轉角葉片 的英文怎麼說

中文拼音 [zhuǎnjiǎopiān]
轉角葉片 英文
corner vane
  • : 轉構詞成分。
  • : 角Ⅰ名詞1 (牛、羊、 鹿等頭上長出的堅硬的東西) horn 2 (古時軍中吹的樂器) bugle; horn 3 (形狀像...
  • : 片構詞成分。
  • 轉角 : corner; diversion; street corner; nook
  1. Because of the technical complexity of the turbine for the three gorges project and on the basis of several important technical problems which have been defined in the international bidding documents for 14 generating units in the left bank power station, the owner of the project has decided another some important technical problems based on appraisal and comparison in the bid appraisal stage after the bidding documents are analyzed and the tender documents are cleared by the tenderers

    由於三峽工程水輪機技術上的復雜性和挑戰性,在左岸電站14臺機組國際招標文件已明確了若干重大技術問題的基礎上,在機組議評標階段,對招標文件進行分析和投標商對投標文件進行澄清說明后,經評議比選,業主又決策了幾個重大技術問題,主要有:水輪機設計水頭的確定,負傾水輪機的應用,兩套水力設計,舍棄初期輪,蝸殼進行水壓試驗等。
  2. Here we found g proteins also function in leaf, silique development and the yield of pollen microspore. we observed several traits or characters in the offsprings of gpal, agbl null mutation and gpa1 overexpression lines and found that the width of mutants " lamina is larger than that of the wild type, whereas the lamina length, petiole length and rosette diameter is smaller than the wild type, the ga overexpression lines is different from the mutants ; the silique length and the pedicel length is larger in mutants than that of wild type, and slightly smaller in overexpression lines than the control ; the morphometric character in silique tip is different in gpal from agbl mutants ; the yield of pollen microspore is larger in null mutants than wild type whereas smaller in overexpression lines

    實驗中我們跟蹤觀察了多代異三聚體g蛋白a亞基超表達基因植株及a , p亞基缺失突變體的表型特徵,發現突變體的寬度大於對應的野生型,長度,柄長度及蓮座直徑小於野生型,而超表達植株的上述某些特徵與突變體相反; gp時突變體的長果長度,花梗柄部長度大於野生型,而超表達ga植株種英則略小於對照; gpal突變體長果尖端未出現咭乙i突變體的特徵: gpal ,口gbl突變體花粉生成量大於野生型,而超表達ga植株的花粉生成量則略小於對照。
  3. 4 ) in a pre - swirl rotator - stator cavities with discrete pre - swirl nozzles and blade - cooling entry holes, the influences of pre - swirl angle and flow parameter on the flow and heat transfer characteristics were numerically investigated. the correlation for average nusselt number vs rotating reynold number or non - dimensional mass flowrate were established. the results show that : advantage of per - swirl inflow is the effect of cooling the blade - cooling entry holes ; pre - swirl inflow increases heat transfer in rotating disk of pre - swirl chamber ; as pre - swirl angle increases, local nusselt number decreases in pre - swirl chamber ; the temperature of stator of inner rotator - stator chamber and per - swirl chamber decreases as rotating reynold number increases ; when the axial mass flowrate maintains constant, heat transfer in the rotating disk of inner rotator - stator cavities does n ' t change as per - swirl mass flowrate increases, while heat transfer in the rotating disk of per - swirl chamber increases ; when the pre - swirl mass flowrate maintains constant, change of the axial mass flowrate has effect on the whole cavity

    結果表明,預旋進氣的優點在於增強了冷卻孔附近的對流換熱效果,局部努謝爾數隨預旋的增大而有所減小;隨旋雷諾數的增加,不論是內靜腔室還是預旋腔室的靜盤上的溫度都不同程度的降低:當軸向中心進氣質量流量不變時,隨預旋進氣的質量流量增加,內靜腔室的盤盤面上的換熱基本沒有變化,而預旋腔室的盤盤面上的換熱效果增強;當預旋進氣質量流量不變時,軸向中心進氣的質量流量的改變對整個盤腔都有影響。
  4. Proceed from the angle of energy and taking considerations on interference factor and drag of airfoil profile, a kind of new typed calculation method on the design of vane air foil was put forward according to the vortex aerodynamics model of the rotor of wind turbines with horizontal axis

    摘要根據水平軸風力機子的渦流氣動模型,從能量的度入手,考慮干涉因子和翼型阻力,提出了翼型設計的一種新型計算方法。
  5. The switching power for driving the stepper - motor. furthermore, i take part in the vgt performance examination, from which i obtains the data map of vane position and boost pressure with economic rules

    參與vgt性能試驗,通過試驗數據的分析,以經濟性原則得到了增壓壓力脈譜圖和最佳位置脈譜圖。
  6. In this way, when obturation cubage leave absorb oil cavity it connects the eduction oil cavity with the v trough and with the increasing of the turning angle, the size of the cross section of v trough become bigger and bigger, which make the pressure between the cavity of two blades much higher and higher, and until it completely connects the eduction oil cavity, it reaches the pressure of the eduction, and it can effectively reduces the fluid noise caused by high pressure return flow

