殘余淬火應力 的英文怎麼說

中文拼音 [cáncuìhuǒyīng]
殘余淬火應力 英文
residual compressive stress
  • : Ⅰ形容詞1 (不完整; 殘缺) incomplete; deficient 2 (剩餘的; 將盡的) remnant; remaining 3 (兇惡...
  • : Ⅰ動詞(剩下) remain; leave: 9減4 余 5。 nine minus four is five ; four from nine leaves five ; i...
  • : 動詞(淬火) temper by dipping in water, oil, etc. ; quench
  • : fire
  • : 應動詞1 (回答) answer; respond to; echo 2 (滿足要求) comply with; grant 3 (順應; 適應) suit...
  • : Ⅰ名1 (力量; 能力) power; strength; ability; capacity 2 [物理學] (改變物體運動狀態的作用) forc...
  1. Based on the analyses on mechanical properties, microstructure and fracture of - the microalloyed steels socrv with various heat treatment technique, it can be affirmed that various fractures arttribute to various mechanism, we can draw conclusion that the strength and toughness of microalloyed steels 50crv will be increase simultaneously by optimal heat treatment technique. to illustrate the mechanism of the strength and toughness of microalloyed steels socrv, we designed the comparative experiment and observed the microstructure of the sample which occurred at different quench and tempering temperature and different tempering time. the last experiment results were determined by the four factors : fined microalloyed elements grains, the decompound of martensite, martensite transformation of remnant austenite and the second phase precipitation

    為解釋微合金化50crv鋼強韌化機理,本文通過對不同溫度,回溫度,回時間下的學性能指標的對比及顯微分析,認為微合金元素的細化晶粒,馬氏體的回分解,奧氏體的轉變,第二相的沉澱析出共同決定了微合金鋼的強韌化情況,特別是由於微合金元素的存在,其細化晶粒及其碳氮化物的沉澱析出,導致鋼的良好的強韌性,並且如果工藝滿足第二相的沉澱析出強化大於回馬氏體分解引起的軟化效,會在硬度曲線中產生明顯的二次硬化現象。
  2. Therefore, it is of interest to investigate residual stresses in aircraft aluminum parts

    因此,研究航空鋁合金構件中的就顯得非常重要。
  3. 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

    本文主要採用數值模擬、理論分析、實驗驗證等方法,對航空構件的產生及影響進行了研究。主要工作集中在以下幾個方面: 1 、闡述了本學位論文的選題背景,在查閱國內外研究文獻的基礎上,歸納總結了航空鋁合金的研究概況,給出了論文的主要研究目標、內容及方法。
  4. 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

    在模擬、拉伸過程獲得含有初始的預拉伸板材以及模擬單齒切削過程獲得切削載荷的基礎上,提出並採用接演算法,對一航空整體結構件的材料銑削過程進行有限元模擬,同時進行了試驗研究.結果表明,有限元模擬的整體結構件的變形與試驗具有一致性,從而證明提出的整體結構件加工模擬關鍵技術的可行性,避免了為研究加工變形而進行的繁瑣的試錯法
  5. These precipitation - hardened aluminum alloys gain their high strengths through heat treatment involving a severe quenching operation, which introduces a very high level of residual stresses

    這些鋁合金為獲得高強度,必須進行固溶與時效處理,其中在過程中會產生很大的
  6. Analysis of quenching residual stress of seamless pipe by fem

    用有限元方法分析無縫鋼管的
  7. Residual stress release in quenched 40cr steel under electropulsing

    的消除
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