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1)  stall margin
失举裕量
2)  stall margin
失速裕量
3)  overdesign ['əuvədi,zain]
裕量
1.
The analysis of the overdesign and the bypass design for the heat exchanger;
换热器设计裕量与旁路设计分析
2.
In the light of process operation and closed loop control, it is proposed that knowable overdesign includes three parts: process condition change overdesign (steady state), equipment aging (steady state) and the control overdesign (dynamic state).
从生产操作和闭环控制的角度,提出可知裕量应当由工艺条件变化裕量(稳态)、设备老化裕量(稳态)和控制裕量(动态)等三个部分构成,并将这一概念应用于换热器操作与设计分析中。
4)  margin [英]['mɑ:dʒɪn]  [美]['mɑrdʒən]
裕量
1.
Since there is no practical operation experience of 300 M W CFB boilers available in China, excessive margin in flow and pressure of air, accounting for 22% and 34.
由于目前尚无300MW循环流化床(CFB)锅炉机组的运行实绩,国内正在建设的、按引进技术制造的国产化300MWCFB锅炉机组的一次风机均选取了非常大的富裕量(约22%的风量裕量和34。
2.
The conception of margin is cited to analyze the constrained functions while getting the minimal results.
针对带中间支骨的耐压圆柱壳结构进行优化,采用改进的复合形法并引入裕量的概念对得到最优解时各个约束条件进行分析。
3.
The problem of margin analysis and control design of FCC regenerator was solved through multi-objective mixed-integer dynamic optimization.
用动态优化的方法求解催化裂化装置再生器的工艺裕量与控制设计。
5)  stall margin
失速裕度
1.
The design strategies of both rotor tip and stator hub forward-swepts were applied to improve the stage efficiency and stall margin.
在此设计基础上对前掠和后掠两个单级的三维数值解进行对比研究,认为前掠、后掠所得风扇效率的差别很小,转子通道在三维相对运动中不存在旋向相反的流动形态;前掠明显提高失速裕度的主要原因是转子通道激波曲面按其自身结构的需要而展向发展,它的展向构形和流向平衡位置不完全随叶片前缘形状改变,因此前掠增大了激波与前缘的相对距离。
2.
In order to extend the stall margin of a centrifugal compressor with splitter blade,two different circumferential groove casing treatments were designed in this paper.
为了提高一带小叶片离心压气机50%设计转速下失速裕度,设计了两套周向槽机匣处理方案,对实壁机匣和处理机匣压气机流场进行了数值模拟分析。
6)  surge margin
失速裕度
1.
The numerical simulation of the performance of axial flow transonic compressor shows that compared to the baseline, the passage shock in the negatively curved rotor moves downstream near the tip, which improves the surge margin of the compressor while moving upstream near the midspan, increasing the energy loss there, so the compressor stage with negatively curved rotor has the lowest efficiency.
对具有弯曲动叶的跨音轴流压气机性能的数值研究表明,反弯曲动叶中通道激波沿径向倾斜角度最大,在顶部移向下游,在中部移向前缘,提高了失速裕度,但也增加了中部损失,反弯曲动叶级效率最低。
补充资料:冲裕
1.晋陆机《皇太子宴玄圃宣猷堂有令赋诗》:"茂德渊冲,天姿玉裕。"本谓道德深厚,姿容温润。后以"冲裕"称颂人君的美好仪容。
说明:补充资料仅用于学习参考,请勿用于其它任何用途。
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