吴轶钢, 杨少轩, 王斌斌, 陈鹏, 徐双喜, 谌伟. 大型无约束型金属波纹管膨胀节隔振测试方法研究[J]. 中国舰船研究. DOI: 10.19693/j.issn.1673-3185.03720
引用本文: 吴轶钢, 杨少轩, 王斌斌, 陈鹏, 徐双喜, 谌伟. 大型无约束型金属波纹管膨胀节隔振测试方法研究[J]. 中国舰船研究. DOI: 10.19693/j.issn.1673-3185.03720
Research on vibration isolation test method of large non-constrained metal bellows expansion joints[J]. Chinese Journal of Ship Research. DOI: 10.19693/j.issn.1673-3185.03720
Citation: Research on vibration isolation test method of large non-constrained metal bellows expansion joints[J]. Chinese Journal of Ship Research. DOI: 10.19693/j.issn.1673-3185.03720

大型无约束型金属波纹管膨胀节隔振测试方法研究

Research on vibration isolation test method of large non-constrained metal bellows expansion joints

  • 摘要: 目的在大型无约束型金属波纹管膨胀节(以下简称金属膨胀节)的隔振试验中,由于其充压时极易发生失稳,试验工装即要平衡内压产生的巨大盲板力,又不能对金属膨胀节两端完全固定,试验难度大,目前缺少标准的试验方法,为此设计了一种用于测试大型无约束型金属波纹管膨胀节隔振效果的试验装置。方法利用双只金属膨胀节对接彼此支撑,两端由台架支撑固定的方法实现轴向稳定,设计轴承拉索和气囊两种不同的限位方式防止径向失稳。利用激振器对充压下金属膨胀节进行轴向和径向激振,采集10Hz~315Hz频率范围内金属膨胀节在两种限位方式下的加速度响应,计算输入端与输出端的振级落差。结果试验结果表明,轴承拉索和气囊装置测量的总振级落差均随着金属膨胀节内部压力增大而减小,且0P、0.8P和P三种内压下气囊装置的总振级落差相对轴承拉索装置在轴向激振方向分别提升了8.59dB、5.70dB和4.80dB,在径向激振方向分别提升了4.32dB、3.57dB和4.95dB。结论所设计的试验装置能获得大型无约束型金属波纹管膨胀节隔振性能,气囊限位装置比轴承拉索限位装置对振级落差影响小,建议大型无约束型金属膨胀节振级落差测试装置采用气囊径向限位可获得较佳的测量结果。

     

    Abstract: Objectives In the vibration isolation test of large non-constrained metal bellows expansion joints (hereinafter referred to as metal expansion joints), due to its easy instability when filling pressure, the test tooling that is to balance the huge blind force generated by the internal pressure, and can not be completely fixed at both ends of the metal expansion joints, the test is difficult, and there is a lack of standard test methods, so a test device is designed to test the vibration isolation effect of large non-constrained metal bellows expansion joints. For this reason, a test device is designed to test the vibration isolation effect of large non-constrained metal bellows expansion joint. Methods The double-metal expansion joints are supported against each other, and both ends are fixed by the pedestal support to achieve axial stabilization, and two different limiting methods, namely, bearing cable and airbag, are designed to prevent radial instability. The axial and radial excitation of the metal expansion joints under pressure is carried out by using the shaker, and the acceleration response of the metal expansion joints in the frequency range of 10Hz~315Hz under the two limiting methods is collected, and the difference in vibration level between the input end and the output end is calculated. Results The test results show that the total vibration level drop measured by the bearing cable and the air bag device decreases with the increase of the internal pressure of the metal expansion joint, and the total vibration level drop of the air bag device under the internal pressure of 0P, 0.8P and P increases by 8.59dB, 5.70dB and 4.80dB, respectively, in the axial excitation direction of the bearing cable device. In the radial excitation direction, 4.32dB, 3.57dB and 4.95dB were increased respectively. Conclusions The designed test device can obtain the vibration isolation performance of large non-constrained metal bellows expansion joints, and the airbag limiting device has less influence on the vibration level drop than the bearing cable limiting device, so it is suggested that the large non-constrained metal expansion joints vibration level drop test device adopts the radial limiting of the airbag to obtain better measurement results.

     

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