高溫塑性 的英文怎麼說

中文拼音 [gāowēnsùxìng]
高溫塑性 英文
high temperature plasticity
  • 高 : Ⅰ形容詞1 （從下向上距離大; 離地面遠） tall; high 2 （在一般標準或平均程度之上; 等級在上的） above...
  • 溫 : Ⅰ形容詞（不冷不熱） warm; lukewarm; hot; gentle; mild Ⅱ名詞1 （溫度） temperature 2 （瘟） acute ...
  • 塑 : 動詞（塑造） model; mould
  • 性 : Ⅰ名詞1 （性格） nature; character; disposition 2 （性能; 性質） property; quality 3 （性別） sex ...
  • 高溫 : high temperature; elevated temperature; hyperthermia; megatemperature; inferno
  1. Plastics. determination of the tendency of compounds and products based on vinyl chloride homopolymers and copolymers to evolve hydrogen chloride and any other acidic products at elevated temperatures. part 1 : congo red method

    塑料.化合物聚乙烯共聚物基產品衍化為氯化氫的共聚物及高溫下的其他酸性產品的傾向性測定.第1部分:剛果紅測定法
  2. When the specimens are deformed in a long time at the optimal superplastic deformation condition, the microstructure is coarsened sharply. if the deformation time is shortened properly or the deformation temperature is decreased appropriately or strain rate is increased, homogeneous and fine equiaxed crystal microstructure can be obtained

    在最佳超塑性條件下長時間變形時，合金顯微組織將發生明顯粗化，適當縮短變形時間、或適當降低超塑變形溫度及提高應變速率，可得到均勻細小的等軸組織。
  3. The product is a chief material for high temperature insulant, used mainly for the producing of polyimid resin, thin film, and insulating paint. it is also a high temperature curing agent and plasticizer. some kinds of curing agents of powder coating are made from it

    主要用於制聚酰亞胺樹脂，聚酰亞胺在廣泛的溫度范圍內具有優良的電氣絕緣性能，亦可做耐高溫環氧樹脂固化劑聚氯乙烯增塑劑及皮革柔軟劑，還可用做某些粉末原料。
  4. The flow stress can be described by temperature - compensated strain rate, the so - called zener - hollomon parameter

    利用7055鋁合金高溫塑性變形時穩態流變應力、應變速率（
  5. While cyclic deformation experiment under constant strain control is performed in 400, the material shows the continuous hardening until cyclic invalidation. ( 3 ) back stress attained by kwl " s method is used to analyse the bauschinger effect during an incremental step cyclic test and cyclic deformation test under constant strain control, it is shown that back stress increases with increasing plastic strain and the numbers of cycle, and the back stress is uniform, regardless of tension or compression conditions. ( 4 ) as far as recrystallized zircaloy - 4 plate is concerned, the back stress in transverse direction is higher than that in rolling direction due to the higher schmid factor in rolling direction

    對于再結晶狀態的zr一4合金板材試樣來說， t方向（橫向）試樣的背應力要高於r方向（軋制方向）的背應力，原因在於r方向的schmid因子高於t方向的schmid因子; 400下， zr一4合金的背應力要明顯低於室溫下的背應力;含氫200pg / g的zr一4合金的背應力大小與無滲氫的zr一4合金背應力相比，無明顯區別;固溶處理后， zr一4合金的背應力大小發生了變化，在較高塑性應變下，背應力均高於固溶處理前的背應力。
  6. Flexible sheets for waterproofing - bitumen, plastic and rubber sheets for roofing - method of artificial ageing by long term exposure to elevated temperature

    防水柔性板.屋頂用瀝青，塑料和橡膠薄板.長期暴露于提高溫的人工老化試驗
  7. Based on test results, numerical simulations on uniaxial tension at 480 and different strain rate have been conducted

    在試驗研究基礎上，利用chaboche粘塑性模型模擬高溫下（ 480 ） 、不同應變速率的單軸拉伸。
  8. A thermoplastic that will abide rough use and great heat

    熱塑性塑料經久耐用，又可承受高溫
  9. Has this plastic been tested for safety in great heat

    這種塑料在高溫下的安全性是否已檢測過？
  10. 3. based on the interrelations of flow stress, strain rate and deformation temperature, the four constants of 7055 aluminum alloy can be calculated during the deformation process. 4

