2019
DOI: 10.1016/j.ymssp.2018.11.013
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An efficient decomposition-condensation method for chatter prediction in milling large-scale thin-walled structures

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Cited by 61 publications
(21 citation statements)
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“…At high cutting speeds, intense shear takes place so rapidly that the contact between neighboring segments reduces and tends to vanish until the discontinuous chips are formed [17]. This instability causes fluctuation of cutting force and thus vibration or even chatter [40] in the metal cutting process, which limit the material removal rate, degrade the surface finish and reduce the tool life [28,[41][42][43][44]. For these reasons, a number of researchers have investigated the formation mechanism of chips to seek a balanced solution.…”
Section: Associated Problemsmentioning
confidence: 99%
“…At high cutting speeds, intense shear takes place so rapidly that the contact between neighboring segments reduces and tends to vanish until the discontinuous chips are formed [17]. This instability causes fluctuation of cutting force and thus vibration or even chatter [40] in the metal cutting process, which limit the material removal rate, degrade the surface finish and reduce the tool life [28,[41][42][43][44]. For these reasons, a number of researchers have investigated the formation mechanism of chips to seek a balanced solution.…”
Section: Associated Problemsmentioning
confidence: 99%
“…They are used as inputs for the initial conditions of the workpiece. Then, self-developed or commercial software such as ANSYSTM [20,24,34,71] or ABAQUS [29,35,53,58,71,150] are used to obtain the FRF of the system, the dynamic behavior or its deflection.…”
Section: Computational Solutionsmentioning
confidence: 99%
“…Tuysuz and Altintas [57] developed an iterated improved reduction system technique combined with a matrix perturbation technique to use the computational time only once. Yang et al [29] used component mode synthesis (CMS) and space structural modification to develop a decomposition-condensation model that reduce computational time. Fei et al [20] solved the dynamic model using a semi-discretization method.…”
Section: Computational Solutionsmentioning
confidence: 99%
“…In aircraft, thin walls are included in the design of fuselage, control surface, on-board equipment and body, etc. [ 1 , 2 , 3 ].…”
Section: Introductionmentioning
confidence: 99%
“…In aircraft, thin walls are included in the design of fuselage, control surface, on-board equipment and body, etc. [1][2][3]. Increasingly frequently, the term "integral (structural) thin-walled elements" is used.…”
Section: Introductionmentioning
confidence: 99%