Study on the method of avoiding resonance for double-walled single-crystal turbine blades based on crystallographic orientation design: A technique for solving macroscopic vibration problems from a microscopic scale

IF 5.8 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Y.C. Zhao , H. Cheng , H. Wang , Y. Zhao , Y.Z. Fan , Z.X. Wen , Z.F. Yue
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Abstract

Third-order torsional vibration frequency dispersion and the corresponding resonance issues that occur in the new double-walled single crystal turbine blades present a challenging engineering design issue. Therefore, a breakthrough in the crystallographic orientation design technology is crucial to achieve frequency adjustment and resonance avoidance. In this study, based on the grain microstructure characteristics, the method of defining the crystal orientation deviation angle of single-crystal blades was proposed for the first time, and the decoupling model of the grain microstructure attitude angles was established accordingly. Subsequently, the experiments were conducted to validate the grain-attitude dependent vibration theory and the orientation research methodology. Then, numerical simulation tests of the orientation-dependent vibration characteristics were conducted to investigate the influence rule of the primary orientation deviation angle and quadrant angle, the secondary orientation rotation angle, and the coupled orientation deviation angle on vibration frequency. Finally, the design schemes were developed, and compared in terms of their effectiveness in achieving frequency adjustment and resonance avoidance. The results showed that Case 7 not only considerably reduced the frequency dispersion, but also achieved the safety-margin requirement for resonance. Therefore, the proposed orientation design method is effective in solving macroscale resonance issues from a microscale perspective in single-crystal blades, and is expected to provide support for the engineering design of turbine blades.
基于晶体取向设计的双壁单晶涡轮叶片避免共振方法研究:一种从微观尺度解决宏观振动问题的技术
新型双壁单晶涡轮叶片的三阶扭振频散及其共振问题是一个具有挑战性的工程设计问题。因此,突破晶体取向设计技术是实现频率调节和避免共振的关键。本研究基于晶粒微观结构特征,首次提出了单晶叶片晶粒取向偏差角的定义方法,并据此建立了晶粒微观结构姿态角的解耦模型。随后,通过实验验证了颗粒-姿态相关振动理论和取向研究方法。在此基础上,进行了定向相关振动特性的数值模拟试验,研究了一次定向偏离角和象限角、二次定向旋转角和耦合定向偏离角对振动频率的影响规律。最后,提出了设计方案,并比较了它们在实现频率调节和共振避免方面的有效性。结果表明,Case 7不仅大大降低了频散,而且达到了共振的安全裕度要求。因此,本文提出的定向设计方法可以有效地从微观角度解决单晶叶片的宏观共振问题,有望为涡轮叶片的工程设计提供支持。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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