Invention Grant
US08382030B2 Variable cycle VTOL powerplant 失效
可变循环VTOL动力装置

  • Patent Title: Variable cycle VTOL powerplant
  • Patent Title (中): 可变循环VTOL动力装置
  • Application No.: US12807311
    Application Date: 2010-09-02
  • Publication No.: US08382030B2
    Publication Date: 2013-02-26
  • Inventor: Patrick A. Kosheleff
  • Applicant: Patrick A. Kosheleff
  • Main IPC: B64C29/00
  • IPC: B64C29/00
Variable cycle VTOL powerplant
Abstract:
A VTOL aircraft powerplant choosing between a low-power, turbofan mode during cruise flight and a high-power, lift fan mode during vertical flight. Turbofan mode is a gas turbine engine's shaft power driving a remote front fan. Its fan flow goes to thrust for cruising flight. During VTOL, front fan output enters a boost compressor. It produces the compressed air for a combustion chamber which feeds a large lift-fan turbine. That is the implementation of lift-fan mode. The boost compressor has more stages than the front fan and is a big added load. The gas turbine engine is supercharged to turn that added load: Part of the boost compressor output is taken during VTOL. This is a new version of the supercharging. During cruise flight, a low pressure turbine stage is bypassed to match the lesser load. That completes the apparatus for a variable-cycle VTOL engine.
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