...
首页> 外文期刊>Journal of Engineering for Gas Turbines and Power >An Experimental and Theoretical Investigation of Wave Propagation in Teflon and Nylon Tubing With Methods to Prevent Aliasing in Pressure Scanners
【24h】

An Experimental and Theoretical Investigation of Wave Propagation in Teflon and Nylon Tubing With Methods to Prevent Aliasing in Pressure Scanners

机译:铁氟龙和尼龙管中波传播的实验和理论研究及防止压力扫描仪混淆的方法

获取原文
获取原文并翻译 | 示例
   

获取外文期刊封面封底 >>

       

摘要

Accurate static and dynamic pressure measurements provide the feedback needed to advance gas turbine efficiency and reliability as well as improve aircraft design and flight control. During turbine testing and aircraft flight testing, flush mounting pressure transducers at the desired pressure measurement location is not always feasible and recess mounting with connective tubing is often used as an alternative. Resonances in the connective tubing can result in aliasing within pressure scanners even within a narrow bandwidth and especially when higher frequency content dc to ~125 Hz is desired. We present experimental results that investigate tube resonances and attenuation in 1.35 mm inner diameter (I.D.) (used on 0.063 in. tubulations) and 2.69 mm I.D. (used on 0.125 in. tubulations) Teflon and Nylon tubing at various lengths. We utilize a novel dynamic pressure generator, capable of creating large changes in air pressure (<1 psi to 10 psi, <6.8 kPa to 68.9 kPa), to determine the frequency response of such tubing from ~1 Hz to 2800 Hz. We further compare these experimental results to established analytical models for propagation of pressure disturbances in narrow tubes. While significant theoretical and experimental work relating to the frequency response of connective tubing or transmission lines has been published, there is limited literature presenting experimental frequency response data with air as the media in elastic tubing. In addition, little progress has been made in addressing the issue of tubing-related aliasing within pressure scanners, as the low sampling rate in scanners often makes postprocessing antialiasing filters ineffective.
机译:准确的静态和动态压力测量可提供提高燃气轮机效率和可靠性以及改善飞机设计和飞行控制所需的反馈。在涡轮机测试和飞机飞行测试期间,在所需压力测量位置上平齐安装压力传感器并不总是可行的,并且通常使用带有连接管的凹槽安装作为替代方法。即使在狭窄的带宽内,连接管中的共振也会导致压力扫描仪内出现混叠,尤其是在需要直流至〜125 Hz的较高频率时。我们提供实验结果,研究在1.35毫米内径(I.D。)(用于0.063英寸输卵管)和2.​​69毫米I.D.中的管共振和衰减。 (在0.125英寸的输液管上使用)各种长度的特氟龙和尼龙管。我们利用一种新颖的动态压力发生器,能够产生较大的气压变化(<1 psi至10 psi,<6.8 kPa至68.9 kPa),来确定这种管在〜1 Hz至2800 Hz的频率响应。我们进一步将这些实验结果与已建立的分析模型进行比较,以分析窄管中压力扰动的传播。尽管已经发表了有关连接管或传输线频率响应的重要理论和实验工作,但很少有文献以空气作为弹性管中的介质来提供实验频率响应数据。此外,在解决压力扫描仪中与油管相关的混叠问题方面进展甚微,因为扫描仪的低采样率通常会使后处理抗混叠滤波器无效。

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