发明名称 |
GASEOUS OXYGEN RESONANCE IGNITER |
摘要 |
A gaseous oxygen resonance igniter includes a body with a first inlet for gaseous oxygen incorporating a supersonic nozzle. An outlet from the body incorporates an orifice of predetermined size to maintain a desired pressure in the body. An aperture in the body opposite the first inlet provides a port to a ceramic resonance cavity. A ceramic bleed disc is engaged at a second end of the resonance cavity. An end cap incorporates a plenum adapted to receive high temperature oxygen flow from the resonance cavity through the bleed disc. An exhaust port is connected to the plenum for the high temperature oxygen which flows to a mixing chamber which introduces pilot fuel for ignition as a combustion initiation torch.
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申请公布号 |
US2005221245(A1) |
申请公布日期 |
2005.10.06 |
申请号 |
US20040818645 |
申请日期 |
2004.04.05 |
申请人 |
ELVANDER JOSHUA E;FISHER STEVEN C;MIYATA SHINJIRO |
发明人 |
ELVANDER JOSHUA E.;FISHER STEVEN C.;MIYATA SHINJIRO |
分类号 |
F23Q9/00;F23Q13/00;(IPC1-7):F23Q9/00 |
主分类号 |
F23Q9/00 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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