Invention Grant
US07901182B2 Near wall cooling for a highly tapered turbine blade 有权
用于高锥度涡轮叶片的近壁冷却

  • Patent Title: Near wall cooling for a highly tapered turbine blade
  • Patent Title (中): 用于高锥度涡轮叶片的近壁冷却
  • Application No.: US11804434
    Application Date: 2007-05-18
  • Publication No.: US07901182B2
    Publication Date: 2011-03-08
  • 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: F01D5/18
  • IPC: F01D5/18
Near wall cooling for a highly tapered turbine blade
Abstract:
A turbine blade having a pressure sidewall and a suction sidewall connected at chordally spaced leading and trailing edges to define a cooling cavity. Pressure and suction side inner walls extend radially within the cooling cavity and define pressure and suction side near wall chambers. A plurality of mid-chord channels extend radially from a radially intermediate location on the blade to a tip passage at the blade tip for connecting the pressure side and suction side near wall chambers in fluid communication with the tip passage. In addition, radially extending leading edge and trailing edge flow channels are located adjacent to the leading and trailing edges, respectively, and cooling fluid flows in a triple-pass serpentine path as it flows through the leading edge flow channel, the near wall chambers and the trailing edge flow channel.
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