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contributor authorKaszynski, Alex A.
contributor authorBeck, Joseph A.
contributor authorBrown, Jeffrey M.
date accessioned2017-05-09T00:58:32Z
date available2017-05-09T00:58:32Z
date issued2013
identifier issn1528-8919
identifier othergtp_135_10_102504.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/151702
description abstractAn automated reverse engineering process is developed that uses a structured light optical measurement system to collect dense point cloud geometry representations. The modeling process is automated through integration of software for point cloud processing, reverse engineering, solid model creation, grid generation, and structural solution. Process uncertainties are quantified on a calibration block and demonstrated on an academic transonic integrally bladed rotor. These uncertainties are propagated through physicsbased models to assess impacts on predicted modal and mistuned forced response. Process details are discussed and recommendations made on reducing uncertainty. Reverse engineered parts averaged a deviation of 0.0002 in. (5 خ¼m) which did not significantly impact low and midrange frequency responses. High frequency modes were found to be sensitive to these uncertainties demonstrating the need for future refinement of reverse engineering processes.
publisherThe American Society of Mechanical Engineers (ASME)
titleUncertainties of an Automated Optical 3D Geometry Measurement, Modeling, and Analysis Process for Mistuned Integrally Bladed Rotor Reverse Engineering
typeJournal Paper
journal volume135
journal issue10
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4025000
journal fristpage102504
journal lastpage102504
identifier eissn0742-4795
treeJournal of Engineering for Gas Turbines and Power:;2013:;volume( 135 ):;issue: 010
contenttypeFulltext


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