• Starter generators, generator control units, Compressor drive motors, DC electric motors, Centrifugal blowers, Vane axial blowers, Rewinding electromechanical services.

    发电机起动器,发电机控制单元,压缩机驱动马达,直流电动机,离心式吹风机,叶片轴向吹风机,重绕机电产品服务。

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  • The hub treatment with a circumferential groove was tested on the stator hub and compared with the casing treatment over the rotor tip for a single stage axial flow compressor.

    在单级轴流压气机上,用周向槽式处理机匣在静子内径处进行轮毂处理,与转子尖部机匣处理作类比。

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  • Finally, the total loss distribution along the blade span of the axial flow compressor is estimated according to an improved end wall loss model and a shock loss model.

    再应用改进了的端壁损失和激波损失模型,最终算出轴流压气机设计点损失沿叶高的分布规律。

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  • Gas composition, volume flow rate, axial power, pressure and temperature of inlet and discharge gases of the compressor have been evaluated with the international general standard.

    采用国际通用标准对压缩机气体组成、容积流量、轴功率、进排气压力和进排气温度等指标进行了测定。

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  • The thermoaerodynamic design philosophy and features of the centrifugal compressor and the axial turbine of the turbocharger GZ680 are discussed.

    本文介绍了GZ680增压器的离心压气机与轴流透平的气动热力学设计思想及特点。

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  • This paper also considers the effects of radial and axial clearances, probe blockage, step matching and measuring techniques on the performance of the compressor.

    本文讨论了径向轴向间隙,探针堵塞,级间配合和一些测试技术对压气机性能的影响。

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  • Test results have shown that the test technology is effective and suitable for test of unsteady flow frequency spectrum performance of axial compressor.

    试验结果表明,该试验技术对进行轴流压气机叶片排流场非定常频谱特性试验是行之有效的。

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  • The deviation between temperature rise efficiency and torque efficiency has a negative impact on the accurate assessment of experimental results of axial compressor.

    轴流压气机试验时,温升效率与扭矩效率之间的偏差给准确评估试验结果造成了一定影响。

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  • 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;

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  • Reason of error generated when axial compressor and TRT blades processed by profiling is analyzed.

    分析了用靠模法加工轴流压缩机叶片及能量回收透平膨胀机叶片时产生误差的原因。

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  • Analyzed some surge curves of axial air compressor which are provided by manufacturers, some factors which should be considered in setting anti_surge curves of axial air compressor are submitted.

    对厂家提供的几台轴流式空气压缩机的喘振曲线进行分析,提出设置轴流式空气压缩机防喘振曲线应考虑的一些因素。

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  • Therefore, it is to shut down axial fan conveyor motor and turn off power after finished products with freeze, as well as notify the operator at ammonia compressor and keep telephone records.

    货将冻结完毕,关闭轴流风机及传送电机,切断电源。通知氨压缩机操作人员,并做好电话记录。

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  • A new model is presented for calculating the end-wall boundary layer and its blade force defect inside the axial compressor cascade, based on theoretical analysis.

    通过理论分析提出一种考虑叶片端部间隙影响的叶片力亏损模型,并对三种轴流压气机叶栅的端壁边界层及叶片力亏损进行了数值计算。

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  • A method for predicting the off design performance of an axial flow compressor is presented.

    本文介绍一种轴流压气机非设计性能的预测方法。

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  • The presented problems and resulted harm about air seal axial clearance in a centrifugal compressor are pointed out.

    指出了离心空压机气封轴向间隙存在的问题及造成的危害。

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  • A stage - by - stage simulation method is introduced for analysis of inlet total pressure distortion effect on the multistage axial flow compressor characteristics.

    介绍了1种分析进口总压畸变对多级轴流压气机特性影响的逐级模拟方法。

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  • Worm compressor in the process of compressed gas, also will inevitably suffer reaction of gas, the force is also in the worm into big radial force and axial force.

    蜗杆压缩机在压缩气体的过程中,也同样必然受到气体的反作用力,该力也在蜗杆上形成很大的径向力和轴向力。

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

    研究了顶部间隙对压气机转子总性能及内部流场的影响。

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  • The utility model relates to a fixing device of a star wheel body axial position of a helical-lobe compressor, belonging to the compressor field.

    本实用新型涉及一种单螺杆压缩机星轮体轴向位置的固定装置,属于压缩机领域。

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  • 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。

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  • Influence of the wake impact effect on the flow field and its average performance in a low speed axial-flow compressor was investigated by using external acoustic excitations.

    通过采用外部声激励的方式,在低速轴流压气机内研究非定常尾流撞击效应对压气机流场结构以及时均气动性能的影响。

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  • The stall surging characteristic and its prevention measure are analysed with focus on low-pressure axial fan, high-pressure axial fan and mutiple-stage axial compressor.

    针对低、高压轴流送风机及多级轴流压缩机在低流量区域的失速喘振特性及其预防措施进行了分析。

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  • A new three-dimensional aerodynamic stability model for an axial flow compressor to study the effects of radial disturbance on the rotating stall is presented.

    给出了考虑压气机径向扰动对失速影响的轴流压气机三维气动稳定性模型。

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  • An experimental study of the stator blade wake in a small axial compressor is performed by using a hotwire anemometer (HWA) under different rotating speeds and mass flow conditions.

    基于小型轴流压气机实验台,运用热线风速仪(HWA),对不同转速、流量工况下,静叶排出口尾迹流动特性进行实验研究。

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  • In this paper, virtual prototype technology of turbo-machinery, multistage axial flow compressor numerical simulation, and integrated design of turbo-machinery and engine have been introduced.

    介绍了叶轮机虚拟样机技术、多级轴流压气机数值仿真和叶轮机与发动机一体化设计。

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

    为实施裕度定制,本文开发了能够体现裕度定制思想的轴流压气机二维特性预估方法。

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  • 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。

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  • The effects of momentum and energy transportation caused by circumferential non uniformities of the flow in a multistage axial compressor are studied.

    本文研究轴流压气机流场周向非均匀性的动量输运和能量输运作用。

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  • This article investigates the nonlinear dynamic characteristics and stability of an axial flow compressor with tip clearance and ball bearings.

    研究叶尖气隙和滚动轴承共同作用下轴流压缩机的非线性动力特性及稳定性。

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  • The characteristics of static pressure changing at stage exits of a multi-stage axial flow compressor relative to the design points at several typical operating modes are investigated.

    对多级轴流式压气机在几个典型工况下各级静压相对于设计点静压的变化特性进行了研究。

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