tip engine 中文意思是什麼

tip engine 解釋
翼尖發動機
  • tip : n 1 （塔、手指、尾巴等的）尖，尖端，頂端，末端，梢。2 裝在末端的東西，加固末端的金屬環[箍]；鞋尖...
  • engine : n. 1. 機械，機器。2. 引擎，蒸汽機，發動機。3. 機車，車頭。4. 工具；〈古語〉方法，手段。vt. 給…安裝發動機。
  1. The example code in that tip explored how to use dois in a simple search engine application

    ）提供了有關這些細微差別的更多詳細信息。
  2. An interpolation program is used to convert the fluent result data to the ansys load data. it is a new method to analyze turbine tip clearance. in this paper, some research of the numerical computation of the tip clearance of aero - engine is done, the parametric method is used and the research on the flow, heat and structure integration analyses is accomplished

    本文對渦輪機匣氣熱固一體化分析方法做了研究，通過編制了載荷轉換與施加程序，從氣熱計算模型中提取溫度場計算結果，並作為載荷加入到熱固耦合計算模型中，實現了高壓渦輪機匣的一體化計算分析，為實現渦輪葉尖間隙的氣熱固一體化分析打下了基礎。
  3. 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

    本文完善了計算渦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渦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渦輪典型部件的冷、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有限元軟體利用循環對稱的方法分析了某型發動機高壓渦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。
  4. The influence of needle tip changes on the diesel engine performance

    噴油嘴針閥頭形狀變化對柴油機性能的影響
  5. In this paper, the status quo of the tip clearance of aero - engine is surveyed, the theory and the method of the numerical computation of tip clearance are introduced, the simple tip clearance calculation program is modified and refined and the computation method of the turbine temperature field is improved

    本文闡述了國內外航空發動機葉尖間隙的研究現狀，介紹了渦輪葉尖間隙計算的理論和方法。對渦輪葉尖間隙準二維計算程序作了修改和完善，改進渦輪部件溫度場的計算方法，增加了變量顯示/修改、程序控制和結果顯示界面，使軟體更加直觀，實用。
  6. Tip clearance has much effect on the properties of aero - engine. as the reference of the project design, the numerical computation of tip clearance can improve the aero - engine performance, reliability and to reduce the specific fuel consumption ( sfc )

    葉尖間隙對航空發動機性能有較大的影響，研究葉尖間隙的數值分析技術可以為工程設計提供參考，從而提高航空發動機的工作性能、可靠性和耐久性。
  7. While this tip doesn t go into the internals of any particular search - engine implementation, it does show how to provide the engine and other clients with sufficient information on parent - child relationships between elements and other nodes to enable it to resolve, for example, xpath location path queries

    我採用了xpath的前一個示例，但文檔排序是xml文檔本身的固有特性，而不僅僅在一個特殊的xml領域。因此它也出現在其它xml技術中。 dom就是一個示例。
  8. Research findings about the tip clearance of engine in the paper are basal, they can be used as reference of control the tip clearance

    本文對發動機的葉尖間隙分析做了一些基礎性工作，對于葉尖間隙控制方面的研究有一定的參考價值。
  9. Research finding about the tip clearance of engine in the paper is basal ; they can be used as reference of aero - engine design and the tip clearance control

    這些工作對于發動機初步設計設計和葉尖間隙控制理論研究有一定的參考價值。
  10. A mathematical model is developed for simulating transient performance of the turbofan engine, in which the transient heat transfer between the components and airflow, tip clearance and components efficiency changes caused by heat transfer are analyzed

    摘要以某渦扇發動機的過渡態性能模擬為研究對象，建立了過渡過程中零部件與氣流之間的不穩定熱交換、由於熱交換引起的間隙變化以及引起的部件效率變化的數學模型，並且將此模型引入面向對象的航空渦扇發動機過渡過程性能模擬程序的框架中。
  11. The calculated result shows that there are significant influences of heat transfer on the engine ' s transient performance, and the component efficiency loss caused by tip clearance changes can not be ignored

    通過計算分析，零部件與氣流之間的熱交換對發動機過渡過程性能有顯著影響；過渡過程葉尖間隙的變化引起的部件效率損失是不容忽視的。
  12. In order of improving the performance and stabilization of aeroengine, it is needed to control the tip clearance of engine. tip clearance numerical analysis is an important content of researching tip clearance control and improving performance of engine

    為改善航空發動機的性能及工作的穩定性，需對發動機的葉尖間隙加以控制，而對葉尖間隙分析是研究葉尖間隙控制方法的重要內容。
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