叶身的英文

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"叶身"怎么读用"叶身"造句

英文翻译手机版

blade
leaf lamina
shank

"叶"英文翻译 leaf; foliage
"身"英文翻译 body
"叶身指标" 英文翻译 : leaf area index
"叶申别托夫" 英文翻译 : jeshimbetov; yeshimbetov
"叶生" 英文翻译 : kanoo
"叶申别科夫" 英文翻译 : jeshimbekov; yeshimbekov
"叶生昌" 英文翻译 : ye shengchang
"叶射线" 英文翻译 : foliar ray
"叶生的" 英文翻译 : follicole
"叶舍夫斯基" 英文翻译 : eshevsky; jeshevski; yeshevski
"叶升堡" 英文翻译 : yeshengpu
"叶舍夫" 英文翻译 : jeshev; yeshev

例句与用法

According to the relationships , the solid bodies of the blade forging parts can be generated from the three parts
研究了叶片锻件榫头、凸台和叶身的相互位置关系及如何生成叶片锻件实体。
The resolution to rectify the distortion of the parametric grid has been proved feasible and effective by practice
经实例验证，本文所提出的叶身曲面无扭曲造型方法能够有效对叶身曲面参数网格的扭曲进行矫正。
The sew method , through curve method and through curve mesh method are presented to construct the turbine blade surface which is a free 3d surface
提出了缝合法，截面线整体造型法和曲线网格法三种不同的叶身型面造型方法。
As the ground of the blade body in nc machining system , the cad model of the blade body surface influences the machining quality of the blade body directly
叶身曲面cad模型作为对叶身进行数控加工的依据，直接影响叶身的加工质量。
The molding procedure includes dealing with the end points of section curves , fitting the curves with the defining points , smoothing the curves , sheet molding of the blade surfaces and solid molding of the blade body
造型过程如下：叶身截面线的端点处理、叶身截面线的拟合处理、叶身截面线的光顺处理、叶身曲面造型、叶身实体生成。
In this thesis , a solution is provided to rectify the distortion of the parametric grid , which is created as well when the cad model of the blade body surface is created by traditional way and seriously damages the quality and efficiency of the blade body
本文针对传统叶身曲面造型方法的不是，提出一种叶片类曲面造型参数网格优化技术，实现叶身曲面无扭曲造型，旨在解决严重影响叶身质量和工作效率参数网格扭曲问题。
The main content is as below : the data of the blade surface is transferred to that of the corresponding forging blade surface by elongating the blade on the tip and on the root , expanding the surface of the blade , extending the blade on both sides , calculating the blance angle
主要工作内容如下：根据叶片零件的型面数据，通过叶尖、叶根型面延伸、叶身型面余量加放、进排气边余量加放、计算平衡角等处理，转化成锻件型面数据。
An aeroengine power - turbine 1 ( superscript st ) stage rotor shrouded blade is taken for an example in the article , tightness of shroud and contact force 、 blade body stress under working state and assembly state are calculated by finite element contact analysis method , influence of working load ( temperature and centrifugal force ) is mainly analyzed
摘要以航空发动机动力涡轮一级带锯齿形叶冠的转子叶片为例，用有限元接触分析方法对装配和工作状态下的叶冠紧度和叶冠接触力、叶身应力进行了计算和分析，着重考察了工作载荷（温度和离心力）对叶冠接触力的影响。
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
具体转化过程包括：叶尖型面延伸、叶根型面延伸、叶身型面余量加放、进排气边余量加放、平衡角的计算、考虑叶片的收缩和回弹、坐标转换等。完成了叶身实体造型。叶身型面是复杂三维弯扭曲面，造型上既有精度要求又有光顺性要求。