Turbojet engine

Turbojet engine

  • CN 102,562,361 A
  • Filed: 02/10/2012
  • Published: 07/11/2012
  • Est. Priority Date: 02/10/2012
  • Status: Active Grant
First Claim
Patent Images

1. turbojet engine;

  • Comprise rotating shaft, gas compressor, firing chamber and turbo machine;

    Gas compressor and turbo machine comprise leaf dish and a plurality of blade structure all around, it is characterized in that;

    said gas compressor and turbo machine one of them flabellum inside at least are provided with the fluid passage;

    The lee face of said flabellum is provided with the fluid introducing port, and said fluid introducing port communicates with the fluid passage;

    The blade tip rear portion of said flabellum lee face is provided with the fluid export mouth, and said fluid export mouth communicates with the fluid passage.

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