axial compressor信息详情

axial compressor发音

意思翻译

[机]轴流式压缩机

相似词语短语

compressor───n.压缩机;压缩物;收缩肌;[医]压迫器

axial───adj.轴的;轴向的;n.(Axial)人名;(法)阿克西亚尔

reciprocating compressor───[机]往复式压缩机;[机]活塞式压缩机;活塞[往复]压气机

axial force───轴线力,轴向力

axial spondyloarthritis───可考虑中轴型脊柱炎

axial fan───轴流式风机,轴流式通风机;[机]轴流式通风机;[机]轴流式风扇;轴两扇风机

axial age───轴心时代;轴心世纪

compressor nebulizer───压缩机雾化器

file compressor───文件压缩程序

双语使用场景

Then the deposition characteristic of different particle diameters in the blade cascade of the axial compressor was obtained.───在此基础上,研究了轴流压缩机叶栅内不同直径粒子在叶片压力面和吸力面的沉积规律;

Results show that the frequency and rotating direction of inlet distortion are most important factors affecting stability of axial compressor.───在低速大尺寸单级压气机实验器上,实验研究了动态进气畸变对压气机稳定边界的影响。

influence of tip clearance on overall performance and detailed flow structure in tip region of an axial compressor rotor was investigated.───顶部间隙对压气机转子总性能及内部流场的影响。

The unsteady surface pressure on stator blade of an axial compressor was measured by means of mounting micro-sensors on blades surface.───本文对一台单级轴流压气机静子叶片非定常表面压力进行了测量。

Compared with the conventional axial compressor, the performance curves of the ram-rotor are vertical to the axis of mass flow rate.───与常规轴流压气机不同,旋转冲压压缩转子的特性曲线垂直于流量坐标轴;

Experimental research was carried on a three-stage low-speed axial compressor with different inlet distortion.───本文对一台带有不同周向进口畸变装置的三级、低速、轴流压气机进行实验研究。

It can produce leaf-shaped axial compressor of 60 sets a year.───年产新叶型的轴流压缩机60台套。

There is introduced a new low-reaction, highly-loaded axial compressor design concept which is coupled with boundary layer suction method.───结合附面层抽吸技术提出了低反动度、高负荷轴流压气机的概念。

The samples then were fixed into fixture, and put onto INSTAON-4505 axial compressor.───将标本稳妥安装在夹具内,置于INSTAON-4505轴向压缩机上。

英语使用场景

Denoising experiment is carried out on discharge noise of single stage axial compressor by using acoustic system of micro perforation plate .

To implement stall margin customizing, two-dimensional performance prediction method of axial compressor for stall margin customizing was developed.

The influence of tip clearance on overall performance and detailed flow structure in tip region of an axial compressor rotor was investigated.