切削载荷的英文

• chip-load

• "切削"英文翻译    cutting; cut; profiling
• "载荷"英文翻译    load; loading
• "切削" 英文翻译 :    [机械工程] cutting; cut; profiling 粗切削 rough cut; 高速切削 high-speed cutting; 金属切削 metal cutting
• "载荷" 英文翻译 :    load; loading◇载荷变化 load fluctuation; variation in load; 载荷装置 load device
• "粗切削" 英文翻译 :    bastard cut; lower cut; rough cutting; rough machining; roughing cut
• "精切削" 英文翻译 :    finishing cut
• "净切削" 英文翻译 :    clean cut
• "冷切削" 英文翻译 :    cold machining
• "慢切削" 英文翻译 :    slow cutting
• "浅切削" 英文翻译 :    light cut; shallow cut
• "切除,切削" 英文翻译 :    remove
• "切削比" 英文翻译 :    cutting ratio
• "切削层" 英文翻译 :    cut level; cutting lay; lay of cutting; layer of cutting
• "切削齿" 英文翻译 :    cogging; cutting teeth; cutting tooth
• "切削刀" 英文翻译 :    bite; cutter blade; kurvenfrmige schneide curved cutting edge; working angles
• "切削的" 英文翻译 :    truncated
• "切削点" 英文翻译 :    schnittpunkt point of intersection
• "切削法" 英文翻译 :    cutting system
• "切削弧" 英文翻译 :    cutting arc
• "切削击," 英文翻译 :    chin
• "切削机" 英文翻译 :    block splitting machine; cutting machine
• "切削剂" 英文翻译 :    coolant; cutting agent
• "切削件" 英文翻译 :    schneidteil cutting part
• "切削角" 英文翻译 :    angle of cutting; cut angle; cutting angle
• "切削具" 英文翻译 :    cutting apparatus

• Some key models including initial residual stress model , dynamic cutting load model and restriction transform model were built and researched deeply by coupled thermo - mechanical method
  在深入研究残余应力施加、动态切削载荷、约束转换等铣削加工模拟关键技术的基础上，采用热力耦合模式进行了求解。
• Machining deformation of aircraft monolithic component is simulated by finite element method ( fem ) and validated by experiment . the initial residual stress in pre - stretched plate is generated by simulating quenching and stretching processes . with a single tool - tooth milling process fem , the machining loads in monolithic component material removing is obtained . restart - calculation is put forward to complete the whole simulation of machining process . to verify the fem result , an experiment is carried out . the deformation distribution of the monolithic component resulting from fem shows a good agreement with the experiment result , which indicates that the key technologies presented in the paper are practicable and can be used to simulate the milling process of monolithic component to predict its deformation . lengthy and expensive trial and error experiment process can be avoided
  在模拟淬火、拉伸过程获得含有初始残余应力的预拉伸板材以及模拟单齿切削过程获得切削载荷的基础上,提出并采用接力算法,对一航空整体结构件的材料铣削过程进行有限元仿真,同时进行了试验研究.结果表明,有限元模拟的整体结构件的变形与试验具有一致性,从而证明提出的整体结构件加工仿真关键技术的可行性,避免了为研究加工变形而进行的繁琐的试错法