Invention Grant
US08192146B2 Turbine blade dual channel cooling system 有权
涡轮叶片双通道冷却系统

  • Patent Title: Turbine blade dual channel cooling system
  • Patent Title (中): 涡轮叶片双通道冷却系统
  • Application No.: US12397788
    Application Date: 2009-03-04
  • Publication No.: US08192146B2
    Publication Date: 2012-06-05
  • Inventor: George Liang
  • Applicant: George Liang
  • Applicant Address: US FL Orlando
  • Assignee: Siemens Energy, Inc.
  • Current Assignee: Siemens Energy, Inc.
  • Current Assignee Address: US FL Orlando
  • Main IPC: F03B11/00
  • IPC: F03B11/00
Turbine blade dual channel cooling system
Abstract:
A turbine blade having an internal cooling system with dual serpentine cooling channels in communication with tip cooling channels is disclosed. In at least one embodiment, the cooling system may include first and second tip cooling channels in communication with the first and second serpentine cooling channels, respectively. The first tip cooling channel may extend from the leading edge to the trailing edge and be formed from a first suction side tip cooling channel and a first pressure side tip cooling channel. The second tip cooling channel may extend from a midchord region toward the trailing edge and may be positioned between the pressure and suction sides such that the second tip cooling channel is positioned generally between the first suction side and pressure side tip cooling channels. The first and second tip cooling channels may exhaust cooling fluids through the trailing edge.
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