发明申请
US20130098039A1 EXHAUST DIFFUSER ADJUSTMENT SYSTEM FOR A GAS TURBINE ENGINE 失效
用于气体涡轮发动机的排气歧管调节系统

  • 专利标题: EXHAUST DIFFUSER ADJUSTMENT SYSTEM FOR A GAS TURBINE ENGINE
  • 专利标题(中): 用于气体涡轮发动机的排气歧管调节系统
  • 申请号: US13276346
    申请日: 2011-10-19
  • 公开(公告)号: US20130098039A1
    公开(公告)日: 2013-04-25
  • 发明人: John A. OrosaJason A. Kopko
  • 申请人: John A. OrosaJason A. Kopko
  • 主分类号: F02C7/00
  • IPC分类号: F02C7/00
EXHAUST DIFFUSER ADJUSTMENT SYSTEM FOR A GAS TURBINE ENGINE
摘要:
A turbine exhaust diffuser adjustment system for a gas turbine engine capable of altering the flow of turbine exhaust gases is disclosed. The turbine exhaust diffuser adjustment system may be formed from one or more flow ramps positioned in a flowpath. The flow ramp may include a downstream, radially outward point that extends radially outward further from the ID flowpath boundary than an upstream, radially outward point that is positioned upstream from the downstream, radially outward point. The flow ramp may be adjustable such that an angular position of a radially outer surface of the flow ramp may be adjusted relative to the ID flowpath boundary, thereby enabling the flowpath to be changed during turbine operation to enhance the efficiency of the turbine engine throughout its range of operation.
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