1) hydrofoil impeller
翼型桨
1.
In an agitated reactor with hydrofoil impeller,effects of draft tube structure and solid content on power consumption and gas holdup were investigated.
4%为佳;翼型桨排出流向上时功耗较小,气含率较高;功耗随固体含量的增加而增大;气液两相体系中的气含率比气液固三相体系中的气含率高;并得到在开孔率为16。
2.
16m) with mixed hydrofoil impeller 6k5 and Rushton turbine was presented.
研究了内径0 382～ 1 16m机械搅拌釜中翼型组合桨气液两相的持气特性 ,考察了结构参数 (包括翼型桨径、桨间距、桨下距离、通气位置、挡板形式及翼型桨排出流方向 )和操作参数 (包括搅拌转速与通气量 )对气含率的影响 。
3.
(The results) indicated that slope blade Rushton turbine-hydrofoil impeller(SRT-HI) was favorable to oxygen transfer in CMC system.
结果表明:在CMC体系中,下层用径向流的涡轮斜叶桨、上层用轴向流的翼型桨有利于氧传递。
2) New type axial impeller
翼型轴流桨
3) hydrofoil impeller
翼形桨
1.
The results showed that process parameters varied with time in fermentation is distinct for different agitator, the hydrofoil impeller replace the disc turbine impeller, might significantly reduce power consumption at the same.
研究结果表明:(1)不同的搅拌桨搅拌其发酵过程参数(粘度,溶氧,效价等)随时间的变化曲线有明显的差异;(2)搅拌功耗同发酵产量之间的关系,翼形桨明显不同于涡轮桨;(3)在相同的生产条件下,用翼形桨代替涡轮桨可节省搅拌功耗。
4) rotor blades
旋翼桨叶
1.
A high strength epoxy matrix and composite cured at moderate temperature for the composite rotor blades of helicopter has been inves-tigated furthermore by using tests of general mechanical properties, nine engineering constants were obtained.
本文对曾用于直升机复合材料旋翼桨叶的高强度环氧树脂基体及其复合材料性能进行了深入的研究工作。
2.
This paper presents the results of a survey of rotor blades optimum design of reducing vibration by modifying blade properties so as to reduce vibratory hub shears and moments, and thereby reduce the vibration level experienced in the fuselage.
围绕降低直升机振动水平的旋翼桨叶减振优化设计 ,对国内外这方面研究进展情况作了综述 ;着重讨论了降低旋翼激振力减振优化设计分析中的几个主要问题 ,包括桨叶减振优化设计途径与目标 ,桨叶优化设计中的分析模型 ,优化设计方法及灵敏度分析技术 ,以及桨叶优化减振设计研究的最新发展方向和需进一步研究的问题等 。
3.
A design oriented method for the dynamic design optimization of composite rotor blades is presented.
提出一种面向设计的复合材料旋翼桨叶结构动力优化方法。
5) rotor blade
旋翼桨叶
1.
Response calculation method for the rotor blade with arbitrary rigid motions;
考虑带有任意刚性运动的旋翼桨叶响应计算方法
2.
Application on Dynamics of Flexible Multibody Systems in Rotor Blade;
柔性多体系统动力学在直升机旋翼桨叶上的应用
3.
A new way to solve dynamical response of rotor blade in helicopter.
提出了一种全新的计算旋翼桨叶动力响应的方法。
6) rotor hub
旋翼桨毂
补充资料：GS,GT型空心桨叶连续干燥机
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说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条