发明名称 Method for developing range of finishing turbomachine part e.g. compressor disk by drag finishing, involves performing reduction of possible choice of parameters to be applied during drag finishing or vibratory finishing
摘要 <p>The method involves defining a set of parameters to be applied during drag finishing or vibratory finishing with regard to quality of abrasive stones, and a possible liquid such as water, utilized for bathing of the stones. A set of frequency and amplitude of vibrations is determined. A wear of the stones is determined. A preliminary step of reduction of possible choice of the parameters to be applied during drag finishing or vibratory finishing is performed by application of exploratory ranges on identical polishing test-tubes (7) presenting simple geometrical forms. An independent claim is also included for a device for developing a range of finishing a turbomachine part by drag finishing or vibratory finishing.</p>
申请公布号 FR3001167(A1) 申请公布日期 2014.07.25
申请号 FR20130050545 申请日期 2013.01.22
申请人 SNECMA;CENTRE NATIONAL DE LA RECHERCHE SCIENTIFIQUE - CNRS;ECOLE NATIONALE D'INGENIEUR DE ST ETIENNE 发明人 GRANGE FABIEN;TEXIER ANTHONY;KERMOUCHE GUILLAUME;RECH JOEL
分类号 B23P9/00;B24B31/00 主分类号 B23P9/00
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