    ）和變形溫度t之間的相關性，求出了7055鋁合金高溫塑性變形的四個材料常數：結構因子a ，應力水平參數，應力指數n和變形激活能q值。
  11. The ultra - low carbon steel ( 0. 001 % c ) is subject to a strain of ~ 10 by utilizing equal channel angular pressing of ten passes with route c at room temperature. the grain size is refined to ~ 0. 3m and the resultant steel exhibited the yield strength over 678mpa with a reasonable good elongation of 47. 4 %

    本研究成功實現了室溫下超低碳鋼c方式下的ecap變形，累計等效真應變達到10 ，獲得了晶粒尺寸為0 . 3 m超細晶試樣，其屈服強度達678mpa ，是普通熱軋態的兩倍多，並保持高的塑性。
  12. The measure of grains " comminution is brought forward to improve plasticity at room temperature. the key of micro - crystal ' s production is that the time of sample ' s being at high temperature is shorter. the process of crystal ' s growing up will be restrained

    提出了通過細化晶粒來提高室溫塑性的措施，指出了細化晶粒的關鍵是在合成過程中使坯料處在高溫狀態的時間短，以抑制晶粒的長大過程。
  13. A study on the flow stress of plastic deformation for ai - 1osn - 4si alloy at high temperature

    新型鋁錫硅合金高溫塑性變形流變應力的研究
  14. The steady flow stress model of 7055 aluminum alloy at high temperature has been established by regression analysis and artificial neural networks methods, respectively

    運用多元數學回歸和人工神經網路方法分別建立了7055鋁合金高溫塑性變形穩態流變應力模型。
  15. The characteristic of deformation microstructure at high temperatures for 7055 aluminum alloy have been studied. the condition of dynamic recovery and dynamic recrystallization took place in 7055 aluminum alloy had been explored

    研究了7055鋁合金高溫壓縮變形時的微觀組織演變特點，探明了7055鋁合金高溫塑性變形時發生動態回復及動態再結晶行為的條件。
  16. The deformation behaviors and evolution behaviors of the microstructure for the new 7055 aluminum alloy at high temperatures have been investigated by isothermal compression testing method with gleeble - 1500 thermal simulator

    本文利用gleeble - 1500熱力模擬試驗機，採用高溫等溫壓縮試驗方法，對7055新型超硬鋁合金的高溫塑性變形流變應力行為及組織演變行為進行了研究。
  17. The interdependences of flow stress a, strain rate and deformation temperature t for the alloy have been studied with the aids of om, edax, dsc, xrd, tem, sem, regression analysis and artificial neural networks methods

    通過om 、 edax 、 xrd 、 tem 、 sem及數學回歸分析和人工神經網路分析等手段，研究了該合金微觀組織特徵，高溫塑性變形過程中的流變應力、應變、應變速率（
  18. Tial - based alloys with high specific strength are the most potential high temperature structural materials for aerospace application. however, the application of these materials is hindered by low resistance of damage, low room - temperature ductility and fracture toughness and high crack growth rate

    Tial基合金比強度高，是最具潛力的航空、航天用高溫結構材料之一，但因其具有較低的抗損傷能力，較低的室溫塑性、斷裂韌性和高裂紋擴展速率，這些斷裂特性阻礙了這種材料的應用，因而仍有必要研究其斷裂機理。
  19. The high - temperature properties of ti3al matrix alloy can satisfy the request of the exit temperature of the areoengine compress. but the room temperature plasticity of ti3al matrix alloy is very low, hard to shape, and manufacture ' s cost is very expensive

    Ti _ 3al基合金高的高溫性能可以滿足飛機發動機壓氣機出口溫度的要求，但由於ti _ 3al基合金室溫塑性差，成形困難，製造成本高；而tc11兩相鈦合金可以在500以下溫度長時間工作，用於壓氣機盤已比較成熟。
  20. With interstitial content increasing, the strength of ct20a alloy increased while the elongation dropped down. the alloy with low interstitial content had better ductility and toughness

    隨間隙元素含量增加合金強度升高而塑性降低，低間隙元素含量的合金在低溫下有較好的塑韌性。
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