发明名称 |
Aircraft engine ignition system |
摘要 |
A plasma jet igniter is used to reliably relight a jet engine at high altitudes under adverse combustion conditions. The air-fuel mixture from the primary combustion zone of the jet engine combustor may be used as the plasma medium or, alternatively, liquid fuel direct from the aircraft fuel system may be used as a fuel charge.
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申请公布号 |
US5367871(A) |
申请公布日期 |
1994.11.29 |
申请号 |
US19930046707 |
申请日期 |
1993.04.16 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
VENKATARAMANI, KATTALAICHERI S.;SCOTT, JOHN C. |
分类号 |
F02C7/264;F02P9/00;H01T13/50;(IPC1-7):F02C7/264 |
主分类号 |
F02C7/264 |
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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