发明申请
US20100135774A1 BALANCING FLYWEIGHT, ROTOR DISK EQUIPPED THEREWITH, ROTOR AND AIRCRAFT ENGINE COMPRISING THEM 有权
平衡飞轮,装有转子盘,转子和包括它们的飞机发动机

  • 专利标题: BALANCING FLYWEIGHT, ROTOR DISK EQUIPPED THEREWITH, ROTOR AND AIRCRAFT ENGINE COMPRISING THEM
  • 专利标题(中): 平衡飞轮,装有转子盘,转子和包括它们的飞机发动机
  • 申请号: US11622667
    申请日: 2007-01-12
  • 公开(公告)号: US20100135774A1
    公开(公告)日: 2010-06-03
  • 发明人: Laurent Gilles Dezouche
  • 申请人: Laurent Gilles Dezouche
  • 申请人地址: FR Paris
  • 专利权人: SNECMA
  • 当前专利权人: SNECMA
  • 当前专利权人地址: FR Paris
  • 优先权: FR0650125 20060113
  • 主分类号: F04D29/66
  • IPC分类号: F04D29/66
BALANCING FLYWEIGHT, ROTOR DISK EQUIPPED THEREWITH, ROTOR AND AIRCRAFT ENGINE COMPRISING THEM
摘要:
The balancing flyweight of a turbomachine rotor includes two pyramid shaped end parts each one having a base and an apex, and an intermediate part which connects the two bases of the end parts together. The two apexes are aligned on a longitudinal axis. The two end parts and the intermediate part exhibit, in cross section through a plane perpendicular to the longitudinal axis, cross-sections having polygonal shapes centered on said longitudinal axis.
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