渦輪葉片 的英文怎麼說

中文拼音 [guōlúnyèpiān]
渦輪葉片 英文
bucker
  • 渦 : 渦名詞1. （漩渦） eddy; whirlpool; vortex 2. （酒窩） dimple
  • 輪 : Ⅰ名1 （輪子） wheel 2 （像輪子的東西） wheel like object; ring; disc 3 （輪船） steamer; steamboa...
  • 片 : 片構詞成分。
  • 渦輪 : [機械工程] turbine; worm wheel渦輪泵 [航空] turbopump; roturbo; 渦輪發動機 turbine engine; 渦輪風...
  1. This steam is used to turn turbine blades of electric generators.

    這蒸汽被用來推動發電機的渦輪葉片。
  2. Fracture failure analysis of the third class turbine vanes in some engine

    級渦輪葉片斷裂失效分析
  3. In this paper. the conclusion of this paper has utility meaning in analysis on turbine blades cooling after some proper correcting of the geometry structure and boundary conditions

    由於所採用的結構及計算域近似渦輪葉片的冷卻形式（主流加熱，內流通道冷卻） ，因此這種方法經過進一步的改進，可用於渦輪葉片冷卻的計算研究。
  4. Wear failure analysis of plasma spray coating on damping area of turbine blade

    渦輪葉片阻尼面等離子噴塗層磨損失效分析
  5. One cooling method that has gained increasing importance is endwall film - cooling, where coolant air is discharged though discrete holes in the inner and outer endwalls of a turbine blade passage. after leaving the holes, the coolant forms a protective layer between the hot mainstream gas and the surface that is to be protected

    目前廣泛採用的一種重要冷卻方法是渦輪葉柵端壁氣膜冷卻，該方法中冷空氣穿過渦輪葉片上內外端壁離散冷卻孔進行交換，且冷空氣流經冷卻孔后在主流熱空氣與被保護表面之間形成保護層。
  6. Accounting for creep and stress relaxation, a long - term life and low cycle fatigue life prediction method for gas turbine engine hot section is established

    摘要建立了考慮蠕變和應力鬆弛的航空發動機渦輪葉片等高溫構件的持久壽命和低循環疲勞壽命預測方法。
  7. Check no damage for fan blades and turbine blades

    檢查風扇葉片和渦輪葉片無損壞跡象。
  8. Fracture failure analysis for turbine blades of stage

    某發動機二級渦輪葉片斷裂失效分析
  9. Analysis on blade fracture and cause for the incident of a gas turbine

    某燃氣輪機渦輪葉片斷裂及事故原因分析
  10. Two mechanics pull a chipped turbine from an f - 15 engine on the flight ramp

    機械師由f - 15戰機的引擎取出破損的渦輪葉片。
  11. Fluid flow and heat transfer characteristics in the leadingof blades at rotating state

    旋轉狀態下渦輪葉片前緣的流動與換熱
  12. The uneven - thickness algorithm is given to. create the section data of inner blade

    本文研究了帶復雜內腔的渦輪葉片的造型方法。
  13. A new model for film cooling effectiveness computation on blade surface in a turbine cascade

    渦輪葉片型面氣膜冷卻效率的計算模型
  14. Two good examples about conjugate heat transfer problem, one with cooling method, the other without cooling inside turbine blade were investigated

    最後進一步地討論了渦輪葉片中無冷卻和有簡單冷卻通道情況下的流/熱耦合計算。
  15. Haibo huang ( mechanical engineering ) directed by jianzhong xu cooling techniques in turbine have become more important since the extra high inlet temperature in turbine

    隨著渦輪前溫度的提高，渦輪葉片的冷卻技術變得十分重要。渦輪葉片中流/熱耦合計算成為必不可少的熱環境分析手段。
  16. A feature information model is proposed to combine the design information and the geometric information of turbine blade in a same model

    本文提出了渦輪葉片特徵信息模型，將渦輪葉片的設計信息和幾何信息有機的統一在了一起。
  17. The design of three dimensional electrode parts is very complex due to the complex turbo blade mould shape and the structure in parametric design process

    在參數化設計過程中，由於渦輪葉片精鑄模具本身的復雜性導致三維電極設計復雜性增加。
  18. A cad system for three dimensional electrode of turbo blade mould part is developed in this paper

    摘要開發了一個針對渦輪葉片模具活塊的電極零件的cad系統。
  19. Clogging up of the cooling air slits in the turbine blades is primarily caused by ultrafine particles with a high specific surface area

    渦輪葉片之間冷卻空氣縫隙的堵塞主要是因為存在高比表面積的超細粒子。
  20. A parameter has been defined to account for both the heat transfer enhancement and pressure loss caused by different shapes and configuration of pin fin arrays and the optimization analysis shows that cube - shaped pin - fin arrays can be viable alternatives for pedestal cooling in a blade trailing edge

    本文提出了一個強化換熱有效性系數來綜合考慮擾流柱換熱和壓力損失的效果，並用它對各種擾流柱進行了優化分析，優化結果表明方形擾流柱排在渦輪葉片尾緣區冷卻結構設計中是優先考慮的一種結構型式。
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