Invention Grant
US08348615B2 Turbine engine rotor disc with cooling passage 有权
具有冷却通道的涡轮发动机转子盘

  • Patent Title: Turbine engine rotor disc with cooling passage
  • Patent Title (中): 具有冷却通道的涡轮发动机转子盘
  • Application No.: US12310285
    Application Date: 2007-08-15
  • Publication No.: US08348615B2
    Publication Date: 2013-01-08
  • Inventor: Richard BluckPaul Jacklin
  • Applicant: Richard BluckPaul Jacklin
  • Applicant Address: DE München
  • Assignee: Siemens Aktiengesellschaft
  • Current Assignee: Siemens Aktiengesellschaft
  • Current Assignee Address: DE München
  • Priority: EP06017536 20060823
  • International Application: PCT/EP2007/058434 WO 20070815
  • International Announcement: WO2008/022954 WO 20080228
  • Main IPC: F01D5/18
  • IPC: F01D5/18
Turbine engine rotor disc with cooling passage
Abstract:
Disclosed is a gas turbine engine rotor disc with a plurality of cooling passages having an essentially radial orientation relative to an axis of rotation of the rotor disc, each cooling passage having an inlet and an outlet and being included relative to a rotor disc surface and a cut-out arranged at the passage at an outlet end of the passage. Each cooling passage terminating in a slot is arranged in the periphery of the rotor disc. Each slot is sized and configured to receive a glade root.
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