Experimental investigation on a Jeffcott rotor with combined coupling misalignment using time-frequency analysis

IF 0.7 4区 工程技术 Q4 ENGINEERING, AEROSPACE
Ashutosh Kumar, P. Sathujoda, N. Bhalla
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引用次数: 0

Abstract

Abstract Rotating machinery, such as turbo-jet engines, operate at a high rotational speed and passes through critical zones. The dynamic response of high-speed machines is critical for long-term stability and functioning. In this work, a fast and effective method for detecting coupling misalignment utilising time-frequency analysis (TFA) based on both the adaptive noise added complete ensemble empirical mode decomposition and wavelet-based denoising is presented. This novel and innovative method detect the coupling misalignment feature via the amplitude modulation aspect in the envelope analysis of the fault-containing intrinsic mode function. The Hilbert spectrum analysis provides spontaneous frequency and spectral energy in the time-frequency domain. The experiments were performed for various rotor accelerations and combined parallel and angular coupling misalignments using a laboratory test rig. The suggested approach gives excellent denoising efficiency and can improve misalignment identification accuracy. Additionally, it may be highly helpful for machinery that starts and stops often.
基于时频分析的Jeffcott转子组合耦合错位实验研究
旋转机械,如涡轮喷气发动机,在高转速下运行并通过临界区域。高速机械的动态响应对其长期稳定性和功能至关重要。本文提出了一种基于自适应噪声加全系综经验模态分解和小波去噪的时频分析(TFA)快速有效的耦合失调检测方法。该方法通过对含故障本征模态函数包络分析中的调幅来检测耦合失调特征。希尔伯特谱分析提供了时频域的自发频率和谱能量。在实验室试验台上,对不同转速下转子的平行耦合和角耦合组合失对进行了实验研究。该方法具有良好的去噪效果,提高了定位误差的识别精度。此外,它可能对经常启动和停止的机器非常有帮助。
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来源期刊
International Journal of Turbo & Jet-Engines
International Journal of Turbo & Jet-Engines 工程技术-工程:宇航
CiteScore
1.90
自引率
11.10%
发文量
36
审稿时长
6 months
期刊介绍: The Main aim and scope of this Journal is to help improve each separate components R&D and superimpose separated results to get integrated systems by striving to reach the overall advanced design and benefits by integrating: (a) Physics, Aero, and Stealth Thermodynamics in simulations by flying unmanned or manned prototypes supported by integrated Computer Simulations based on: (b) Component R&D of: (i) Turbo and Jet-Engines, (ii) Airframe, (iii) Helmet-Aiming-Systems and Ammunition based on: (c) Anticipated New Programs Missions based on (d) IMPROVED RELIABILITY, DURABILITY, ECONOMICS, TACTICS, STRATEGIES and EDUCATION in both the civil and military domains of Turbo and Jet Engines. The International Journal of Turbo & Jet Engines is devoted to cutting edge research in theory and design of propagation of jet aircraft. It serves as an international publication organ for new ideas, insights and results from industry and academic research on thermodynamics, combustion, behavior of related materials at high temperatures, turbine and engine design, thrust vectoring and flight control as well as energy and environmental issues.
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