介绍,并指出使用电子束物理气相沉积技术制备微层材料具有广阔的发展前景。 相似文献
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IntroductionExpensive turbine parts like HPT(HighPressure Turine)blades or vanes are replaced bynew parts in case of damage.For example theburn through of the inner side of a blade or vane(Figure 1)is a frequently appearing damage,which cannot be repaired… 相似文献
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航天器返回地球的气动特性综述 总被引:4,自引:0,他引:4
航天器返回地球的飞行过程中,气动特性是实现将宇宙飞行速度减到落地前速度、保证再入飞行得到有效控制以及再入防热安全可靠的关键因素。针对简单旋成体气动外形、半弹道式再入控制、烧蚀防热类返回航天器,综述了返回地球过程中变化的空气流域特性、航天器周围的气体绕流环境、空气与航天器作用产生的动力学与热效应等。系统地给出了该类航天器的再入气动特性参数与飞行性能的共性规律,包括:气动阻力与再入减速、气动升力与再入轨迹控制、配平攻角与飞行稳定性、气动加热与防热,以及再入过程中不同气动特性航天器、气象条件变化等对再入飞行性能的影响规律。为航天器开展返回飞行过程的跨流域气动性能工程研制提供设计参考。 相似文献
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James C. Leary Richard F. Conde George Dakermanji Carl S. Engelbrecht Carl J. Ercol Karl B. Fielhauer David G. Grant Theodore J. Hartka Tracy A. Hill Stephen E. Jaskulek Mary A. Mirantes Larry E. Mosher Michael V. Paul David F. Persons Elliot H. Rodberg Dipak K. Srinivasan Robin M. Vaughan Samuel R. Wiley 《Space Science Reviews》2007,131(1-4):187-217
The MErcury Surface, Space ENvironment, GEochemistry, and Ranging (MESSENGER) spacecraft was designed and constructed to withstand the harsh environments associated with achieving and operating in Mercury
orbit. The system can be divided into eight subsystems: structures and mechanisms (e.g., the composite core structure, aluminum
launch vehicle adapter, and deployables), propulsion (e.g., the state-of-the-art titanium fuel tanks, thruster modules, and
associated plumbing), thermal (e.g., the ceramic-cloth sunshade, heaters, and radiators), power (e.g., solar arrays, battery,
and controlling electronics), avionics (e.g., the processors, solid-state recorder, and data handling electronics), software
(e.g., processor-supported code that performs commanding, data handling, and spacecraft control), guidance and control (e.g.,
attitude sensors including star cameras and Sun sensors integrated with controllers including reaction wheels), radio frequency
telecommunications (e.g., the spacecraft antenna suites and supporting electronics), and payload (e.g., the science instruments
and supporting processors). This system architecture went through an extensive (nearly four-year) development and testing
effort that provided the team with confidence that all mission goals will be achieved.
Larry E. Mosher passed away during the preparation of this paper. 相似文献
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Snort报文检测及解析机制分析 总被引:2,自引:0,他引:2
Snort是目前最受关注的一个代码开放网络入侵检测系统(NIDS)。报文检测和解析是其最基本也是最重要的部分。本文分析了Snort的系统结构和检测原理及模式,对Snort报文捕获和报文解析的实现进行了分析,提出了Snort存在的缺陷和改进建议。 相似文献
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从理论上分析谐振器的静电制动特性和机械力学特性,给出了活动梳齿的谐振频率和谐振振幅的解析解,提供谐振器结构设计的依据.设计了四种结构形式的谐振器,充分考虑不同静电激励方式对谐振器的影响,合理选取结构参数,有效提高了谐振器抑制侧向失稳和粘附效应的能力.借助有限元软件在考虑硅微加工特性和可行性的基础上对谐振器模态和固有频率的仿真和计算,优化了谐振器结构参数,使工作模态远离其他高阶模态,具有良好的频率特性. 相似文献
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中央维护系统概念及其应用 总被引:3,自引:0,他引:3
二十世纪八十年代以来,国外航空界研制开发了民用直升机的健康与使用状况监控系统(HUMS),并将这一概念引入军机,先后建立了用于军用直升机的联合先进飞机健康与使用状况监控系统(JAHUMS)项目和用于歼击机的故障预测与健康管理(PHM)项目,本文基于当前国外HUMS的发展状况,借鉴JAHUMS和PHM的构想,将HUMS概念引入到民用固定翼飞机中央维护系统(CMS)中,对CMS概念、应用和其关键技术进行了初步探讨。 相似文献
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The Mercury Dual Imaging System on the MESSENGER Spacecraft 总被引:1,自引:0,他引:1
S. Edward Hawkins III John D. Boldt Edward H. Darlington Raymond Espiritu Robert E. Gold Bruce Gotwols Matthew P. Grey Christopher D. Hash John R. Hayes Steven E. Jaskulek Charles J. Kardian Jr. Mary R. Keller Erick R. Malaret Scott L. Murchie Patricia K. Murphy Keith Peacock Louise M. Prockter R. Alan Reiter Mark S. Robinson Edward D. Schaefer Richard G. Shelton Raymond E. Sterner II Howard W. Taylor Thomas R. Watters Bruce D. Williams 《Space Science Reviews》2007,131(1-4):247-338
The Mercury Dual Imaging System (MDIS) on the MESSENGER spacecraft will provide critical measurements tracing Mercury’s origin
and evolution. MDIS consists of a monochrome narrow-angle camera (NAC) and a multispectral wide-angle camera (WAC). The NAC
is a 1.5° field-of-view (FOV) off-axis reflector, coaligned with the WAC, a four-element refractor with a 10.5° FOV and 12-color
filter wheel. The focal plane electronics of each camera are identical and use a 1,024×1,024 Atmel (Thomson) TH7888A charge-coupled
