| 航空航天用高频高压正弦压力发生器的设计仿真 |
| |
| 引用本文： | 张忠立,倪玉山,张进明,王灿,任学弟,秦亭亭,刘贝贝,徐子翼.航空航天用高频高压正弦压力发生器的设计仿真[J].上海航天,2019,36(3):130-136. |
| |
| 作者姓名： | 张忠立 倪玉山 张进明 王灿 任学弟 秦亭亭 刘贝贝 徐子翼 |
| |
| 作者单位： | 上海市计量测试技术研究院;复旦大学航空航天系 |
| |
| 基金项目： | 上海市科委技术标准专项(18DZ2203800)；国家质检总局科技项目(2016QK113)；上海航天科技创新基金(SAST2016004) |
| |
| 摘 要： | 研制高频高压正弦压力发生器,测试航空航天用压力传感器在高频高压工况下的动态性能是确保发动机优化测试和控制系统有效的关键。为解决现有平面扫掠型正弦压力发生器存在频率和压力受限的问题,提出了一种径向活塞式正弦压力发生器的原理及结构设计,并进一步基于任意拉格朗日欧拉法进行数值仿真,计算其正弦信号在不同压力和不同工作频率下的动静幅值比与失真度,以及优化压力传感器的安装位置。结果表明:设计的径向活塞式正弦压力发生器应确保0.2～8.0 MPa的工作压力和200～10 000 Hz的正弦压力工作频率,正弦压力动静幅值比优于20%,可应用于航空发动机、汽轮机等领域的动态测试。
|
| 关 键 词： | 正弦压力 动态测试 任意拉格朗日欧拉法 数值仿真 |
| 收稿时间： | 2018/9/3 0:00:00 |
| 修稿时间： | 2018/9/26 0:00:00 |
Design and Simulation of Sinusoidal Pressure Generator with High Frequency and Pressure for Aeronautics and Astronautics |
| |
| ZHANG Zhongli,NI Yushan,ZHANG Jinming,WANG Can,REN Xuedi,QIN Tingting,LIU Beibei and XU Ziyi.Design and Simulation of Sinusoidal Pressure Generator with High Frequency and Pressure for Aeronautics and Astronautics[J].Aerospace Shanghai,2019,36(3):130-136. |
| |
| Authors: | ZHANG Zhongli NI Yushan ZHANG Jinming WANG Can REN Xuedi QIN Tingting LIU Beibei and XU Ziyi |
| |
| Institution: | Institute of Measurement and Testing Technology, Shanghai 201203, China;Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, China,Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, China,Institute of Measurement and Testing Technology, Shanghai 201203, China,Institute of Measurement and Testing Technology, Shanghai 201203, China,Institute of Measurement and Testing Technology, Shanghai 201203, China,Institute of Measurement and Testing Technology, Shanghai 201203, China,Institute of Measurement and Testing Technology, Shanghai 201203, China and Department of Aeronautics and Astronautics, Fudan University, Shanghai 200433, China |
| |
| Abstract: | Developing a sinusoidal pressure device with high frequency and pressure and testing the dynamic performance of pressure transducers used for aeronautics and astronautics is the key to ensure the effectiveness of the engine optimization test and control system. To solve the frequency and pressure limitation of the existing plane-scanning sinusoidal pressure generator, the principle and structure design of the radial piston type of the sinusoidal pressure generator has been first put forward. Meanwhile, numerical simulations have been carried out based on the arbitrary Lagrange-Eulerian (ALE) method, in order to calculate dynamic-static amplitude ratios and distortion degrees under different inlet pressures and frequencies, and further optimize installation locations of pressure transducers. Results show that such radial piston type of the sinusoidal pressure generator at least ensures 0.2-8.0 MPa and 200-10 000 Hz, additionally the dynamic-static amplitude ratio of the sinusoidal pressure is better than 20%, which can be applied to the dynamic test of the aero engine, the steam turbine and other fields. |
| |
| Keywords: | sinusoidal pressure dynamic testing arbitrary Lagrange-Eulerian method numerical simulation |
| 本文献已被 CNKI 等数据库收录！ |
| 点击此处可从《上海航天》浏览原始摘要信息 |
| 点击此处可从《上海航天》下载免费的PDF全文 |
|
