Chinese translation for "axial flow compressor"

轴两压缩机
轴流式空气压缩机
轴流式压气机
轴流式压缩机
轴流压缩机

Related Translations:

axial gland:  轴腺

axial vector:  轴矢量轴向量轴向矢量轴向向量

axial diffuser:  轴向导叶轴向式扩压器

axial distribution:  轴向分布

axial module:  轴向模数

axial groove:  挤塑机进料段轴向沟槽

axial impeller:  轴流叶轮轴向式叶轮

axial articulation:  轴向滑链连接

axial wobble:  轴向摆动轴向震摆

axial filament:  轴丝

Example Sentences:

	1.	Axial flow compressor 轴流式压缩机
	2.	Experimental study of small perturbation induced rotating stall in axial flow compressor 轴流压气机小扰动诱发旋转失速的试验研究
	3.	Technical specification for construction of fccu axial flow compressor - flue gas turbine trains 催化裂化装置轴流压缩机-烟气轮机机组施工技术规程
	4.	Experimental research of an axial flow compressor performance with stepped tip gap casing configuration 梯状尖部间隙机匣处理对轴流压气机性能影响的实验研究
	5.	Exploring attenuation of steady circumferential pressure distortion of axial flow compressor with axial fan stage 风扇级负荷对其进口总压畸变响应特性影响研究
	6.	The experimental results show that the unsteady flow frequency domain performances of the axial flow compressor will be varied with mass flow , rotating speed , blade row spacing and inlet distortion 实验结果表明，工作流量、工作转速、动?静叶排轴向间距以及进气畸变均对压气机的非定常频谱特性产生影响。
	7.	In order to investigate the unsteady flow frequency domain performances of an axial flow compressor at different mass flow , rotating speed and blade row spacing , plus inlet flow distortion , and considering aerodynamic characteristics and stability of the compressor , the low speed research compressor ( lsc ) at college of energy and power in nuaa is used to carry out the experiment studies . a large amount of test data has been gained through dynamic pressure transducers embedded in the stator blades at the tip , middle and hub section , then fast fourier transform algorithm ( fft ) is applied to calculate the frequency data 为探讨轴流压气机在工作流量、工作转速及动?静叶排轴向间距变化时的叶片排流场非定常频谱特性变化规律，并耦合进气畸变的影响，同时与压气机气动性能和气动稳定性相关联，作者利用南京航空航天大学能源与动力学院的低速大尺寸轴流压气机( lsc )试验器，采取在静子叶片表面埋入动态压力传感器的实验方法，对叶尖、叶中和叶根三个截面的动态压力进行了测量，获得了大量的可靠的实验数据。
	8.	Abstract : concerning the models for discribing aerodynamic stability of axial flow compressor , the original model is one - dimensional , and it is reasonable for the onset of surge only . for the onset of rotating stall , there are just some two - dimensional models at published literatures . a three - dimensional aerodynamic of compressor has been presented in this paper . an aerodynamic stability model concerning radial disturbance of compressor is presented . the calculated results show that the occurrence of radial disturbance is related to the axial velocity disturbance , which has important effect on aerodynamic stability of compressor . the position of onset of stall , in blade tip or hub , is dependent upon the characteristics of blade element . the comparisons of calculated results predicted by 2d and 3d aerodynamic stability model have also been made in this paper 文摘:轴流压气机的气动稳定性模型，最初为一维模型，仅适用于描述喘振发作.对于旋转失速发作，在公开文献中有一些二维模型发表.本文提出了一类考虑压气机径向扰动对失速影响的新的气动稳定性模型.计算结果表明压气机的轴向扰动往往随着径向扰动的产生，径向扰动的强度影响压气机的气动稳定性，在叶尖还是叶根首先产生失速与压气机基元叶栅特性密切相关.本文对轴流压气机二维和三维气动稳定性模型的计算结果进行了对比分析
	9.	Concerning the models for discribing aerodynamic stability of axial flow compressor , the original model is one - dimensional , and it is reasonable for the onset of surge only . for the onset of rotating stall , there are just some two - dimensional models at published literatures . a three - dimensional aerodynamic of compressor has been presented in this paper . an aerodynamic stability model concerning radial disturbance of compressor is presented . the calculated results show that the occurrence of radial disturbance is related to the axial velocity disturbance , which has important effect on aerodynamic stability of compressor . the position of onset of stall , in blade tip or hub , is dependent upon the characteristics of blade element . the comparisons of calculated results predicted by 2d and 3d aerodynamic stability model have also been made in this paper 轴流压气机的气动稳定性模型，最初为一维模型，仅适用于描述喘振发作.对于旋转失速发作，在公开文献中有一些二维模型发表.本文提出了一类考虑压气机径向扰动对失速影响的新的气动稳定性模型.计算结果表明压气机的轴向扰动往往随着径向扰动的产生，径向扰动的强度影响压气机的气动稳定性，在叶尖还是叶根首先产生失速与压气机基元叶栅特性密切相关.本文对轴流压气机二维和三维气动稳定性模型的计算结果进行了对比分析

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