航空铝合金的英文

• aerometal

• "航空"英文翻译    aviation; voyage
• "铝合金"英文翻译    alufer; ardal; aluminium all ...
• "铝合金" 英文翻译 :    [冶金学] alufer; ardal; aluminium alloy◇铝合金导线 aluminium alloy conductor
• "伯马斯蒂克航空用耐热铸造铝合金" 英文翻译 :    birmastic
• "伯马斯蒂克航空用铸造铝合金" 英文翻译 :    birmastic
• "伯马西尔航空用铸造铝合金" 英文翻译 :    birmasil
• "航空设备用铝合金锻制品的超声波检验" 英文翻译 :    standard practice for ultrasonic inspection of
• "mst钛铝合金" 英文翻译 :    mst alloy
• "y铝合金" 英文翻译 :    aluminium y alloys
• "阿派铝合金" 英文翻译 :    alpax
• "巴恩铝合金" 英文翻译 :    bahnaluminium
• "包铝合金" 英文翻译 :    alclad
• "钡铝合金" 英文翻译 :    barium aluminium alloy
• "变形铝合金" 英文翻译 :    deformable aluminium alloy
• "布锡铝合金" 英文翻译 :    bourbon
• "超硬铝合金" 英文翻译 :    extra super duralumin alloy; sd alloy
• "船用铝合金" 英文翻译 :    marine aluminium alloy
• "导电铝合金" 英文翻译 :    cond aluminium
• "蒂坦铝合金" 英文翻译 :    titanal
• "锻铝合金" 英文翻译 :    wrought aluminium alloy; wrought aluminum alloy
• "锻用铝合金" 英文翻译 :    aluminum alloy for temper
• "锻造铝合金" 英文翻译 :    reflectal; wrought aluminium alloy
• "锻制铝合金" 英文翻译 :    aluminum wrought alloy
• "钒铝合金" 英文翻译 :    vananum
• "防蚀铝合金" 英文翻译 :    corrosion resistance aluminium alloy

• Review of pulsed laser deposition technology
  航空铝合金的发展回顾与展望
• The development of corrosion protection of aluminum aerospace alloys
  航空铝合金防腐保护研究进展
• Study on accelerated tests for atmospheric corrosion of aeronautical aluminum alloy
  航空铝合金大气腐蚀加速试验研究
• Therefore , it is of interest to investigate residual stresses in aircraft aluminum parts
  因此，研究航空铝合金构件中的淬火残余应力就显得非常重要。
• The wear patterns and wear mechanisms of solid cemented carbide are analyzed in high - speed milling of aluminum alloy
  摘要对硬质合金整体立铣刀高速铣削加工航空铝合金时的刀具磨损形态及其磨损机理进行了观察和分析。
• In chapter 2 , based on the status analysis on the research of milling force , its characteristic is studied for the aero - material of aluminum alloy 7075 - t7351 , and the empirical model is established by using the regression - orthogonal experimental method where the factor number is five and the standard number is four
  第二章在总结国内外铣削力研究现状的基础上,采用多因素正交试验研究了航空铝合金7075 - t7351的铣削力学特性,建立了该材料的铣削力经验模型,为研究切削力对加工变形的影响提供了依据。
• Second , on the numerical arithmetic of the quench - induced residual stresses ground , the quenching process of 7075t73 aluminum plate is simulated , the effect of material characteristics along with the plate temperature varying in quenching is considered , and on conditions of the different water temperature and different plate thickness , the quenching processes are compared
  2 、建立了航空铝合金板材淬火过程的弹塑性力学模型，对航空铝合金板材温度场与应力场进行了数值模拟，模拟过程考虑了材料特性随温度变化的影响，并对不同的淬火影响因素进行了分析。
• First , the research background of this dissertation is set forth , and summarized with the overview of the history and the current development of residual stress research , based on reading a lot of literatures , and summarized with the general situations of aircraft aluminum alloys quenching and numerical simulation , those are pointed out objective , significance , methods of this research
  本文主要采用数值模拟、理论分析、实验验证等方法，对航空构件淬火残余应力的产生及影响进行了研究。主要工作集中在以下几个方面： 1 、阐述了本学位论文的选题背景，在查阅国内外研究文献的基础上，归纳总结了航空铝合金淬火残余应力的研究概况，给出了论文的主要研究目标、内容及方法。
• The study work in the dissertation is an important part of the tenth five - year defence advanced research project of “ study on control technology of the machining distortion for complex structure parts ” supported by pla general armament department of china . theoretical analysis and experimental study are carried out on the initial residual stresses and their effects on milling distortion for thick aero - aluminum - alloy plate
  本文作为总装备部“十五”预研项目“复杂结构件加工变形控制技术研究”的主要组成部分,以航空铝合金厚板为对象,研究重点定位在其初始残余应力分布规律及其对数控铣削加工变形的影响。