device detector. Only one camera operates at a time, allowing them to share a common set of control electronics. The NAC and
the WAC are mounted on a pivoting platform that provides a 90° field-of-regard, extending 40° sunward and 50° anti-sunward
from the spacecraft +Z-axis—the boresight direction of most of MESSENGER’s instruments. Onboard data compression provides capabilities for pixel
binning, remapping of 12-bit data into 8 bits, and lossless or lossy compression. MDIS will acquire four main data sets at
Mercury during three flybys and the two-Mercury-solar-day nominal mission: a monochrome global image mosaic at near-zero emission
angles and moderate incidence angles, a stereo-complement map at off-nadir geometry and near-identical lighting, multicolor
images at low incidence angles, and targeted high-resolution images of key surface features. These data will be used to construct
a global image base map, a digital terrain model, global maps of color properties, and mosaics of high-resolution image strips.
Analysis of these data will provide information on Mercury’s impact history, tectonic processes, the composition and emplacement
history of volcanic materials, and the thickness distribution and compositional variations of crustal materials. This paper
summarizes MDIS’s science objectives and technical design, including the common payload design of the MDIS data processing
units, as well as detailed results from ground and early flight calibrations and plans for Mercury image products to be generated
from MDIS data. 相似文献
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土壤优先流模型理论与观测技术的研究进展 总被引:1,自引:0,他引:1
优先流是土壤中常见的和重要的水流运动和溶质运移形式。由于土壤优先流的形成和影响因素众多、表现形式多样,加之土壤优先流的快速非平衡特征明显以及土壤高度的空间变异性,准确描述和模拟土壤优先流的时空变化特征一直以来都是土壤水文学界的热点问题和难点问题。该文从优先流的定义、表现类型、形成和影响因素、模型理论与观测技术等5个方面综述了土壤优先流的研究进展,指出该领域今后的主要研究方向为建立土壤优先流的统一判别标准、提升优先流模型理论的有效性、发展优先流的专用观测技术设备。文章对深入研究土壤优先流具有参考价值。 相似文献
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Yang Moucun a * Nie Hong b a College of Energy Power Engineering Nanjing University of Aeronautics Astronautics Nanjing China b College of Aerospace Engineering Nanjing University of Aeronautics Astronautics Nanjing China 《中国航空学报》2007,20(6):518-523
Based on probabilistic fracture mechanics approach, a new concept of material initial fatigue quality (MIFQ) is developed. Then, the relation between S-N curve and crack propagation curve is studied. From the study, a new durability analysis method is presented. In this method, S-N curve is used to determine crack growth rate under constant amplitude loading and evaluate the effects of different factors on durability and then the structural durability is analyzed. The tests and analyses indicate that this method has lower dependence on testing, and higher accuracy, reliability and generality and is convenient for application. 相似文献
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Geodetic Methods for Calibration of GRACE and GOCE 总被引:2,自引:0,他引:2
It is beyond doubt that calibration and validation are essential tools in the process of reaching the goals of gravity missions
like GRACE and GOCE and to obtain results of the highest possible quality. Both tools, although general and obvious instruments
for any mission, have specific features for gravity missions. Therefore, it is necessary to define exactly what is expected
(and what cannot be expected) from calibration and what from validation and how these tools should work in our case. The general
calibration and validation schemes for GRACE and GOCE are outlined. Calibration will be linked directly to the instrument
and the measurements whereas validation will be linked to data derived from the original measurements. Calibration includes
on-ground, internal, and external calibration as well as error assessment. The calibration phase results in corrected measurements
along with an a posteriori error model. Validation of e.g. calibrated measurements or geoid heights means checking against
independent data to assess whether there are no systematic errors left and/or whether the error model describes the true error
reasonably well. Geodetic methods for calibration typically refer to external calibration and error assessment, and will be
illustrated with an example.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献