发明申请
- 专利标题： Off-axis pulse detonation configuration for gas turbine engine
- 专利标题（中）： 燃气涡轮发动机的离轴脉冲爆震配置
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申请号： US10870876申请日： 2004-06-18
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公开(公告)号： US20050279077A1公开(公告)日： 2005-12-22
- 发明人: Edward Hall , Adam Rasheed , Anthony Dean
- 申请人： Edward Hall , Adam Rasheed , Anthony Dean
- 专利权人： General Electric Company
- 当前专利权人： General Electric Company
- 主分类号： F02C5/00
- IPC分类号： F02C5/00 ; F02C5/02 ; F02K5/02 ; F02K7/02 ; F02K9/78
摘要：
The present invention is a gas turbine engine system containing a compressor stage, a pulse detonation stage, and a turbine stage. During operation of the engine system, compressed flow from the compressor stage is directed to at least one off-axis pulse detonation tube in the pulse detonation stage. The off-axis pulse detonation tube detonates a mixture containing the compressed flow and a fuel to create a detonation wave, which is routed to an inlet portion of a reverse flow turbine. The exhaust flow from the reverse flow turbine is then directed away from the engine through ducting.