发明授权
EP2125282B1 PROCÉDÉ DE RÉPARATION DE PIÈCES USINÉES TELLES QUE DES AUBES DE TURBOMACHINES OU DES PALES DE DAM 有权
方法的修复加工工件如何TURBOMASCHINEN勺或整体叶盘

  • 专利标题: PROCÉDÉ DE RÉPARATION DE PIÈCES USINÉES TELLES QUE DES AUBES DE TURBOMACHINES OU DES PALES DE DAM
  • 专利标题(英): Method for repairing machined components such as turbomachine blades or blisk blades
  • 专利标题(中): 方法的修复加工工件如何TURBOMASCHINEN勺或整体叶盘
  • 申请号: EP08787820.3
    申请日: 2008-03-19
  • 公开(公告)号: EP2125282B1
    公开(公告)日: 2010-12-08
  • 发明人: DERRIEN, GérardKERNEIS, StéphaneGASNE, LudovicLEONETTI, Claude
  • 申请人: SNECMA
  • 申请人地址: 2, boulevard du Général Martial Valin 75015 Paris FR
  • 专利权人: SNECMA
  • 当前专利权人: SNECMA
  • 当前专利权人地址: 2, boulevard du Général Martial Valin 75015 Paris FR
  • 代理机构: Bloch & Bonnétat
  • 优先权: FR0702021 20070320
  • 国际公布: WO2008135656 20081113
  • 主分类号: B23P6/00
  • IPC分类号: B23P6/00 F01D5/00 G05B19/425 G05B19/4097
PROCÉDÉ DE RÉPARATION DE PIÈCES USINÉES TELLES QUE DES AUBES DE TURBOMACHINES OU DES PALES DE DAM
摘要:
The invention relates to a method for repairing by machining a workpiece (1) such as the vane of a turbomachine, from a known process of the part (B), wherein said method includes the step of deforming (32) the profile (B) by a morphing process so that the deformed profile interpolates a cloud of points (A) measured on the part. The deformation of the profile (B) includes a comparison of each having an excessive or non-sufficient thickness (20) on the part to be machined (1) with elementary deformation configurations (CED) (5) each in the form of a mapping and points portion, the elementary deformation configurations (CED) (5) being stored in a database (100), and the database (100) associating for each elementary deformation configurations (CED) (102) the parameters of the morphing function (101).
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