Development of a new model for the varying dynamics of flexible pocket-structures during machining

  1. Get@NRC: Development of a new model for the varying dynamics of flexible pocket-structures during machining (Opens in a new window)
DOIResolve DOI:
AuthorSearch for: ; Search for: ; Search for:
Journal titleJournal of Manufacturing Science and Engineering, Transactions of the ASME
Article number41002
SubjectAerospace components; Analytical modeling; change of thickness; Computation time; Developed model; Dynamic effects; Experimental validations; Finite elements; Model formulation; Multi-span beams; Multi-span plate; New model; Part quality; Pocket structures; Prediction errors; Rayleigh-Ritz methods; Thin walled components; Thin-walled; thin-walled aerospace structures; Trial functions; Work pieces; Aerospace industry; Aspect ratio; Dynamic models; Dynamic response; Milling (machining); Thin walled structures; Finite element method
AbstractMany of the aerospace components are characterized by having pocket-shaped thin-walled structures. During milling, the varying dynamics of the workpiece due to the change of thickness affects the final part quality. Available dynamic models rely on computationally prohibitive techniques that limit their use in the aerospace industry. In this paper, a new dynamic model was developed to predict the vibrations of thin-walled pocket structures during milling while taking into account the continuous change of thickness. The model is based on representing the change of thickness of a pocket-structure with a two-directional multispan plate. For the model formulation, the Rayleigh-Ritz method is used together with multispan beam models for the trial functions in both the x- and y-directions. An extensive finite element (FE) validation of the developed model was performed for different aspect ratios of rectangular and nonrectangular pockets and various change of thickness schemes. It was shown that the proposed model can accurately capture the dynamic effect of the change of thickness with prediction errors of less than 5 and at least 20 times reduction in the computation time. Experimental validation of the models was performed through the machining of thin-walled components. The predictions of the developed models were found to be in excellent agreement with the measured dynamic responses. © 2011 American Society of Mechanical Engineers.
Publication date
AffiliationNational Research Council Canada (NRC-CNRC); Aerospace (AERO-AERO)
Peer reviewedYes
NPARC number21271086
Export citationExport as RIS
Report a correctionReport a correction
Record identifierc0bbc111-ef68-4c5b-8d4c-8241d99b5297
Record created2014-03-24
Record modified2016-05-09
Bookmark and share
  • Share this page with Facebook (Opens in a new window)
  • Share this page with Twitter (Opens in a new window)
  • Share this page with Google+ (Opens in a new window)
  • Share this page with Delicious (Opens in a new window)