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IssuesArchive of Issues2023-2pp.602-621

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Wujiu Pan, Haoyong Qu, Lele Sun, and Xianmu Li, "Nonlinear Vibration Behavior of Aero-Engine Rotor-Bearing System in Maneuvering Flight," Mech. Solids. 58 (2), 602-621 (2023)
Year 2023 Volume 58 Number 2 Pages 602-621
DOI 10.3103/S0025654422601501
Title Nonlinear Vibration Behavior of Aero-Engine Rotor-Bearing System in Maneuvering Flight
Author(s) Wujiu Pan (School of Mechatronics Engineering, Shenyang Aerospace University, Shenyang, 110136 PR China; Advanced Manufacturing Technology Research Center, Shenyang Aerospace University, Shenyang, 110136 PR China, panspace@sina.cn)
Haoyong Qu (School of Mechatronics Engineering, Shenyang Aerospace University, Shenyang, 110136 PR China; Advanced Manufacturing Technology Research Center, Shenyang Aerospace University, Shenyang, 110136 PR China)
Lele Sun (School of Mechanical Science and Engineering, Huazhong University of Science and Technology, Wuhan, 430074 PR China)
Xianmu Li (School of Mechatronics Engineering, Shenyang Aerospace University, Shenyang, 110136 PR China; Advanced Manufacturing Technology Research Center, Shenyang Aerospace University, Shenyang, 110136 PR China)
Abstract Analyzing the dynamic characteristics of an aero-engine rotor-bearing system helps professionals predict and judge the dynamic behavior of aero-engines. It is different from the traditional dynamic analysis of rotor system with fixed foundation, this paper considers the dynamics of the rotorbearing system caused by the horizontal yawing maneuver load. This paper establishes a finite element model of a double-disc rotor-bearing system, and use the Newmark-β algorithm to solve the system. The model established in this paper is compared with the model established in ANSYS software, and the correctness of this model is verified. The influence of the maneuver load on the nonlinear dynamics of the rotor-bearing system under horizontal yawing is analyzed in detail. The study found, the maneuver load can suppress nonlinear vibration; the increase of maneuver load can reduce the nonlinear influence of the system caused by changes in relevant bearing parameters; and between two times the critical speed and three times the critical speed, the system will produce rich and complex nonlinear dynamic phenomena such as single periodic motion, multi periodic motion, and quasiperiodic motion.
Keywords horizontal yawing, nonlinear analysis, double-disc rotor system, dynamic modeling
Received 23 October 2022Revised 26 December 2022Accepted 11 January 2023
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