首页> 外文会议>SAE Noise and Vibration Conference and Exhibition >Development of an Experimental Facility to Characterize Performance, Surge, and Acoustics in Turbochargers
【24h】

Development of an Experimental Facility to Characterize Performance, Surge, and Acoustics in Turbochargers

机译:在涡轮增压器中表征性能,浪涌和声学的实验设施的开发

获取原文

摘要

A cold turbocharger test facility was designed and developed at The Ohio State University to measure the performance characteristics under steady state operating conditions, investigate unsteady surge, and acquire acoustic data. A specific turbocharger is used for a thermodynamic analysis to determine the capabilities and limitations of the facility, as well as for the design and construction of the screw compressor, flow control, oil, and compression systems. Two different compression system geometries were incorporated. One system allows compressor performance measurements left of the surge line, while the other incorporates a variable-volume plenum. At the full plenum volume and a specific impeller tip speed, the temporal variation of the compressor inlet and outlet and the plenum pressures as well as the turbocharger speed is presented for stable, mild surge, and deep surge operating points. The behavior at these operating points is also analyzed in the frequency domain to examine particularly the discrete low frequencies and amplitudes associated with the surge oscillations. Finally, mild and deep surge frequencies are compared with calculated Helmholtz frequencies as a function of impeller tip speed and plenum volume.
机译:在俄亥俄州州立大学设计和开发了一种寒冷的涡轮增压器测试设施,以测量稳态运行条件下的性能特征,调查不稳定的浪涌,获取声学数据。特定的涡轮增压器用于热力学分析,以确定设施的能力和限制,以及螺杆压缩机,流量控制,油和压缩系统的设计和构造。结合了两个不同的压缩系统几何形状。一个系统允许压缩机的压缩性能测量避免的电涌线,而另一个系统包括可变卷增压室。在全增压体积和特定的叶轮尖端速度下,提出了压缩机入口和出口的时间变化以及增压器速度,以及涡轮增压器速度,用于稳定,温和的浪涌和深浪涌的工作点。在频域中还分析了这些操作点的行为,以检查与浪涌振荡相关联的离散低频和幅度。最后,将温和和深浪涌频率与计算的Helmholtz频率进行比较,作为叶轮尖端速度和增压体积的函数。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号