2023
DOI: 10.1177/09544062221147405
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Stiffness and geometry characteristics of flange connection with bolt failure and its influence on rotor dynamics

Abstract: Flange connection is widely used in aero-engine rotor system. The state of bolt is very important to the stable operation of the rotor, but the impact of bolt failure on the dynamic characteristics of the rotor system is not clear. Thus, the stiffness and geometry characteristics of flange connection with bolts failure and its influence on rotor dynamic response are studied. Firstly, a three-dimensional solid finite element model considering contact characteristics and a stiffness test device for flange connec… Show more

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Cited by 6 publications
(2 citation statements)
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“…Yu Liu [10] obtained the stiffness characteristics and shaft bending characteristics of flange connection after bolt failure via numerical simulation and experimental tests. The rotor motion equation with local stiffness asymmetry and initial bending characteristics caused by flange connection bolt failure was established.…”
Section: Introductionmentioning
confidence: 99%
“…Yu Liu [10] obtained the stiffness characteristics and shaft bending characteristics of flange connection after bolt failure via numerical simulation and experimental tests. The rotor motion equation with local stiffness asymmetry and initial bending characteristics caused by flange connection bolt failure was established.…”
Section: Introductionmentioning
confidence: 99%
“…The review of the literature above indicates that it is necessary to study the stiffness characteristic of the flange joint with a spigot using the FE method and experiments, and establish the corresponding simplified analytical model for convenience of use. For this reason, based on the authors' previous finite element studies [25,28], an experimental instrument is built to study and verify the stiffness characteristics of the flange joint, and a simplified analytical model is proposed on this basis.…”
Section: Introductionmentioning
confidence: 99%