Stiffness and geometry characteristics of flange connection with bolt failure and its influence on rotor dynamics
Author:
Affiliation:
1. School of Aero-Engine, Shenyang Aerospace University, Shenyang, Liaoning, PR China
2. Liaoning Key Laboratory of Advanced Measurement and Test Technology for Aviation Propulsion System, Shenyang Aerospace University, Shenyang, Liaoning, PR China
Abstract
Publisher
SAGE Publications
Subject
Mechanical Engineering
Link
http://journals.sagepub.com/doi/pdf/10.1177/09544062221147405
Reference30 articles.
1. Nonlinear interval analysis of rotor response with joints under uncertainties
2. Analytical model of bolted disk–drum joints and its application to dynamic analysis of jointed rotor
3. Dynamic investigation of aeroengine high pressure rotor system considering assembly characteristics of bolted joints
4. Failure modes of bolt and nut assemblies under tensile loading
5. Investigation into the self-loosening behavior of bolted joint subjected to rotational loading
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1. Rub-impact dynamic analysis of a dual-rotor system with bolted joint structure: Theoretical and experimental investigations;Mechanical Systems and Signal Processing;2024-03
2. Rotor Vibration Characteristics Considering Nonlinear Stiffness of Spigot Bolts;Journal of Vibration Engineering & Technologies;2024-02-21
3. Research on the Influence of Disc–Drum Connection Bolt Preloading Rotor Assembly Modal Characteristics and Diagnosis Technology;Machines;2024-01-22
4. Stiffness Characteristics and Analytical Model of a Flange Joint with a Spigot;Symmetry;2023-06-07
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