    這樣,當密閉容積離開吸油窗口之後,通過v型尖槽逐漸與排油窗口連通,隨著的增加, v型尖槽通流截面積逐漸增大,這就使兩間容腔內的壓力逐漸升高,直至完全接通排油窗口時,才升壓達到壓油腔的壓力,這樣可以有效地降低因高壓迴流而引起的流體噪聲。
  7. Through repairing the worn parts of four hydropower stations of xinzhuang, zaoqi, suide and qiemo, and taking some comprehensive anti - abrasion measures, such as checking and repairing the runner blade, cutting the head of blade into round shape, adding an apron to the outer edge of blade and increasing a guiding plate in the head of blade, a good effectiveness has been gained so that it increases the output of generating unit and enhances the abrasion resistant capacity

    通過對新莊、棗渠、綏德、且末4個水電站的磨蝕破壞部件的修復、測型與修型、頭部割圓外緣加裙邊、頭部加導流板等抗磨蝕措施的綜合治理,取得較好效果,使機組出力增加、抗磨蝕能力提高。
  8. In this paper, some off - line manual methods for regulation of flow equation have been compared and analyzed. based on pid speed governor of turbines, two kinds of governors are designed for adjustable - blade pump, which can perform autoregulation on water height of the fore bay and on pump output by adjusting the blade angle of adjustable - blade pump. the computation models of the two kinds of governors are also offered and the transient simulation can be done on pc

    文中,比較分析了現有的多種離線手動調節流量平衡的方法,在水輪機pid調速器的基礎上,針對槳泵設計了兩種新型調節器,通過改變槳泵的安放,分別能對泵站前池水位和泵的輸出流量進行自動調節;提出了兩種新型調節器的計算模型,使槳泵在線自動調節動態模擬得以在微機上得以實現。
  9. The velocity - coefficient method was used to design a 180mm diameter impeller with five single - arc - cylinder blades. the exit angle and inlet angle of the segment are 35. 1 and 36. 0 in degrees respectively. the shape volute ' s cross - section is the rectangle

    輪採用速度系數法設計,輪外徑180mm ,共有5張單圓弧圓柱形,其出口安放、進口安放分別為35 . 1度、 36 . 0度。
  10. The complex vortex system structure and shock wave system structure inside this rotor is obtained. wall flow patterns on the blade surface and hub surface are found out. the complex vortex system structure, such as horseshoe vortex, passage vortex, corner vortex and trailing vortex, and the interaction with shock wave system are researched. especially, the character of the tip clearance flow inside the rotor passage is revealed, and the interaction between shock wave and tip clearance flow near blade tip and the evolution of tip clearance flow are considered

    給出了表面及輪轂面上的壁面流型,分析並揭示了道內的馬蹄渦、通道渦、渦、尾渦等復雜渦系及其與激波的相互干涉;特別是,分析並揭示了道內頂隙射流的特點,得到了頂隙附近激波與泄漏流動的干涉形態及泄漏流動的發展,並著重給出了其與激波的干涉形態。
  11. Lastly, previous vane are analysed by fluent, we calculate the pressure distribution chart and report chart of each wing form, then alter the torsion angle and the airfoil form of the vane respectively, finally ascertain the influence curve of the torsion angle and the airfoil form of the vane on which act the lift power

    最後,通過fluent對設計出的分析,得出其壓力分布圖和報告圖。然後從改變的扭度和翼型兩個方面分析其對升力和阻力的影響。得出的扭和翼型對升阻比的影響曲線,在文章的結尾部分估算了無人機的一些性能參數。
  12. A variable vector propeller, called the " varivec propeller ", is under development as a new propulsion system for the undersea robot. the varivec propeller is a kind of specific propeller that is capable of continuously generating any degree of thrust in any three dimensional direction by varying blades " pitches cyclically in the process of rotation and responds easily to the slightest change in the robot

    全方向推進器是一種在運動過程中螺距可以變化的螺旋槳,該推進器是一種全新的設計,它最大特點是通過螺距在槳的過程中周期性的改變,產生前後、上下、左右六個方向的推力,並可以容易的對海洋機器人的微小運動作出反應。
  13. The changing procedure includes : extending of the blade on the tip, extending of the blade on the root, expanding of the surfaces of the blade, extending of the blade on both sides, calculating the balance angle, changing the coordinate system, changing the data on the consideration of the shrinking and the reflecting of the blade material, etc. a blade surface is bended and distorted in three dimensions

    具體化過程包括:尖型面延伸、根型面延伸、身型面余量加放、進排氣邊余量加放、平衡的計算、考慮的收縮和回彈、坐標換等。完成了身實體造型。身型面是復雜三維彎扭曲面,造型上既有精度要求又有光順性要求。
  14. A numerical simulation was performed to analyze the effect of bowed blades on the separation structures in a high - turning compressor cascade

    摘要通過數值模擬,分析了周向彎曲對大折壓氣機柵內分離結構的影響。
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