Pressure Pulsations by a Centrifugal Compressor at Blade Passing Frequency

Author(s):  
Itsuro Hayashi ◽  
Shigehiko Kaneko

Pressure pulsations excited by a centrifugal compressor or fan at blade passing frequency may cause severe noise and vibrations in piping systems. Therefore, the practical evaluation method of pressure pulsations is strongly required. In this study, a one-dimensional excitation source model for a compressor was proposed based on the equation of motion. An experiment was performed for the validation of this model. As a result, the relation of the maximum pressure amplitude in piping systems to the location of the excitation source under resonant conditions can be evaluated by introducing the equivalent resistance of the compressor and that of piping systems. The role of the system resistance to the response of pressure pulsations is discussed in detail.

Author(s):  
Itsuro Hayashi ◽  
Shigehiko Kaneko

The characteristics of the pressure pulsations in a drum connected to a piping system excited by a centrifugal compressor or a blower operated at blade-passing frequencies were investigated. In this study, the equivalent resistance of a compressor and that of a piping system were introduced and linked to the three dimensional calculation model, so that the non-linear damping proportional to velocity squared in the system is properly incorporated. The experiment was performed in order to validate the proposed simulation model. As a result, the three dimensional pressure response in the drum as well as the pipe can be well evaluated by this model. Furthermore, the effect of the acoustic dynamic absorber on the pressure pulsations in the pipe and drum is evaluated. When the resonant frequency of the pipe coincides with that of the drum, two peaks appear in the frequency response curve around the resonant frequency of the pipe, because the drum acts as an acoustic dynamic absorber. It is shown that the maximum pressure amplitude in the drum is obtained when the resonant frequency of the pipe is slightly shifted from the resonant frequency of the drum under the small damping conditions. The effect of the damping in the drum and the mode shape of the drum on the maximum pressure amplitude in the drum is discussed in detail.


2016 ◽  
Vol 138 (3) ◽  
Author(s):  
Akira Maekawa ◽  
Takashi Tsuji ◽  
Tsuneo Takahashi ◽  
Minoru Kato

This study proposes a method to measure pressure pulsations in piping systems easily and directly for their accurate evaluation of occurrence location and pressure amplitude. In the proposed method, the pulsations were estimated by combining the strain measurement result on the pipe outer surface with the calculated formula result for thick-walled cylinders. The proposed method was validated experimentally using a mock-up piping system. It was demonstrated that the method could measure the amplitudes and behavior of pressure pulsations with a practical accuracy. The factors influencing the measurement accuracy of the method were also discussed. The method is expected to contribute to more efficient plant maintenance to prevent fatigue failure of piping and plant components because the pulsations that the method measures are the main cause of vibration fatigue and acoustic noise in piping systems.


Author(s):  
Zheji Liu ◽  
Raymond Smith

Centrifugal compressors used in gas transmission produce strong pressure pulsations, piping vibration, and noise. These are undesirable by-products of the compressor operation that is inherently an unsteady process. This is particularly true for compressors that use a vane diffuser, rather than a vaneless scroll type of diffuser. High vibration levels can potentially cause structural damage in the piping, particularly instrumentation connections, which can cause unnecessary machine down-time and production loss, and is a potential safety hazard. This paper discusses a unique technique to reduce centrifugal compressor piping vibration. This technique reduces aeroacoustics excitation by mounting a duct resonator array inside a compressor diffuser. The effectiveness of this technique is demonstrated by a recent field application to address a noise and vibration concern of a compressor installed in a pipeline station. This compressor had run successfully for several years with a high (but not excessive) level of high frequency vibration in the unit piping. Recent changes in pipeline operating conditions resulted in a significant increase in vibration and associated problems including failure of thermowells and resistance temperature detectors (RTDs). A preliminary measurement of gas pressure pulsations and piping vibration revealed a severe level of high frequency vibration that could lead to a fatigue failure of the unit piping, if operation continued under these conditions. Additional vibration data were measured from the compressor to characterize the noise and vibration and to establish the baseline for future comparison. The baseline vibration data are characterized with a dominant component at the blade passing frequency that makes the duct resonator array an ideal solution. Consequently, a resonator array was designed, manufactured, and installed to reduce the compressor piping vibration and noise. A final test was conducted to verify the effectiveness of the resonator array. Comparing the data acquired before and after the resonator array shows that the dominant vibration level at the blade passing frequency was reduced by 93% on average. The compressor is now able to operate safely at the new pipeline conditions, and it runs much quieter over the full operating range.


Author(s):  
Ning Zhang ◽  
Bo Gao ◽  
Chao Li ◽  
Dan Ni ◽  
Guoping Li

Effects of the staggered blades on unsteady pressure pulsations of a centrifugal pump with a specific speed ns=147 are investigated by the numerical simulation method. The obtained results are compared with the original blades. To clarify the resulting effects, eight monitoring points are used to extract pressure signals at three typical working conditions, and component at the blade passing frequency fBPF is emphasized. Results show that the pump efficiency and head will be reduced by the staggered blades, and at the nominal flow rate, the reduction is about 1.5% from comparison with the original blades. For all the eight points, the staggered blades contribute to the reduction of pressure amplitudes at fBPF when the pump works at three flow rates. The averaged reduction is 15.5% at the nominal flow rate. However, the negative effect on the second harmonic of fBPF will be caused by the staggered blades, and the corresponding pressure amplitude will increase at 2fBPF. It means that the pressure pulsation energy will be redistributed among the discrete components in pressure spectrum by the staggered blades. From the TKE distribution, it is found that the TKE values on the blade pressure side will be significantly affected by the staggered blades.


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