contact hardening 中文意思是什麼

contact hardening 解釋
接觸淬火
  • contact : n 1 接觸；聯系；交涉。2 〈美國〉（有勢力的）熟人；門路。3 【數學】相切；【電學】接觸；觸頭；觸點...
  • hardening : n. 1. 硬化；【冶金】淬火。2. 硬化劑。
  1. The shakedown conditions of contact surface layer based on kinematic - hardening model was given

    提出了接觸體安定性下限分析的線性規劃法和直接疊代法。
  2. Sealing materials for metallic threaded joints in contact with 1st, 2nd and 3rd family gases and hot water. part 2 : non - hardening jointing compounds

    接觸第1 2 3族氣體及熱水的金屬螺紋連接用密封材料.第2部分:非時效硬化的密封材料
  3. Sealing materials for metallic threaded joints in contact with 1st, 2nd and 3rd family gases and hot water - non - hardening jointing compounds

    與第1 ， 2 ， 3類家庭用燃氣和熱水裝置連接的金屬螺紋接頭的密封材料.非硬化密封劑
  4. Studying on the shakedown theories and plastic deformation of contact surface layer the shakedown of contact surface layer is related to the strain - hardening models of materials, such as isotropic hardening, kinematic - hardening, and mixed - hardening. the existing results based on experiments and theory show that the shearing strain behavior of contact surface layer caused by friction can be comparatively described with kinematic - hardening

    研究中，圍繞強化後接觸表面疲勞問題，從強化模型選擇、接觸表層安定性存在的條件及其失效規律，進行了詳細的概念定義、定理證明及推論演算等理論工作，為接觸表面層安定性的數值模擬和疲勞分析奠定了理論基礎。
  5. At present an important subject is researched on prediction methods of the initiation life of rolling / sliding contact fatigue of surface hardening layer based on shakedown theories under cycle contact loading for the strategies of applications of contact element, such as gears, bearings, and railroad rails

    接觸體表面強化（噴丸、塗層）層的疲勞裂紋萌生壽命的研究，是當前齒輪、軸承等接觸件失效分析中的前沿課題。它具有重要而廣泛的工程背景。
  6. In this thesis, the strain - hardening model of contact surface layer, the numerical theories and computational methods for shakedown analyses of contact body are systematically studied and applied to the aero - gear. the mentality is that the effects of the surface hardening and contact fatigue on contact surface layer under cycle contact loading are investigated by using shakedown analysis methods considering in a quantitative way the details of stress - inelastic strain responses, residual stress and residual strain computations

    在國家「航空基金」 、 「總裝預研基金」等課題的資助下，本文以接觸體安定分析與接觸表面層疲勞裂紋萌生壽命預測一般演算法研究為手段，深入、系統研究了接觸體安定分析的數值理論和計算方法，全面研究了影響航空齒輪表面強化層失效的原因並提出了齒輪表面強化層裂紋萌生壽命的預測方法。
  7. Sealing materials for metallic threaded joints in contact with 1st, 2nd and 3rd family gases and hot water - part 2 : non - hardening jointing compounds ; german version en 751 - 2 : 1996

    與第1 ，第2及第3族氣體及熱水接觸的金屬螺紋連接部位
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