渦型元件 的英文怎麼說

中文拼音 [guōxíngyuánjiàn]
渦型元件 英文
vortex element
  • : 渦名詞1. (漩渦) eddy; whirlpool; vortex 2. (酒窩) dimple
  • : Ⅰ量詞(用於個體事物) piece; article; item Ⅱ名詞1. (指可以一一計算的事物) 2. (文件) letter; correspondence; paper; document
  1. Workers can be equipped with hill, north alliance, hill pushed torque converter ( single grade four - turbine components increase power and increase torque ) with isuzu enhanced feicheng driving axle or axle

    可配備山工、北聯、山推變矩器(單級四輪提高功率,增大扭矩)配備五十鈴加強驅動橋或肥城車橋。
  2. The paper establishes mathematics model of electromagnetic heating system of eddy current field and temperature field, and gives corresponding discrete format with elements as eight nodes, hexahedron equal cell, through calculating eddy - current field to gain the internal heat source that the temperature field needed, to use discrete method to solve the problem of induction - heating part ' s temperature field by axial symmetrical electromagnetic, and then to analyze the characteristic of instantaneous temperature field

    本文建立了電磁加熱系統的流場和溫度場間接耦合的數學模,分析了不同頻率下流和溫度的分佈情況,並以八節點六面體等參為例給出了流場對應的離散格式,通過計算流場獲得溫度場所需要的內熱源強度,加熱部的溫度場以軸對稱格式進行離散求解,並對瞬態溫度場有限單法的求解特點進行了分析。
  3. Against a prototype which is being produced , its three dimension end region entity model of stator is established , and with the aim of simplifying calculation , the theory of how to simplify entity model is studied , then the theory is made use of , and the end region entity model of stator is simplifi - ed ; meshing characteristics of three dimension entity model and shortcomin - gs of end region entity model of stator are studied , then meshing method of three dimension end region entity model of powerformer stator is studied as well , and the simplified entity model is meshed with this meshed model , the distribution of end region magnetic field of stator is analyzed , and the magnetic field energy and reactance of powerformer end region are calculated and compared with design value because the prototype is being produced , in this paper , stator core , gap and eddy equipment are not taken into consideration , and this has a little influence on the result , but through analysis , the result is proved to be good through the example calculation , it is known that the method of this paper is useful and through theoretic analysis , it is proved that end region

    針對一臺生產中的樣機,對其建立了定子端部三維實體模,而且為了達到簡化計算的目的,研究了如何將其簡化的理論,並應用這些理論對樣機定子端部實體模進行了簡化;研究了三維實體模的剖分特點和定子端部實體模存在的缺點,在此基礎之上,研究了對簡化的powerformer定子端部三維實體模的剖分方法,並且對簡化的實體模進行了剖分。應用剖分的三維實體模,用有限法分析了powerformer定子端部的磁場分佈,計算了端部區域的磁場儲能,並利用磁場儲能計算了powerformer定子端部漏抗,將計算值與設計值進行了比較、分析。由於樣機處在設計生產階段,本文暫時沒有考慮定子鐵心、氣隙和流器對端部磁場的影響,這對分析結果有一定的影響,但是仍然得到較好結果。
  4. The result of the calculation for tip clearance is reasonable when it is compared with theory. two ways are put forward for convention of dimension of the turbine components from high temperature to low one, which is related with tip clearance, a simple example is used to illuminate that the two ways are useful, using the method of design optimization, axiisk and a blade of a certain turhine is analysed, it showes that the method of design optimization is feasible to be used for convertion of dimension of the turbine components. finally, ansys software is used to analyzed the variation of tip clearance with the method of cyclic symmetry analysis when engine works under the conditions of temperature and rotational speed, am using a new method to deal with thermal contact resistance in the calculation

    本文完善了計算輪葉尖間隙的簡化演算法程序,增加了程序的計算功能,並將其應用於某高壓輪進行葉尖間隙分析,所得結果與理論結果進行了對比,得出修改後的程序用於葉尖間隙計算是合理的;同時提出了與葉尖間隙相關的輪典的冷、熱態的尺寸兩種換算方法,使用優化設計的方法進行了實例分析,說明了所提出的計算方法是可行的;最後應用ansys有限軟體利用循環對稱的方法分析了某發動機高壓輪在溫度場及離心力作用下的葉尖間隙在發動機工作過程中變化情況,並分析了計算中的接觸熱阻的處理問題。
  5. In lifting - surface theory, the non - liner phenomena of the trailing vortex in the transition wake area and of the tip vortex separation are considered. in surface panel method hyperboloidal quadrilateral panels are employed and the morino ' s analytical formulation is used to determine the influence coefficients. the more reasonable pressure kutta condition is satisfied at the trailing edge of propeller blade

    在計算中,對于升力面理論,本論文考慮了過渡區尾收縮和葉梢分離的非線現象的影響;對于面法,本論文採用的是計算較為簡便的基於擾動速度勢的基本公式及雙曲面形狀的面,在槳葉隨邊滿足更趨合理的壓力kutta條,並用morino導出的解析公式計算面的影響系數的快速有效的數值預報方法。
  6. In order to avoid the shell cracking during baking process of quick investment casting based on stereolithography ( sl ) pattern, an expanding model of sl pattern - ceramic shell is proposed via analyzing the interaction between investment shell and sl pattern, then the cracking condition of investment shell is given

    摘要為了解決快速熔模鑄造中殼開裂問題,對樹脂模殼材料在消失過程中的熱變形機理和殼開裂條進行了有限分析,建立了原殼熱變形數學模,並應用於新燃氣輪導向器的快速鑄造。
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